command: ./cs_solver *************************************************************** (R) Code_Saturne Version 7.0.2 Copyright (C) 1998-2021 EDF S.A., France revision d029e16a2 build Tue 12 Oct 2021 05:18:20 PM CEST The Code_Saturne CFD tool is free software; you can redistribute it and/or modify it under the terms of the GNU General Public License as published by the Free Software Foundation; either version 2 of the License, or (at your option) any later version. The Code_Saturne CFD tool is distributed in the hope that it will be useful, but WITHOUT ANY WARRANTY; without even the implied warranty of MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU General Public License for more details. *************************************************************** Local case configuration: Date: Mon 03 Jan 2022 11:30:36 AM CET System: Linux 4.9.0-16-amd64 (Scibian 9.0) Machine: gacn0102 Processor: model name : Intel(R) Xeon(R) Gold 6140 CPU @ 2.30GHz Memory: 192108 MB User: f08055 (BENOIT DE LAAGE DE MEUX) Directory: /gpfsgaia/scratch/F08055/VARIOUS_CASES/rot_disk/RANS1/RESU/20220103-1130 OpenMP threads: 1 Processors/node: 36 Compilers used for build: C compiler: icc (ICC) 18.0.1 20171018 C++ compiler: icpc (ICC) 18.0.1 20171018 Fortran compiler: ifort (IFORT) 18.0.1 20171018 MPI version 3.1 (MPICH 3.2) I/O read method: standard input and output, serial access I/O write method: standard input and output, serial access External libraries for partitioning: ParMETIS 4.0.3 PT-SCOTCH 6.0.6 =============================================================== CALCULATION PREPARATION ======================= =========================================================== No error detected during the data verification cs_user_parameters.f90 and others). =========================================================== CALCULATION PARAMETERS SUMMARY ============================== ----------------------------------------------------------- ** DIMENSIONS ---------- --- Physics NVAR = 8 (Nb variables ) NSCAL = 1 (Nb scalars ) NSCAUS = 0 (Nb user scalars ) NSCAPP = 1 (Nb specific physics scalars ) ----------------------------------------------------------- ** HOMOGENEOUS MIXTURE MODEL VoF ---------------------------------------- IVOFMT = 0 ( 0 : disabled ) ( > 0: enabled ) ----------------------------------------------------------- ** TIME STEPPING ------------- --- Per-variable properties ------------------------------------ Variable ISTAT CDTVAR ------------------------------------ Velocity 1 0.1000E+01 Pressure 0 0.1000E+01 k 1 0.1000E+01 omega 1 0.1000E+01 TempK 1 0.1000E+01 Wall distance 0 0.1000E+01 ---------------------------- ISTAT = 0 ou 1 (1 for unsteady ) CDTVAR > 0 (time step multiplier ) --- Order of base time stepping scheme ISCHTP = 1 (1: order 1; 2: order 2 ) ----------------------------------------------------------- ** STOKES ------ -- Continuous phase: ISTMPF = 1 (time scheme for flow (0: explicit (THETFL = 0 ) (1: std scheme (Saturne 1.0 ) (2: 2nd-order (THETFL = 0.5 ) THETVI = 0.00000E+00 (theta for total viscosity ((1+theta).new-theta.old THETCP = -0.99900E+03 (specific heat theta-scheme ((1+theta).new-theta.old THETSN = 0.00000E+00 (Nav-Stokes S.T. theta scheme) ((1+theta).new-theta.old THETST = 0.00000E+00 (Turbulence S.T. theta-scheme) ((1+theta).new-theta.old EPSUP = 0.10000E-04 (Velocity/pressure coupling stop test ) ----------------------------------------------------------- ** WALL DISTANCE COMPUTATION ------------------------- ICDPAR = 1 ( 1: std, reread if restart (-1: std, recomputed if restrt ( 2: old, reread if restart (-2: old, recomputed if restrt ----------------------------------------------------------- ** SCALARS ------- ITBRRB = 0 (T or H reconstruction at bdy) ----------------------------------------------------- Variable Number ITURT ----------------------------------------------------- TempK 1 0 ------------------------------------------------------------- ------------------------------------ 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. is_temerature = 0 or 1 (use Cp or not ) VISLS0 = >0 (Reference viscosity ) SIGMAS = >0 (Schmidt ) RVARFL = >0 (Rf, cf variance dissipation ) ICLVFL = 0, 1 or 2 (Variance clipping mode ) SCAMIN = (Min authorized value ) SCAMAX = (Max authorized value ) For variances, SCAMIN is ignored and SCAMAX is used only if ICLVFL = 2 ------------------------------------------------------ Scalar THETSS THETVS ------------------------------------------------------ 1 0.0000E+00 0.0000E+00 ------------------------------------------------------ THETSS = (theta for source terms ) ((1+theta).new-theta.old ) THETVS = (theta for scalar diffusivity ((1+theta).new-theta.old ) ----------------------------------------------------------- ** CALCULATION MANAGEMENT ---------------------- --- Restarted calculation ISUITE = 0 (1: restarted calculation ) ILEAUX = 1 (1: read restart/auxiliary ) IECAUX = 1 (1: write checkpoint/auxiliary) --- Calculation time The numbering of time steps and the measure of simulated physical time are absolute values, and not values relative to the current calculation. NTPABS = 0 (Initial time step) NTMABS = 1000000 (Final time step required) ----------------------------------------------------------- ** INPUT-OUTPUT ------------ --- Restart file NTSUIT = 2400 (Checkpoint frequency ) --- Probe history files NTHIST = 1 (Output frequency ) FRHIST = -.10000E+01 (Output frequency (s) ) -- -- -- --- run_solver.log files NTLIST = 1 (Output frequency ) -- -- -- --- Additional post-processing variables (ipstdv) ipstfo = 7 (Force exerted by the fluid on the boundary) ipstyp = 1 (y+ at boundary) ipsttp = 1 (T+ at boundary) ipstft = 1 (Thermal flux at boundary) ipstnu = 1 (Dimensionless thermal flux at boundary) ----------------------------------------------------------- ** ALE METHOD (MOVING MESH) ----------- IALE = 0 (1: activated,2: CDO ) NALINF = 0 (Fluid initialization iterations) IFLXMW = 0 (ALE mass flux computation 0: thanks to vertices 1: thanks to mesh velocity) ----------------------------------------------------------- Postprocessing output writers: ------------------------------ -1: name: results directory: postprocessing format: EnSight Gold options: separate_meshes time dependency: fixed mesh output: every 800 time steps, at start, at end -5: name: directory: monitoring format: time_plot options: CSV time dependency: fixed mesh output: every time step -6: name: directory: profiles format: plot options: time dependency: fixed mesh output: at end -7: name: histograms directory: histograms format: histogram options: txt time dependency: fixed mesh output: at end Reading file: mesh_input.csm Finished reading: mesh_input.csm Number of cells: 79200 ---------------------------------------------------------- Number of cells + halo cells: 79200 ---------------------------------------------------------- Number of interior faces: 157608 ---------------------------------------------------------- Number of boundary faces: 159984 ---------------------------------------------------------- Histogram of the number of interior faces per cell: minimum value = 3 maximum value = 4 1 : [ 3 ; 4 ] = 79200 ---------------------------------------------------------- Renumbering mesh: renumbering for cells: pre-numbering: no renumbering cells adjacent to ghost cells last: no numbering: no renumbering renumbering for interior faces: cell adjacency pre-ordering: lowest id first faces adjacent to ghost cells last: no numbering: multipass renumbering for boundary faces: numbering: no shared cell across threads renumbering for vertices: numbering: no renumbering Numbering for cells: type: default number of halo-adjacent elements: 79200 Numbering for interior faces: type: default number of halo-adjacent elements: 157608 Numbering for boundary faces: type: default number of halo-adjacent elements: 159984 ---------------------------------------------------------- Matrix bandwidth for volume mesh : 19900 Matrix profile/lines for volume mesh : 299 Mesh coordinates: minimum and maximum X : 0.0000000e+00 5.0000002e-04 Y : -2.3997934e-01 2.3997934e-01 Z : -2.3997934e-01 2.3997934e-01 Mesh Number of cells: 79200 Number of interior faces: 157608 Number of boundary faces: 159984 Number of vertices: 159984 Groups: "Bohn_1995_configB_2D_Ra1E7" cells: 79200 boundary faces: 159984 "DOWN" boundary faces: 792 "LEFT" boundary faces: 79200 "RIGHT" boundary faces: 79200 "UP" boundary faces: 792 --- Information on the volumes Minimum control volume = 9.8138905e-11 Maximum control volume = 1.3847289e-09 Total volume for the domain = 6.5906818e-05 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 (0.105 s) --- Information on volume zones Volume zone "cells" id = 0 Number of cells = 79200 Volume = 6.5907e-05 Center of gravity = (0.00025, 2.6223e-08, -2.6189e-08) Surface = -1 (not computed) Volume zone "all_cells" id = 1 Number of cells = 79200 Volume = 6.5907e-05 Center of gravity = (0.00025, 2.6223e-08, -2.6189e-08) Surface = -1 (not computed) --- Information on boundary zones Boundary zone "boundary_faces" id = 0 Number of faces = 159984 Surface = 0.26477 Center of gravity = (0.00025, 2.7061e-08, -2.7027e-08) Perimeter = -1 (not computed) Boundary zone "HUB" id = 1 Number of faces = 792 Surface = 0.00039265 Center of gravity = (0.00025, -5.4565e-08, 5.4543e-08) Perimeter = -1 (not computed) Boundary zone "BC_2" id = 2 Number of faces = 79200 Surface = 0.13181 Center of gravity = (7.0183e-18, 2.7121e-08, -2.7087e-08) Perimeter = -1 (not computed) Boundary zone "BC_3" id = 3 Number of faces = 79200 Surface = 0.13181 Center of gravity = (0.0005, 2.7121e-08, -2.7087e-08) Perimeter = -1 (not computed) Boundary zone "SHROUD" id = 4 Number of faces = 792 Surface = 0.00075388 Center of gravity = (0.00025, 4.8617e-08, -4.8573e-08) Perimeter = -1 (not computed) Probe set: "probes": maximum distance between cell centers and requested coordinates: 4.402e-07 ALMAX = 0.40393E-01 (Characteristic length ) ALMAX is the cubic root of the domain volume. ALMAX is the length used to initialize the turbulence. -------------------------------------------------------------------------------- ** VARIABLES INITIALIZATION ------------------------ ----------------------------------------- Property Min. value Max. value ----------------------------------------- density 0.1205E+01 0.1205E+01 molecular_viscos 0.1810E-04 0.1810E-04 turbulent_viscos 0.1192E-02 0.1192E-02 ----------------------------------------- --- 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 1584 Rough wall 6 0 Symmetry 4 158400 Free outlet 3 0 Free inlet 14 0 Convective inlet 16 0 Free surface 15 0 Undefined 1 0 ------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] 0 0 0 0 v Velocity[Y] 0 0 0 0 v Velocity[Z] 0 0 0 0 v ǁVelocityǁ 0 0 0 0 v Pressure 0 0 0 0 v k 0.0006 0.0006 0.0006 0.0006 v omega 0.60641 0.60641 0.60641 0.60641 v TempK 288 288 288 288 v Density 1.205 1.205 1.205 1.205 v TurbVisc 0.0011923 0.0011923 0.0011923 0.0011923 v CourantNb 0 0 0 0 v FourierNb 0 0 0 0 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 0 0 0 0 v volume_forces[X] 0 0 0 0 v volume_forces[Y] 0 0 0 0 v volume_forces[Z] 0 0 0 0 v ǁvolume_forcesǁ 0 0 0 0 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 288 288 288 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0 0 0 =============================================================== MAIN CALCULATION ================ =============================================================== =============================================================== INSTANT 0.963000000E-03 TIME STEP NUMBER 1 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.92226E-10 0.92384E-10 Friction velocity uk : 0.16270E-02 0.16279E-02 Dimensionless distance yplus : 0.10824E-01 0.10843E-01 Friction thermal sca. tstar : -0.72201E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.76024E-02 0.76154E-02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** WALL DISTANCE ------------- Min distance = 0.99922E-04 Max distance = 0.57120E-01 ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.92226E-10 0.92384E-10 Friction velocity uk : 0.16270E-02 0.16279E-02 Dimensionless distance yplus : 0.10824E-01 0.10843E-01 Friction thermal sca. tstar : -0.72201E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.76024E-02 0.76154E-02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 c Velocity[X] 0.00000E+00 c Velocity[Y] 0.00000E+00 c Velocity[Z] 0.00000E+00 c Pressure 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 c k 0.19493E-06 28 0.53778E-03 0.74822E-01 0.97190E+03 c omega 0.22321E+03 21 0.53308E-03 0.79423E+07 0.10313E+04 c TempK 0.94131E+02 34 0.81594E-05 0.54107E+03 0.26017E+01 c Wall distance 0.25964E-06 22 0.39335E-03 0.11510E+01 0.10384E+04 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] 0 0 0 0 v Velocity[Y] 0 0 0 0 v Velocity[Z] 0 0 0 0 v ǁVelocityǁ 0 0 0 0 v Pressure 0 0 0 0 v k 2.283e-05 0.015141 0.0083559 0.0088004 v omega 88.062 88.062 88.062 88.062 v TempK 288 296.74 288.36 288.11 v Density 1.205 1.205 1.205 1.205 v TurbVisc 0.0011923 0.0011923 0.0011923 0.0011923 v CourantNb 0 0 0 0 v FourierNb 1.4213 42.002 6.5138 3.1029 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] 0 0 0 0 v volume_forces[Z] 0 0 0 0 v ǁvolume_forcesǁ 0 0 0 0 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 288.27 288.16 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.010843 0.00010725 4.6897e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.4213 42.002 6.5138 3.1029 INSTANT 0.192600000E-02 TIME STEP NUMBER 2 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10604E-08 0.10691E-08 Friction velocity uk : 0.14059E-03 0.14159E-03 Dimensionless distance yplus : 0.93533E-03 0.94304E-03 Friction thermal sca. tstar : -0.70246E+05 0.00000E+00 Dim-less thermal sca. tplus : 0.65692E-03 0.66233E-03 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10604E-08 0.10691E-08 Friction velocity uk : 0.14059E-03 0.14159E-03 Dimensionless distance yplus : 0.93533E-03 0.94304E-03 Friction thermal sca. tstar : -0.70246E+05 0.00000E+00 Dim-less thermal sca. tplus : 0.65692E-03 0.66233E-03 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.51319E-10 5 0.53559E-02 0.66770E-10 0.10384E+04 c Velocity[X] 0.17478E-28 c Velocity[Y] 0.33385E-10 c Velocity[Z] 0.33385E-10 c Pressure 0.40755E-11 44 0.72767E-08 0.20461E-03 0.10384E+04 c k 0.28825E-05 4 0.45523E-05 0.10315E-04 0.11510E+02 c omega 0.66352E+01 4 0.19481E-03 0.70775E+12 0.10382E+04 c TempK 0.94142E+02 3 0.66350E-06 0.95727E+03 0.34598E+01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -4.5814e-15 4.9434e-15 -2.3999e-19 -6.1527e-20 v Velocity[Y] -3.0769e-06 3.0844e-06 -1.8637e-12 -1.1481e-12 v Velocity[Z] -3.0845e-06 3.0768e-06 7.3542e-13 1.7741e-14 v ǁVelocityǁ 6.1717e-13 3.6325e-06 1.4702e-07 6.0421e-08 v Pressure -9.9092e-06 0.0007882 2.2826e-05 3.1484e-21 v k 5.9458e-05 0.014732 0.0083025 0.0087336 v omega 87.452 4.3355e+05 10904 2017.3 v TempK 288 316.09 288.62 288.17 v Density 1.205 1.205 1.205 1.205 v TurbVisc 3.124e-07 0.00020719 0.00011434 0.00012042 v CourantNb 3.9593e-12 5.9861e-06 2.9067e-07 1.1575e-07 v FourierNb 0.15504 1.3442 0.46093 0.30483 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -0.80094 0.80094 3.2432e-05 3.5056e-08 v volume_forces[Z] -0.80094 0.80094 -3.2428e-05 -3.3742e-08 v ǁvolume_forcesǁ 0 0.80127 0.03299 0.0098902 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 288.63 288.26 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.00094304 9.291e-06 4.0608e-06 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.15504 1.3442 0.46093 0.30483 INSTANT 0.288900000E-02 TIME STEP NUMBER 3 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.51226E-09 0.66514E-03 Friction velocity uk : 0.29035E-03 0.77081E-03 Dimensionless distance yplus : 0.19334E-02 0.51283E-02 Friction thermal sca. tstar : -0.19391E+05 0.00000E+00 Dim-less thermal sca. tplus : 0.13579E-02 0.36018E-02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.51226E-09 0.66514E-03 Friction velocity uk : 0.29035E-03 0.77081E-03 Dimensionless distance yplus : 0.19334E-02 0.51283E-02 Friction thermal sca. tstar : -0.19391E+05 0.00000E+00 Dim-less thermal sca. tplus : 0.13579E-02 0.36018E-02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.15583E-09 10 0.42842E-02 0.25545E-09 0.70090E+03 c Velocity[X] 0.31071E-27 c Velocity[Y] 0.12773E-09 c Velocity[Z] 0.12773E-09 c Pressure 0.10572E-10 37 0.88039E-08 0.18979E-03 0.22169E+03 c k 0.28593E-05 4 0.34360E-05 0.98792E-05 0.11361E+02 c omega 0.11220E+03 2 0.51871E-05 0.15427E+12 0.90826E+03 c TempK 0.94149E+02 3 0.34759E-06 0.27200E+03 0.18439E+01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -2.1517e-14 2.547e-14 -2.1644e-18 -5.2249e-19 v Velocity[Y] -1.2637e-05 1.2818e-05 -4.0732e-12 -2.5549e-12 v Velocity[Z] -1.2819e-05 1.2637e-05 3.7274e-12 2.1499e-12 v ǁVelocityǁ 2.6373e-12 1.5034e-05 4.0577e-07 1.5904e-07 v Pressure -1.1496e-05 0.0011222 2.6941e-05 1.0449e-21 v k 1.8445e-06 0.014453 0.0082236 0.0086624 v omega 86.851 2.3029e+05 6036.7 1155.2 v TempK 288 324.98 288.79 288.21 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.6526e-10 0.00020286 0.00011238 0.0001198 v CourantNb 3.8729e-12 1.7145e-05 7.9251e-07 3.0215e-07 v FourierNb 0.15498 1.3387 0.42578 0.29578 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -2.5731 2.5731 5.6016e-05 3.5675e-08 v volume_forces[Z] -2.5731 2.5731 -5.6011e-05 -3.4072e-08 v ǁvolume_forcesǁ 2.2311e-11 2.574 0.057116 0.015678 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 288.89 288.33 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.0051283 2.8542e-05 1.3768e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.15498 1.3387 0.42578 0.29578 INSTANT 0.385200000E-02 TIME STEP NUMBER 4 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.69524E-08 0.15033E-02 Friction velocity uk : 0.21567E-04 0.15024E-02 Dimensionless distance yplus : 0.14361E-03 0.99956E-02 Friction thermal sca. tstar : -0.26281E+05 0.00000E+00 Dim-less thermal sca. tplus : 0.10086E-03 0.70203E-02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.69524E-08 0.15033E-02 Friction velocity uk : 0.21567E-04 0.15024E-02 Dimensionless distance yplus : 0.14361E-03 0.99956E-02 Friction thermal sca. tstar : -0.26281E+05 0.00000E+00 Dim-less thermal sca. tplus : 0.10086E-03 0.70203E-02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.27049E-09 9 0.14887E-02 0.33701E-09 0.45502E+03 c Velocity[X] 0.15945E-27 c Velocity[Y] 0.16851E-09 c Velocity[Z] 0.16851E-09 c Pressure 0.62391E-11 35 0.51053E-08 0.82841E-04 0.15960E+03 c k 0.28365E-05 4 0.27755E-05 0.80999E-05 0.10374E+02 c omega 0.37211E+02 2 0.69947E-05 0.30789E+11 0.66557E+03 c TempK 0.94154E+02 2 0.20107E-05 0.11271E+03 0.11868E+01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -2.9641e-14 3.664e-14 -5.3465e-18 -1.2784e-18 v Velocity[Y] -2.2067e-05 2.2406e-05 -5.1176e-12 -2.7237e-12 v Velocity[Z] -2.2407e-05 2.2067e-05 4.486e-12 2.0428e-12 v ǁVelocityǁ 3.01e-12 2.6277e-05 7.097e-07 2.7482e-07 v Pressure -1.292e-05 0.0013809 3.0674e-05 6.0272e-21 v k 3.4034e-07 0.014177 0.0081542 0.0085938 v omega 86.257 1.3991e+05 3807.5 758.76 v TempK 288 329.35 288.92 288.25 v Density 1.205 1.205 1.205 1.205 v TurbVisc 9.651e-12 0.00020027 0.00011171 0.00011949 v CourantNb 1.3869e-11 2.9529e-05 1.3333e-06 5.0665e-07 v FourierNb 0.15491 1.3359 0.41884 0.2934 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -3.3873 3.3874 7.1246e-05 3.5807e-08 v volume_forces[Z] -3.3873 3.3874 -7.1241e-05 -3.3999e-08 v ǁvolume_forcesǁ 9.534e-11 3.3885 0.072694 0.019548 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 289.06 288.37 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.0099956 3.4547e-05 1.9663e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.15491 1.3359 0.41884 0.2934 INSTANT 0.481500000E-02 TIME STEP NUMBER 5 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.93326E-07 0.19873E-02 Friction velocity uk : 0.61988E-05 0.19866E-02 Dimensionless distance yplus : 0.41277E-04 0.13217E-01 Friction thermal sca. tstar : -0.15217E+05 0.00000E+00 Dim-less thermal sca. tplus : 0.28991E-04 0.92827E-02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.93326E-07 0.19873E-02 Friction velocity uk : 0.61988E-05 0.19866E-02 Dimensionless distance yplus : 0.41277E-04 0.13217E-01 Friction thermal sca. tstar : -0.15217E+05 0.00000E+00 Dim-less thermal sca. tplus : 0.28991E-04 0.92827E-02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.38288E-09 9 0.67152E-03 0.37015E-09 0.32842E+03 c Velocity[X] 0.13639E-27 c Velocity[Y] 0.18508E-09 c Velocity[Z] 0.18508E-09 c Pressure 0.40461E-11 31 0.63327E-08 0.46775E-04 0.12744E+03 c k 0.28142E-05 4 0.23515E-05 0.72566E-05 0.99005E+01 c omega 0.18307E+02 2 0.49792E-05 0.37038E+10 0.29658E+03 c TempK 0.94157E+02 2 0.17458E-05 0.63436E+02 0.89030E+00 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -3.2304e-14 3.5887e-14 -9.5109e-18 -2.2713e-18 v Velocity[Y] -2.9792e-05 3.0264e-05 -7.7043e-12 -4.3381e-12 v Velocity[Z] -3.0265e-05 2.9792e-05 6.0167e-12 2.6309e-12 v ǁVelocityǁ 9.259e-12 3.5521e-05 1.0324e-06 3.9892e-07 v Pressure -1.4305e-05 0.0015965 3.4293e-05 -1.3635e-22 v k 3.7662e-07 0.013917 0.0080871 0.0085264 v omega 85.672 1.0924e+05 2980.4 610.07 v TempK 288 331.76 289.02 288.27 v Density 1.205 1.205 1.205 1.205 v TurbVisc 2.9312e-12 0.00019767 0.00011106 0.00011919 v CourantNb 1.8779e-11 4.1808e-05 1.8817e-06 7.1756e-07 v FourierNb 0.15484 1.3257 0.41282 0.29121 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -3.7884 3.7884 8.2282e-05 3.4909e-08 v volume_forces[Z] -3.7884 3.7884 -8.2275e-05 -3.2438e-08 v ǁvolume_forcesǁ 1.0881e-10 3.7898 0.083978 0.022462 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 289.18 288.4 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.013217 4.5004e-05 2.5795e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.15484 1.3257 0.41282 0.29121 INSTANT 0.577800000E-02 TIME STEP NUMBER 6 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.22575E-07 0.23106E-02 Friction velocity uk : 0.66522E-05 0.23098E-02 Dimensionless distance yplus : 0.44296E-04 0.15367E-01 Friction thermal sca. tstar : -0.10705E+05 0.00000E+00 Dim-less thermal sca. tplus : 0.31111E-04 0.10793E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.22575E-07 0.23106E-02 Friction velocity uk : 0.66522E-05 0.23098E-02 Dimensionless distance yplus : 0.44296E-04 0.15367E-01 Friction thermal sca. tstar : -0.10705E+05 0.00000E+00 Dim-less thermal sca. tplus : 0.31111E-04 0.10793E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.49278E-09 8 0.36203E-03 0.38795E-09 0.25560E+03 c Velocity[X] 0.24604E-27 c Velocity[Y] 0.19397E-09 c Velocity[Z] 0.19397E-09 c Pressure 0.28692E-11 30 0.30303E-08 0.30687E-04 0.10719E+03 c k 0.27922E-05 4 0.20312E-05 0.66428E-05 0.95506E+01 c omega 0.13910E+02 2 0.13935E-05 0.16403E+09 0.66104E+02 c TempK 0.94159E+02 2 0.15043E-05 0.42150E+02 0.72565E+00 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -4.5812e-14 2.707e-14 -1.4019e-17 -3.3534e-18 v Velocity[Y] -3.8521e-05 3.8834e-05 -9.4569e-12 -5.1708e-12 v Velocity[Z] -3.8833e-05 3.852e-05 5.1355e-12 8.6917e-13 v ǁVelocityǁ 9.6379e-12 4.5545e-05 1.3639e-06 5.2785e-07 v Pressure -1.5672e-05 0.0017845 3.7838e-05 5.1248e-21 v k 5.1073e-07 0.013726 0.0080209 0.0084599 v omega 85.095 1.0365e+05 2775.6 571.99 v TempK 288 333.23 289.1 288.29 v Density 1.205 1.205 1.205 1.205 v TurbVisc 4.1544e-12 0.00019524 0.00011044 0.00011889 v CourantNb 2.3263e-11 5.3685e-05 2.4304e-06 9.3172e-07 v FourierNb 0.15477 1.3086 0.40734 0.28915 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.0089 4.009 9.1051e-05 3.4069e-08 v volume_forces[Z] -4.0089 4.009 -9.1043e-05 -3.1007e-08 v ǁvolume_forcesǁ 3.3471e-10 4.0104 0.092943 0.024857 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 289.28 288.43 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015367 5.2308e-05 2.9985e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.15477 1.3086 0.40735 0.28916 INSTANT 0.674100000E-02 TIME STEP NUMBER 7 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12644E-06 0.25405E-02 Friction velocity uk : 0.84232E-05 0.25394E-02 Dimensionless distance yplus : 0.56089E-04 0.16895E-01 Friction thermal sca. tstar : -0.83742E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.39393E-04 0.11866E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12644E-06 0.25405E-02 Friction velocity uk : 0.84232E-05 0.25394E-02 Dimensionless distance yplus : 0.56089E-04 0.16895E-01 Friction thermal sca. tstar : -0.83742E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.39393E-04 0.11866E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60142E-09 8 0.22266E-03 0.39766E-09 0.20855E+03 c Velocity[X] 0.34980E-27 c Velocity[Y] 0.19883E-09 c Velocity[Z] 0.19883E-09 c Pressure 0.22008E-11 29 0.83703E-07 0.22405E-04 0.92927E+02 c k 0.27706E-05 4 0.17682E-05 0.61635E-05 0.92747E+01 c omega 0.13217E+02 2 0.28834E-06 0.70880E+07 0.13837E+02 c TempK 0.94162E+02 2 0.13032E-05 0.30697E+02 0.61922E+00 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -6.079e-14 3.5998e-14 -1.8356e-17 -4.4025e-18 v Velocity[Y] -4.841e-05 4.8865e-05 -1.1843e-11 -6.5976e-12 v Velocity[Z] -4.8864e-05 4.8408e-05 6.3955e-12 1.1835e-12 v ǁVelocityǁ 1.2016e-11 5.7426e-05 1.6996e-06 6.5996e-07 v Pressure -1.7033e-05 0.0019531 4.1325e-05 -1.6853e-22 v k 5.9129e-07 0.013537 0.0079553 0.0083943 v omega 84.526 1.0317e+05 2730.3 562.84 v TempK 288 334.23 289.17 288.31 v Density 1.205 1.205 1.205 1.205 v TurbVisc 5.9376e-12 0.00019375 0.00010984 0.00011859 v CourantNb 2.7937e-11 6.5032e-05 2.9768e-06 1.1478e-06 v FourierNb 0.15471 1.2859 0.40227 0.28719 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.1443 4.1444 9.8443e-05 3.3199e-08 v volume_forces[Z] -4.1443 4.1444 -9.8433e-05 -2.9756e-08 v ǁvolume_forcesǁ 3.4841e-10 4.146 0.1005 0.026934 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 289.36 288.45 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.016895 5.7527e-05 3.2969e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.15471 1.2859 0.40227 0.28719 INSTANT 0.770400000E-02 TIME STEP NUMBER 8 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.17883E-06 0.27133E-02 Friction velocity uk : 0.95199E-05 0.27121E-02 Dimensionless distance yplus : 0.63392E-04 0.18044E-01 Friction thermal sca. tstar : -0.70431E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.44522E-04 0.12673E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.17883E-06 0.27133E-02 Friction velocity uk : 0.95199E-05 0.27121E-02 Dimensionless distance yplus : 0.63392E-04 0.18044E-01 Friction thermal sca. tstar : -0.70431E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.44522E-04 0.12673E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.70946E-09 8 0.15099E-03 0.40176E-09 0.17557E+03 c Velocity[X] 0.40055E-27 c Velocity[Y] 0.20088E-09 c Velocity[Z] 0.20088E-09 c Pressure 0.17981E-11 31 0.73284E-07 0.17691E-04 0.82272E+02 c k 0.27493E-05 3 0.27623E-05 0.57779E-05 0.90527E+01 c omega 0.13158E+02 2 0.11264E-06 0.90445E+06 0.49481E+01 c TempK 0.94163E+02 2 0.11396E-05 0.23662E+02 0.54362E+00 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -7.5737e-14 4.5609e-14 -2.2315e-17 -5.3669e-18 v Velocity[Y] -5.7732e-05 5.8321e-05 -1.2799e-11 -6.6479e-12 v Velocity[Z] -5.832e-05 5.773e-05 7.2969e-12 1.1012e-12 v ǁVelocityǁ 7.747e-12 6.8656e-05 2.037e-06 7.9428e-07 v Pressure -1.8388e-05 0.0021073 4.4763e-05 4.0186e-21 v k 6.2494e-07 0.013351 0.0078901 0.0083295 v omega 83.964 1.0313e+05 2715.5 559.54 v TempK 288 334.96 289.24 288.33 v Density 1.205 1.205 1.205 1.205 v TurbVisc 6.9062e-12 0.00019224 0.00010925 0.00011829 v CourantNb 3.0762e-11 7.6266e-05 3.5195e-06 1.3652e-06 v FourierNb 0.15464 1.267 0.39753 0.28532 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.2358 4.2359 0.00010491 3.2461e-08 v volume_forces[Z] -4.2358 4.2359 -0.0001049 -2.8605e-08 v ǁvolume_forcesǁ 4.3439e-10 4.2376 0.1071 0.028796 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 289.43 288.47 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.018044 6.1444e-05 3.521e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.15464 1.267 0.39753 0.28532 INSTANT 0.866700000E-02 TIME STEP NUMBER 9 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.31132E-07 0.28496E-02 Friction velocity uk : 0.99563E-05 0.28483E-02 Dimensionless distance yplus : 0.66298E-04 0.18950E-01 Friction thermal sca. tstar : -0.62104E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.46563E-04 0.13309E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.31132E-07 0.28496E-02 Friction velocity uk : 0.99563E-05 0.28483E-02 Dimensionless distance yplus : 0.66298E-04 0.18950E-01 Friction thermal sca. tstar : -0.62104E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.46563E-04 0.13309E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.81711E-09 8 0.11005E-03 0.40176E-09 0.15112E+03 c Velocity[X] 0.40487E-27 c Velocity[Y] 0.20088E-09 c Velocity[Z] 0.20088E-09 c Pressure 0.15405E-11 29 0.75997E-07 0.14782E-04 0.73973E+02 c k 0.27284E-05 3 0.24984E-05 0.54671E-05 0.88766E+01 c omega 0.13154E+02 2 0.62888E-07 0.19572E+06 0.23025E+01 c TempK 0.94165E+02 2 0.10066E-05 0.18963E+02 0.48662E+00 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.014e-14 5.5177e-14 -2.5746e-17 -6.2087e-18 v Velocity[Y] -6.6413e-05 6.7125e-05 -1.3521e-11 -6.3379e-12 v Velocity[Z] -6.7123e-05 6.6411e-05 8.1941e-12 9.6652e-13 v ǁVelocityǁ 6.2687e-12 7.9135e-05 2.3746e-06 9.3019e-07 v Pressure -1.9744e-05 0.0022502 4.8159e-05 -5.1248e-21 v k 6.3536e-07 0.013169 0.0078253 0.0082654 v omega 83.409 1.0313e+05 2709.4 557.96 v TempK 288 335.52 289.29 288.35 v Density 1.205 1.205 1.205 1.205 v TurbVisc 7.3017e-12 0.00019074 0.00010868 0.000118 v CourantNb 3.507e-11 8.8076e-05 4.0585e-06 1.5834e-06 v FourierNb 0.15458 1.2465 0.39307 0.28352 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.3025 4.3026 0.00011071 3.1763e-08 v volume_forces[Z] -4.3025 4.3026 -0.0001107 -2.7601e-08 v ǁvolume_forcesǁ 2.8005e-10 4.3043 0.11303 0.030502 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 289.5 288.49 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.01895 6.4526e-05 3.6975e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.15458 1.2465 0.39307 0.28352 INSTANT 0.963000000E-02 TIME STEP NUMBER 10 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19610E-07 0.29612E-02 Friction velocity uk : 0.10103E-04 0.29598E-02 Dimensionless distance yplus : 0.67282E-04 0.19692E-01 Friction thermal sca. tstar : -0.56190E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.47255E-04 0.13830E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19610E-07 0.29612E-02 Friction velocity uk : 0.10103E-04 0.29598E-02 Dimensionless distance yplus : 0.67282E-04 0.19692E-01 Friction thermal sca. tstar : -0.56190E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.47255E-04 0.13830E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.92433E-09 8 0.84594E-04 0.39875E-09 0.13228E+03 c Velocity[X] 0.38129E-27 c Velocity[Y] 0.19937E-09 c Velocity[Z] 0.19937E-09 c Pressure 0.13671E-11 30 0.79623E-07 0.12868E-04 0.67306E+02 c k 0.27078E-05 3 0.22694E-05 0.52105E-05 0.87350E+01 c omega 0.13153E+02 2 0.41763E-07 0.58090E+05 0.12546E+01 c TempK 0.94167E+02 2 0.89783E-06 0.15634E+02 0.44183E+00 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.0375e-13 6.4467e-14 -2.8637e-17 -6.9237e-18 v Velocity[Y] -7.4456e-05 7.5277e-05 -1.5003e-11 -6.671e-12 v Velocity[Z] -7.5275e-05 7.4455e-05 9.4362e-12 1.1097e-12 v ǁVelocityǁ 6.8059e-12 8.8861e-05 2.7116e-06 1.0673e-06 v Pressure -2.1116e-05 0.002384 5.1518e-05 2.4222e-21 v k 6.3415e-07 0.012991 0.0077609 0.0082021 v omega 82.862 1.0313e+05 2706.5 557.04 v TempK 288 335.97 289.35 288.37 v Density 1.205 1.205 1.205 1.205 v TurbVisc 7.4237e-12 0.00018925 0.00010812 0.00011772 v CourantNb 3.9317e-11 9.9628e-05 4.595e-06 1.8027e-06 v FourierNb 0.15451 1.2248 0.38887 0.28179 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.3539 4.3539 0.000116 3.111e-08 v volume_forces[Z] -4.3539 4.3539 -0.00011599 -2.6687e-08 v ǁvolume_forcesǁ 2.2661e-10 4.3558 0.11843 0.032087 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 289.55 288.51 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.019692 6.7044e-05 3.8419e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.15451 1.2248 0.38888 0.2818 INSTANT 0.105930000E-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 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.35504E-07 0.30554E-02 Friction velocity uk : 0.10119E-04 0.30540E-02 Dimensionless distance yplus : 0.67390E-04 0.20318E-01 Friction thermal sca. tstar : -0.51763E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.47331E-04 0.14270E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.35504E-07 0.30554E-02 Friction velocity uk : 0.10119E-04 0.30540E-02 Dimensionless distance yplus : 0.67390E-04 0.20318E-01 Friction thermal sca. tstar : -0.51763E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.47331E-04 0.14270E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.10310E-08 8 0.67619E-04 0.39353E-09 0.11731E+03 c Velocity[X] 0.34476E-27 c Velocity[Y] 0.19677E-09 c Velocity[Z] 0.19677E-09 c Pressure 0.12449E-11 30 0.81912E-07 0.11540E-04 0.61823E+02 c k 0.26874E-05 3 0.20695E-05 0.49947E-05 0.86200E+01 c omega 0.13153E+02 2 0.30826E-07 0.21290E+05 0.75953E+00 c TempK 0.94168E+02 2 0.80790E-06 0.13174E+02 0.40556E+00 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.165e-13 7.3342e-14 -3.1033e-17 -7.5205e-18 v Velocity[Y] -8.1901e-05 8.2816e-05 -1.6779e-11 -7.2344e-12 v Velocity[Z] -8.2814e-05 8.19e-05 1.0526e-11 1.0239e-12 v ǁVelocityǁ 1.4175e-11 9.7874e-05 3.0471e-06 1.2052e-06 v Pressure -2.2488e-05 0.0025104 5.4846e-05 -1.7726e-21 v k 6.2706e-07 0.012819 0.0076968 0.0081395 v omega 82.321 1.0313e+05 2705.1 556.43 v TempK 288 336.34 289.4 288.38 v Density 1.205 1.205 1.205 1.205 v TurbVisc 7.4096e-12 0.00018778 0.00010759 0.00011744 v CourantNb 4.3362e-11 0.00011086 5.1274e-06 2.0223e-06 v FourierNb 0.15445 1.2022 0.3849 0.28014 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.3951 4.3951 0.00012089 3.0507e-08 v volume_forces[Z] -4.3951 4.3951 -0.00012087 -2.581e-08 v ǁvolume_forcesǁ 2.4603e-10 4.3971 0.12342 0.033576 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 289.61 288.52 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.020318 6.9164e-05 3.9634e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.15445 1.2022 0.38491 0.28014 INSTANT 0.115560000E-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 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.18527E-06 0.31365E-02 Friction velocity uk : 0.10131E-04 0.31350E-02 Dimensionless distance yplus : 0.67468E-04 0.20857E-01 Friction thermal sca. tstar : -0.48326E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.47386E-04 0.14649E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.18527E-06 0.31365E-02 Friction velocity uk : 0.10131E-04 0.31350E-02 Dimensionless distance yplus : 0.67468E-04 0.20857E-01 Friction thermal sca. tstar : -0.48326E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.47386E-04 0.14649E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.11370E-08 8 0.55651E-04 0.38670E-09 0.10514E+03 c Velocity[X] 0.30456E-27 c Velocity[Y] 0.19335E-09 c Velocity[Z] 0.19335E-09 c Pressure 0.11554E-11 30 0.82890E-07 0.10577E-04 0.57227E+02 c k 0.26674E-05 3 0.18940E-05 0.48094E-05 0.85252E+01 c omega 0.13153E+02 1 0.86147E-06 0.90307E+04 0.49469E+00 c TempK 0.94170E+02 2 0.73277E-06 0.11295E+02 0.37549E+00 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.2829e-13 8.1735e-14 -3.2996e-17 -8.0128e-18 v Velocity[Y] -8.8795e-05 8.979e-05 -1.7668e-11 -6.854e-12 v Velocity[Z] -8.9788e-05 8.8795e-05 1.1571e-11 8.0665e-13 v ǁVelocityǁ 1.4091e-11 0.00010623 3.38e-06 1.3434e-06 v Pressure -2.3863e-05 0.0026305 5.8145e-05 -4.4859e-21 v k 6.1694e-07 0.012651 0.0076331 0.0080776 v omega 81.791 1.0313e+05 2704.4 555.97 v TempK 288 336.66 289.45 288.4 v Density 1.205 1.205 1.205 1.205 v TurbVisc 7.3267e-12 0.00018635 0.00010707 0.00011716 v CourantNb 4.7319e-11 0.00012173 5.6537e-06 2.2414e-06 v FourierNb 0.15438 1.179 0.38115 0.27855 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.4291 4.4292 0.00012544 2.9931e-08 v volume_forces[Z] -4.4291 4.4292 -0.00012542 -2.4975e-08 v ǁvolume_forcesǁ 5.1241e-10 4.4312 0.12806 0.034985 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 289.66 288.54 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.020857 7.0986e-05 4.0678e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.15438 1.179 0.38115 0.27856 INSTANT 0.125190000E-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 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.16896E-06 0.32073E-02 Friction velocity uk : 0.10064E-04 0.32058E-02 Dimensionless distance yplus : 0.67015E-04 0.21328E-01 Friction thermal sca. tstar : -0.45589E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.47067E-04 0.14980E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.16896E-06 0.32073E-02 Friction velocity uk : 0.10064E-04 0.32058E-02 Dimensionless distance yplus : 0.67015E-04 0.21328E-01 Friction thermal sca. tstar : -0.45589E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.47067E-04 0.14980E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.12422E-08 7 0.46867E-04 0.37864E-09 0.95046E+02 c Velocity[X] 0.26557E-27 c Velocity[Y] 0.18932E-09 c Velocity[Z] 0.18932E-09 c Pressure 0.10884E-11 27 0.82842E-07 0.98605E-05 0.53314E+02 c k 0.26477E-05 3 0.17409E-05 0.46471E-05 0.84458E+01 c omega 0.13153E+02 1 0.66749E-06 0.47380E+04 0.35833E+00 c TempK 0.94171E+02 2 0.66943E-06 0.98200E+01 0.35011E+00 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.3915e-13 8.9624e-14 -3.4589e-17 -8.415e-18 v Velocity[Y] -9.5189e-05 9.625e-05 -1.8769e-11 -6.591e-12 v Velocity[Z] -9.625e-05 9.5189e-05 1.2862e-11 7.4863e-13 v ǁVelocityǁ 1.2516e-11 0.00011399 3.7095e-06 1.4816e-06 v Pressure -2.524e-05 0.0027453 6.1419e-05 -5.8066e-21 v k 6.0528e-07 0.012488 0.0075699 0.0080165 v omega 81.267 1.0313e+05 2704.1 555.6 v TempK 288 336.93 289.49 288.41 v Density 1.205 1.205 1.205 1.205 v TurbVisc 7.2088e-12 0.00018491 0.00010657 0.00011689 v CourantNb 5.1281e-11 0.00013222 6.1728e-06 2.4595e-06 v FourierNb 0.15432 1.1564 0.37765 0.27705 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.4578 4.4579 0.0001297 2.938e-08 v volume_forces[Z] -4.4578 4.4579 -0.00012969 -2.4214e-08 v ǁvolume_forcesǁ 5.0938e-10 4.46 0.13242 0.036326 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 289.71 288.55 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.021328 7.2578e-05 4.159e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.15432 1.1564 0.37766 0.27705 INSTANT 0.134820000E-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 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.13810E-06 0.32699E-02 Friction velocity uk : 0.99261E-05 0.32684E-02 Dimensionless distance yplus : 0.66097E-04 0.21745E-01 Friction thermal sca. tstar : -0.43369E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.46422E-04 0.15272E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.13810E-06 0.32699E-02 Friction velocity uk : 0.99261E-05 0.32684E-02 Dimensionless distance yplus : 0.66097E-04 0.21745E-01 Friction thermal sca. tstar : -0.43369E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.46422E-04 0.15272E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.13464E-08 7 0.40126E-04 0.36972E-09 0.86551E+02 c Velocity[X] 0.22998E-27 c Velocity[Y] 0.18486E-09 c Velocity[Z] 0.18486E-09 c Pressure 0.10349E-11 27 0.82140E-07 0.92926E-05 0.49938E+02 c k 0.26282E-05 3 0.16050E-05 0.45019E-05 0.83776E+01 c omega 0.13153E+02 1 0.54952E-06 0.29052E+04 0.28059E+00 c TempK 0.94172E+02 2 0.61544E-06 0.86383E+01 0.32835E+00 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.4913e-13 9.7013e-14 -3.5872e-17 -8.7411e-18 v Velocity[Y] -0.00010127 0.00010225 -1.9895e-11 -6.2667e-12 v Velocity[Z] -0.00010225 0.00010127 1.4237e-11 6.8404e-13 v ǁVelocityǁ 1.1427e-11 0.0001212 4.035e-06 1.6193e-06 v Pressure -2.6621e-05 0.0028553 6.467e-05 6.0793e-21 v k 5.9284e-07 0.012331 0.0075071 0.007956 v omega 80.749 1.0313e+05 2704 555.27 v TempK 288 337.16 289.54 288.43 v Density 1.205 1.205 1.205 1.205 v TurbVisc 7.0729e-12 0.00018351 0.00010608 0.00011663 v CourantNb 5.5225e-11 0.00014231 6.684e-06 2.6761e-06 v FourierNb 0.15425 1.1337 0.37432 0.2756 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.4826 4.4826 0.00013373 2.8859e-08 v volume_forces[Z] -4.4826 4.4826 -0.00013372 -2.3482e-08 v ǁvolume_forcesǁ 4.5244e-10 4.4847 0.13653 0.03761 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 289.75 288.57 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.021745 7.3984e-05 4.2396e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.15425 1.1337 0.37433 0.2756 INSTANT 0.144450000E-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 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11253E-06 0.33258E-02 Friction velocity uk : 0.97785E-05 0.33243E-02 Dimensionless distance yplus : 0.65114E-04 0.22117E-01 Friction thermal sca. tstar : -0.41545E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.45732E-04 0.15533E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11253E-06 0.33258E-02 Friction velocity uk : 0.97785E-05 0.33243E-02 Dimensionless distance yplus : 0.65114E-04 0.22117E-01 Friction thermal sca. tstar : -0.41545E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.45732E-04 0.15533E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.14496E-08 7 0.34808E-04 0.36021E-09 0.79306E+02 c Velocity[X] 0.19855E-27 c Velocity[Y] 0.18010E-09 c Velocity[Z] 0.18010E-09 c Pressure 0.99072E-12 30 0.80940E-07 0.88284E-05 0.46995E+02 c k 0.26090E-05 3 0.14837E-05 0.43698E-05 0.83176E+01 c omega 0.13153E+02 1 0.47186E-06 0.20270E+04 0.23438E+00 c TempK 0.94174E+02 2 0.56900E-06 0.76745E+01 0.30948E+00 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.5829e-13 1.0392e-13 -3.6896e-17 -9.0034e-18 v Velocity[Y] -0.00010694 0.00010783 -2.1142e-11 -5.9719e-12 v Velocity[Z] -0.00010783 0.00010694 1.5718e-11 6.3288e-13 v ǁVelocityǁ 1.0658e-11 0.00012792 4.3559e-06 1.7564e-06 v Pressure -2.802e-05 0.0029612 6.79e-05 1.1904e-20 v k 5.8005e-07 0.012178 0.0074448 0.0078963 v omega 80.239 1.0313e+05 2704.1 554.97 v TempK 288 337.37 289.58 288.44 v Density 1.205 1.205 1.205 1.205 v TurbVisc 6.9278e-12 0.00018213 0.00010561 0.00011636 v CourantNb 5.9123e-11 0.000152 7.1867e-06 2.891e-06 v FourierNb 0.15418 1.1111 0.37113 0.2742 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.5041 4.5042 0.00013755 2.8359e-08 v volume_forces[Z] -4.5041 4.5042 -0.00013753 -2.2779e-08 v ǁvolume_forcesǁ 4.1309e-10 4.5063 0.14042 0.038843 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 289.79 288.58 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.022117 7.5238e-05 4.3115e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.15418 1.1111 0.37114 0.2742 INSTANT 0.154080000E-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 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.89197E-07 0.33761E-02 Friction velocity uk : 0.96247E-05 0.33745E-02 Dimensionless distance yplus : 0.64090E-04 0.22451E-01 Friction thermal sca. tstar : -0.40035E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.45013E-04 0.15768E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.89197E-07 0.33761E-02 Friction velocity uk : 0.96247E-05 0.33745E-02 Dimensionless distance yplus : 0.64090E-04 0.22451E-01 Friction thermal sca. tstar : -0.40035E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.45013E-04 0.15768E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.15516E-08 7 0.30516E-04 0.35029E-09 0.73055E+02 c Velocity[X] 0.17130E-27 c Velocity[Y] 0.17514E-09 c Velocity[Z] 0.17514E-09 c Pressure 0.95327E-12 29 0.79415E-07 0.84381E-05 0.44402E+02 c k 0.25900E-05 3 0.13752E-05 0.42477E-05 0.82637E+01 c omega 0.13153E+02 1 0.41629E-06 0.15532E+04 0.20516E+00 c TempK 0.94175E+02 2 0.52870E-06 0.68765E+01 0.29293E+00 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.667e-13 1.1038e-13 -3.7708e-17 -9.2127e-18 v Velocity[Y] -0.00011223 0.00011303 -2.2518e-11 -5.716e-12 v Velocity[Z] -0.00011303 0.00011223 1.7293e-11 5.8863e-13 v ǁVelocityǁ 1.0132e-11 0.0001342 4.672e-06 1.8927e-06 v Pressure -2.9424e-05 0.0030634 7.111e-05 -5.7177e-21 v k 5.6715e-07 0.012036 0.007383 0.0078372 v omega 79.734 1.0313e+05 2704.1 554.68 v TempK 288 337.55 289.61 288.45 v Density 1.205 1.205 1.205 1.205 v TurbVisc 6.7787e-12 0.00018102 0.00010515 0.00011611 v CourantNb 6.2998e-11 0.00016129 7.6807e-06 3.1039e-06 v FourierNb 0.15412 1.0889 0.36808 0.27285 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.5231 4.5232 0.00014118 2.7878e-08 v volume_forces[Z] -4.5231 4.5232 -0.00014117 -2.21e-08 v ǁvolume_forcesǁ 3.8528e-10 4.5254 0.14413 0.040031 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 289.83 288.59 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.022451 7.6365e-05 4.376e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.15412 1.0889 0.36809 0.27285 INSTANT 0.163710000E-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 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.66185E-07 0.34215E-02 Friction velocity uk : 0.94666E-05 0.34199E-02 Dimensionless distance yplus : 0.63037E-04 0.22753E-01 Friction thermal sca. tstar : -0.38779E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.44273E-04 0.15980E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.66185E-07 0.34215E-02 Friction velocity uk : 0.94666E-05 0.34199E-02 Dimensionless distance yplus : 0.63037E-04 0.22753E-01 Friction thermal sca. tstar : -0.38779E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.44273E-04 0.15980E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.16525E-08 7 0.26996E-04 0.34011E-09 0.67611E+02 c Velocity[X] 0.14790E-27 c Velocity[Y] 0.17005E-09 c Velocity[Z] 0.17005E-09 c Pressure 0.92061E-12 29 0.77677E-07 0.81012E-05 0.42101E+02 c k 0.25713E-05 3 0.12776E-05 0.41335E-05 0.82143E+01 c omega 0.13153E+02 1 0.37348E-06 0.12654E+04 0.18519E+00 c TempK 0.94176E+02 2 0.49344E-06 0.62072E+01 0.27830E+00 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.7444e-13 1.1642e-13 -3.8345e-17 -9.3783e-18 v Velocity[Y] -0.00011717 0.00011787 -2.4017e-11 -5.4958e-12 v Velocity[Z] -0.00011788 0.00011717 1.8886e-11 4.7808e-13 v ǁVelocityǁ 9.8668e-12 0.00014008 4.9828e-06 2.0278e-06 v Pressure -3.0834e-05 0.0031623 7.4302e-05 6.6492e-22 v k 5.5427e-07 0.011906 0.0073218 0.0077789 v omega 79.236 1.0313e+05 2704.2 554.4 v TempK 288 337.72 289.65 288.46 v Density 1.205 1.205 1.205 1.205 v TurbVisc 6.6281e-12 0.00018003 0.0001047 0.00011586 v CourantNb 6.6818e-11 0.00017019 8.1653e-06 3.3144e-06 v FourierNb 0.15406 1.067 0.36516 0.27154 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.5401 4.5401 0.00014465 2.7414e-08 v volume_forces[Z] -4.5401 4.5401 -0.00014464 -2.144e-08 v ǁvolume_forcesǁ 3.6628e-10 4.5424 0.14767 0.04118 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 289.87 288.6 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.022753 7.7384e-05 4.4343e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.15406 1.067 0.36517 0.27154 INSTANT 0.173340000E-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 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.44031E-07 0.34627E-02 Friction velocity uk : 0.93064E-05 0.34612E-02 Dimensionless distance yplus : 0.61970E-04 0.23027E-01 Friction thermal sca. tstar : -0.37732E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.43524E-04 0.16173E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.44031E-07 0.34627E-02 Friction velocity uk : 0.93064E-05 0.34612E-02 Dimensionless distance yplus : 0.61970E-04 0.23027E-01 Friction thermal sca. tstar : -0.37732E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.43524E-04 0.16173E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.17521E-08 7 0.24048E-04 0.32979E-09 0.62826E+02 c Velocity[X] 0.12789E-27 c Velocity[Y] 0.16489E-09 c Velocity[Z] 0.16489E-09 c Pressure 0.89131E-12 28 0.76286E-07 0.78024E-05 0.40041E+02 c k 0.25529E-05 3 0.11896E-05 0.40257E-05 0.81682E+01 c omega 0.13153E+02 1 0.33860E-06 0.10710E+04 0.17037E+00 c TempK 0.94178E+02 2 0.46237E-06 0.56396E+01 0.26526E+00 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.8156e-13 1.2208e-13 -3.8838e-17 -9.5074e-18 v Velocity[Y] -0.0001218 0.0001224 -2.5613e-11 -5.2854e-12 v Velocity[Z] -0.0001224 0.0001218 2.0654e-11 4.5284e-13 v ǁVelocityǁ 9.8269e-12 0.00014558 5.2882e-06 2.1618e-06 v Pressure -3.2249e-05 0.0032583 7.7477e-05 6.974e-21 v k 5.4147e-07 0.011779 0.0072611 0.0077212 v omega 78.745 1.0313e+05 2704.3 554.13 v TempK 288 337.87 289.69 288.47 v Density 1.205 1.205 1.205 1.205 v TurbVisc 6.4777e-12 0.00017905 0.00010427 0.00011561 v CourantNb 7.0691e-11 0.00017871 8.6405e-06 3.5225e-06 v FourierNb 0.15399 1.0502 0.36236 0.27027 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.5553 4.5554 0.00014798 2.6962e-08 v volume_forces[Z] -4.5553 4.5554 -0.00014796 -2.0799e-08 v ǁvolume_forcesǁ 3.5668e-10 4.5576 0.15106 0.042293 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 289.91 288.62 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.023027 7.8308e-05 4.4872e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.15399 1.0502 0.36236 0.27028 INSTANT 0.182970000E-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 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.21728E-07 0.35004E-02 Friction velocity uk : 0.91446E-05 0.34988E-02 Dimensionless distance yplus : 0.60893E-04 0.23278E-01 Friction thermal sca. tstar : -0.36862E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.42767E-04 0.16349E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.21728E-07 0.35004E-02 Friction velocity uk : 0.91446E-05 0.34988E-02 Dimensionless distance yplus : 0.60893E-04 0.23278E-01 Friction thermal sca. tstar : -0.36862E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.42767E-04 0.16349E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.18503E-08 7 0.21557E-04 0.31941E-09 0.58591E+02 c Velocity[X] 0.11081E-27 c Velocity[Y] 0.15971E-09 c Velocity[Z] 0.15971E-09 c Pressure 0.86466E-12 27 0.74803E-07 0.75337E-05 0.38187E+02 c k 0.25347E-05 3 0.11102E-05 0.39230E-05 0.81244E+01 c omega 0.13153E+02 1 0.30905E-06 0.92800E+03 0.15859E+00 c TempK 0.94179E+02 2 0.43478E-06 0.51535E+01 0.25356E+00 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.8813e-13 1.2737e-13 -3.9211e-17 -9.6064e-18 v Velocity[Y] -0.00012614 0.00012664 -2.8292e-11 -6.0456e-12 v Velocity[Z] -0.00012664 0.00012614 2.0926e-11 -1.1061e-12 v ǁVelocityǁ 9.9528e-12 0.00015074 5.5883e-06 2.2946e-06 v Pressure -3.367e-05 0.0033515 8.0636e-05 1.0348e-20 v k 5.288e-07 0.011654 0.007201 0.0076642 v omega 78.259 1.0313e+05 2704.4 553.85 v TempK 288 338.01 289.72 288.49 v Density 1.205 1.205 1.205 1.205 v TurbVisc 6.3283e-12 0.00017807 0.00010385 0.00011537 v CourantNb 7.4463e-11 0.00018686 9.1063e-06 3.7281e-06 v FourierNb 0.15393 1.0341 0.35966 0.26905 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.5691 4.5691 0.00015117 2.6526e-08 v volume_forces[Z] -4.5691 4.5691 -0.00015116 -2.0175e-08 v ǁvolume_forcesǁ 3.5524e-10 4.5714 0.15431 0.043374 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 289.94 288.63 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.023278 7.915e-05 4.5354e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.15393 1.0341 0.35967 0.26905 INSTANT 0.192600000E-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 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.16704E-07 0.35348E-02 Friction velocity uk : 0.89905E-05 0.35332E-02 Dimensionless distance yplus : 0.59867E-04 0.23507E-01 Friction thermal sca. tstar : -0.36144E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.42047E-04 0.16510E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.16704E-07 0.35348E-02 Friction velocity uk : 0.89905E-05 0.35332E-02 Dimensionless distance yplus : 0.59867E-04 0.23507E-01 Friction thermal sca. tstar : -0.36144E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.42047E-04 0.16510E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.19472E-08 7 0.19429E-04 0.30906E-09 0.54816E+02 c Velocity[X] 0.96236E-28 c Velocity[Y] 0.15453E-09 c Velocity[Z] 0.15453E-09 c Pressure 0.83984E-12 27 0.72767E-07 0.72865E-05 0.36508E+02 c k 0.25167E-05 3 0.10381E-05 0.38246E-05 0.80823E+01 c omega 0.13153E+02 1 0.28338E-06 0.81610E+03 0.14872E+00 c TempK 0.94180E+02 2 0.41012E-06 0.47334E+01 0.24299E+00 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.9419e-13 1.3234e-13 -3.9486e-17 -9.6805e-18 v Velocity[Y] -0.00013021 0.0001306 -3.0057e-11 -5.8357e-12 v Velocity[Z] -0.00013061 0.00013021 2.2943e-11 -1.0726e-12 v ǁVelocityǁ 1.0346e-11 0.00015559 5.8831e-06 2.4261e-06 v Pressure -3.5094e-05 0.0034423 8.3779e-05 3.4625e-21 v k 5.1628e-07 0.011531 0.0071416 0.0076079 v omega 77.779 1.0313e+05 2704.5 553.58 v TempK 288 338.13 289.76 288.5 v Density 1.205 1.205 1.205 1.205 v TurbVisc 6.1803e-12 0.0001771 0.00010344 0.00011513 v CourantNb 7.8152e-11 0.00019573 9.5637e-06 3.9313e-06 v FourierNb 0.15387 1.0183 0.35707 0.26786 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.5816 4.5816 0.00015425 2.6047e-08 v volume_forces[Z] -4.5816 4.5816 -0.00015423 -1.9533e-08 v ǁvolume_forcesǁ 3.5979e-10 4.584 0.15745 0.044425 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 289.98 288.64 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.023507 7.9921e-05 4.5795e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.15387 1.0183 0.35708 0.26786 INSTANT 0.202230000E-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 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.29774E-07 0.35664E-02 Friction velocity uk : 0.88452E-05 0.35648E-02 Dimensionless distance yplus : 0.58899E-04 0.23717E-01 Friction thermal sca. tstar : -0.35559E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.41367E-04 0.16657E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.29774E-07 0.35664E-02 Friction velocity uk : 0.88452E-05 0.35648E-02 Dimensionless distance yplus : 0.58899E-04 0.23717E-01 Friction thermal sca. tstar : -0.35559E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.41367E-04 0.16657E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.20427E-08 7 0.17598E-04 0.29877E-09 0.51430E+02 c Velocity[X] 0.83774E-28 c Velocity[Y] 0.14939E-09 c Velocity[Z] 0.14939E-09 c Pressure 0.81669E-12 27 0.70735E-07 0.70586E-05 0.34980E+02 c k 0.24990E-05 3 0.97274E-06 0.37298E-05 0.80413E+01 c omega 0.13153E+02 1 0.26070E-06 0.72488E+03 0.14016E+00 c TempK 0.94181E+02 2 0.38795E-06 0.43677E+01 0.23341E+00 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.9979e-13 1.37e-13 -3.9678e-17 -9.7335e-18 v Velocity[Y] -0.0001341 0.00013462 -3.1918e-11 -5.6276e-12 v Velocity[Z] -0.00013462 0.0001341 2.5049e-11 -1.0376e-12 v ǁVelocityǁ 9.6523e-12 0.00016061 6.173e-06 2.5564e-06 v Pressure -3.6534e-05 0.0035308 8.6908e-05 3.2511e-21 v k 5.0395e-07 0.011411 0.0070827 0.0075522 v omega 77.305 1.0313e+05 2704.6 553.3 v TempK 288 338.25 289.79 288.51 v Density 1.205 1.205 1.205 1.205 v TurbVisc 6.0342e-12 0.00017613 0.00010303 0.00011489 v CourantNb 8.1988e-11 0.00020475 1.0013e-05 4.1324e-06 v FourierNb 0.15381 1.0026 0.35458 0.26671 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.5931 4.5931 0.00015721 2.5637e-08 v volume_forces[Z] -4.5931 4.5931 -0.0001572 -1.8942e-08 v ǁvolume_forcesǁ 3.7399e-10 4.5955 0.16047 0.04545 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 290.01 288.65 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.023717 8.0627e-05 4.6199e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.15381 1.0026 0.35459 0.26671 INSTANT 0.211860000E-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 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.57271E-07 0.35954E-02 Friction velocity uk : 0.86827E-05 0.35938E-02 Dimensionless distance yplus : 0.57812E-04 0.23910E-01 Friction thermal sca. tstar : -0.35091E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.40603E-04 0.16793E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.57271E-07 0.35954E-02 Friction velocity uk : 0.86827E-05 0.35938E-02 Dimensionless distance yplus : 0.57812E-04 0.23910E-01 Friction thermal sca. tstar : -0.35091E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.40603E-04 0.16793E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.21368E-08 6 0.14390E-04 0.28862E-09 0.48379E+02 c Velocity[X] 0.73075E-28 c Velocity[Y] 0.14431E-09 c Velocity[Z] 0.14431E-09 c Pressure 0.79266E-12 30 0.68544E-07 0.68269E-05 0.33581E+02 c k 0.24815E-05 3 0.91324E-06 0.36382E-05 0.80011E+01 c omega 0.13153E+02 1 0.24046E-06 0.64854E+03 0.13257E+00 c TempK 0.94182E+02 2 0.36791E-06 0.40470E+01 0.22467E+00 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -2.0497e-13 1.4138e-13 -3.9802e-17 -9.7691e-18 v Velocity[Y] -0.0001395 0.00014003 -3.3878e-11 -5.4342e-12 v Velocity[Z] -0.00014003 0.0001395 2.7236e-11 -1.0039e-12 v ǁVelocityǁ 8.8167e-12 0.00016722 6.4581e-06 2.6854e-06 v Pressure -3.7982e-05 0.0036172 9.0022e-05 6.6186e-22 v k 4.9179e-07 0.011293 0.0070244 0.0074972 v omega 76.837 1.0313e+05 2704.7 553.02 v TempK 288 338.35 289.82 288.52 v Density 1.205 1.205 1.205 1.205 v TurbVisc 5.8901e-12 0.00017516 0.00010264 0.00011466 v CourantNb 8.5816e-11 0.00021349 1.0457e-05 4.3318e-06 v FourierNb 0.15375 0.98731 0.35217 0.26559 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.6037 4.6037 0.00016008 2.5237e-08 v volume_forces[Z] -4.6037 4.6037 -0.00016006 -1.8366e-08 v ǁvolume_forcesǁ 3.4893e-10 4.6061 0.16339 0.04645 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 290.04 288.66 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.02391 8.1275e-05 4.6569e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.15375 0.98731 0.35218 0.2656 INSTANT 0.221490000E-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 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.64276E-07 0.36221E-02 Friction velocity uk : 0.85094E-05 0.36206E-02 Dimensionless distance yplus : 0.56658E-04 0.24088E-01 Friction thermal sca. tstar : -0.34731E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.39793E-04 0.16918E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.64276E-07 0.36221E-02 Friction velocity uk : 0.85094E-05 0.36206E-02 Dimensionless distance yplus : 0.56658E-04 0.24088E-01 Friction thermal sca. tstar : -0.34731E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.39793E-04 0.16918E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.22295E-08 6 0.13158E-04 0.27860E-09 0.45614E+02 c Velocity[X] 0.63902E-28 c Velocity[Y] 0.13930E-09 c Velocity[Z] 0.13930E-09 c Pressure 0.77172E-12 27 0.66579E-07 0.66252E-05 0.32297E+02 c k 0.24642E-05 3 0.85900E-06 0.35495E-05 0.79615E+01 c omega 0.13153E+02 1 0.22227E-06 0.58357E+03 0.12576E+00 c TempK 0.94183E+02 2 0.34970E-06 0.37640E+01 0.21666E+00 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -2.0985e-13 1.4551e-13 -3.9869e-17 -9.7902e-18 v Velocity[Y] -0.00014465 0.00014519 -3.594e-11 -5.2597e-12 v Velocity[Z] -0.00014518 0.00014465 2.9513e-11 -9.6337e-13 v ǁVelocityǁ 8.7915e-12 0.00017353 6.7383e-06 2.8131e-06 v Pressure -3.9436e-05 0.0037017 9.3123e-05 -1.0014e-20 v k 4.7984e-07 0.011178 0.0069668 0.0074429 v omega 76.375 1.0313e+05 2704.8 552.74 v TempK 288 338.45 289.85 288.53 v Density 1.205 1.205 1.205 1.205 v TurbVisc 5.7481e-12 0.0001742 0.00010226 0.00011444 v CourantNb 8.9633e-11 0.00022194 1.0893e-05 4.5292e-06 v FourierNb 0.15369 0.97227 0.34985 0.26451 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.6134 4.6134 0.00016286 2.4848e-08 v volume_forces[Z] -4.6134 4.6134 -0.00016284 -1.7804e-08 v ǁvolume_forcesǁ 3.1872e-10 4.6158 0.16622 0.047427 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 290.07 288.67 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.024088 8.1872e-05 4.691e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.15369 0.97227 0.34986 0.26451 INSTANT 0.231120000E-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 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.21592E-07 0.36468E-02 Friction velocity uk : 0.83378E-05 0.36453E-02 Dimensionless distance yplus : 0.55515E-04 0.24252E-01 Friction thermal sca. tstar : -0.34470E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.38990E-04 0.17033E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.21592E-07 0.36468E-02 Friction velocity uk : 0.83378E-05 0.36453E-02 Dimensionless distance yplus : 0.55515E-04 0.24252E-01 Friction thermal sca. tstar : -0.34470E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.38990E-04 0.17033E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.23207E-08 6 0.12072E-04 0.26877E-09 0.43097E+02 c Velocity[X] 0.55993E-28 c Velocity[Y] 0.13438E-09 c Velocity[Z] 0.13438E-09 c Pressure 0.75157E-12 27 0.64643E-07 0.64332E-05 0.31112E+02 c k 0.24471E-05 3 0.80948E-06 0.34633E-05 0.79222E+01 c omega 0.13153E+02 1 0.20586E-06 0.52765E+03 0.11958E+00 c TempK 0.94184E+02 2 0.33307E-06 0.35129E+01 0.20930E+00 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -2.1448e-13 1.494e-13 -3.9889e-17 -9.799e-18 v Velocity[Y] -0.00014956 0.0001501 -3.8093e-11 -5.0937e-12 v Velocity[Z] -0.00015009 0.00014955 3.186e-11 -9.3239e-13 v ǁVelocityǁ 9.4458e-12 0.00017955 7.0134e-06 2.9394e-06 v Pressure -4.0895e-05 0.0037843 9.621e-05 -6.5236e-21 v k 4.6808e-07 0.011064 0.0069098 0.0073892 v omega 75.918 1.0313e+05 2704.8 552.46 v TempK 288 338.54 289.88 288.54 v Density 1.205 1.205 1.205 1.205 v TurbVisc 5.6085e-12 0.00017324 0.00010189 0.00011421 v CourantNb 9.3444e-11 0.00023011 1.1322e-05 4.7241e-06 v FourierNb 0.15363 0.95754 0.34761 0.26345 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.6225 4.6224 0.00016555 2.4468e-08 v volume_forces[Z] -4.6225 4.6224 -0.00016553 -1.7256e-08 v ǁvolume_forcesǁ 3.1781e-10 4.6249 0.16896 0.048383 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 290.1 288.68 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.024252 8.2422e-05 4.7224e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.15363 0.95754 0.34762 0.26346 INSTANT 0.240750000E-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 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.20881E-07 0.36696E-02 Friction velocity uk : 0.81881E-05 0.36681E-02 Dimensionless distance yplus : 0.54518E-04 0.24404E-01 Friction thermal sca. tstar : -0.34302E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.38290E-04 0.17140E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.20881E-07 0.36696E-02 Friction velocity uk : 0.81881E-05 0.36681E-02 Dimensionless distance yplus : 0.54518E-04 0.24404E-01 Friction thermal sca. tstar : -0.34302E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.38290E-04 0.17140E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.24104E-08 6 0.11114E-04 0.25913E-09 0.40797E+02 c Velocity[X] 0.49156E-28 c Velocity[Y] 0.12956E-09 c Velocity[Z] 0.12956E-09 c Pressure 0.73209E-12 27 0.62750E-07 0.62492E-05 0.30015E+02 c k 0.24302E-05 3 0.76419E-06 0.33794E-05 0.78831E+01 c omega 0.13153E+02 1 0.19100E-06 0.47918E+03 0.11396E+00 c TempK 0.94186E+02 2 0.31781E-06 0.32888E+01 0.20251E+00 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -2.1878e-13 1.5306e-13 -3.9869e-17 -9.7976e-18 v Velocity[Y] -0.00015423 0.00015477 -4.035e-11 -4.9432e-12 v Velocity[Z] -0.00015477 0.00015423 3.4297e-11 -8.9773e-13 v ǁVelocityǁ 1.0454e-11 0.0001853 7.2833e-06 3.0641e-06 v Pressure -4.2361e-05 0.0038653 9.9284e-05 1.0201e-20 v k 4.5654e-07 0.010953 0.0068535 0.0073362 v omega 75.466 1.0313e+05 2704.8 552.18 v TempK 288 338.63 289.91 288.55 v Density 1.205 1.205 1.205 1.205 v TurbVisc 5.4712e-12 0.00017228 0.00010152 0.00011399 v CourantNb 9.7251e-11 0.000238 1.1741e-05 4.9162e-06 v FourierNb 0.15357 0.94315 0.34545 0.26243 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.6309 4.6309 0.00016816 2.4098e-08 v volume_forces[Z] -4.6309 4.6309 -0.00016814 -1.6721e-08 v ǁvolume_forcesǁ 3.4147e-10 4.6333 0.17162 0.049319 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 290.13 288.69 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.024404 8.293e-05 4.7514e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.15357 0.94315 0.34546 0.26243 INSTANT 0.250380000E-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 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.63725E-07 0.36906E-02 Friction velocity uk : 0.80613E-05 0.36891E-02 Dimensionless distance yplus : 0.53674E-04 0.24544E-01 Friction thermal sca. tstar : -0.34224E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.37697E-04 0.17238E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.63725E-07 0.36906E-02 Friction velocity uk : 0.80613E-05 0.36891E-02 Dimensionless distance yplus : 0.53674E-04 0.24544E-01 Friction thermal sca. tstar : -0.34224E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.37697E-04 0.17238E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.24986E-08 6 0.10259E-04 0.24970E-09 0.38687E+02 c Velocity[X] 0.43225E-28 c Velocity[Y] 0.12485E-09 c Velocity[Z] 0.12485E-09 c Pressure 0.71319E-12 27 0.60917E-07 0.60725E-05 0.28997E+02 c k 0.24136E-05 3 0.72272E-06 0.32978E-05 0.78441E+01 c omega 0.13153E+02 1 0.17751E-06 0.43692E+03 0.10881E+00 c TempK 0.94187E+02 2 0.30376E-06 0.30878E+01 0.19622E+00 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -2.2279e-13 1.5652e-13 -3.9816e-17 -9.7878e-18 v Velocity[Y] -0.00015869 0.00015923 -4.283e-11 -4.9223e-12 v Velocity[Z] -0.00015922 0.00015869 3.6667e-11 -1.0152e-12 v ǁVelocityǁ 1.0451e-11 0.00019078 7.5479e-06 3.1872e-06 v Pressure -4.3832e-05 0.0039447 0.00010235 2.3808e-21 v k 4.4522e-07 0.010844 0.0067978 0.0072837 v omega 75.02 1.0313e+05 2704.8 551.9 v TempK 288 338.71 289.93 288.56 v Density 1.205 1.205 1.205 1.205 v TurbVisc 5.3363e-12 0.00017132 0.00010117 0.00011378 v CourantNb 1.0102e-10 0.00024562 1.2152e-05 5.1052e-06 v FourierNb 0.15351 0.92909 0.34335 0.26143 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.6388 4.6387 0.0001707 2.3736e-08 v volume_forces[Z] -4.6388 4.6387 -0.00017068 -1.62e-08 v ǁvolume_forcesǁ 3.7792e-10 4.6412 0.1742 0.050236 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 290.16 288.7 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.024544 8.3399e-05 4.7781e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.15351 0.92909 0.34336 0.26143 INSTANT 0.260010000E-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 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.28397E-07 0.37101E-02 Friction velocity uk : 0.78967E-05 0.37086E-02 Dimensionless distance yplus : 0.52579E-04 0.24674E-01 Friction thermal sca. tstar : -0.34233E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.36928E-04 0.17329E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.28397E-07 0.37101E-02 Friction velocity uk : 0.78967E-05 0.37086E-02 Dimensionless distance yplus : 0.52579E-04 0.24674E-01 Friction thermal sca. tstar : -0.34233E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.36928E-04 0.17329E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.25854E-08 6 0.94989E-05 0.24049E-09 0.36745E+02 c Velocity[X] 0.38068E-28 c Velocity[Y] 0.12024E-09 c Velocity[Z] 0.12024E-09 c Pressure 0.69487E-12 26 0.59138E-07 0.59026E-05 0.28049E+02 c k 0.23972E-05 3 0.68467E-06 0.32182E-05 0.78051E+01 c omega 0.13153E+02 1 0.16526E-06 0.39992E+03 0.10411E+00 c TempK 0.94188E+02 2 0.29078E-06 0.29068E+01 0.19037E+00 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -2.2652e-13 1.5979e-13 -3.9735e-17 -9.7707e-18 v Velocity[Y] -0.00016294 0.00016347 -4.5354e-11 -4.8607e-12 v Velocity[Z] -0.00016346 0.00016293 3.9253e-11 -1.0059e-12 v ǁVelocityǁ 1.104e-11 0.00019602 7.807e-06 3.3086e-06 v Pressure -4.5308e-05 0.0040226 0.00010539 5.0712e-21 v k 4.3411e-07 0.010737 0.0067428 0.007232 v omega 74.579 1.0313e+05 2704.8 551.61 v TempK 288 338.78 289.96 288.57 v Density 1.205 1.205 1.205 1.205 v TurbVisc 5.204e-12 0.00017037 0.00010082 0.00011356 v CourantNb 1.048e-10 0.00025297 1.2553e-05 5.2911e-06 v FourierNb 0.15345 0.91537 0.34132 0.26046 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.6462 4.6461 0.00017317 2.3378e-08 v volume_forces[Z] -4.6462 4.6461 -0.00017315 -1.5687e-08 v ǁvolume_forcesǁ 3.778e-10 4.6486 0.17672 0.051137 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 290.19 288.71 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.024674 8.3832e-05 4.8028e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.15345 0.91537 0.34133 0.26046 INSTANT 0.269640000E-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 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19387E-07 0.37282E-02 Friction velocity uk : 0.77468E-05 0.37267E-02 Dimensionless distance yplus : 0.51580E-04 0.24794E-01 Friction thermal sca. tstar : -0.34330E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.36227E-04 0.17414E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19387E-07 0.37282E-02 Friction velocity uk : 0.77468E-05 0.37267E-02 Dimensionless distance yplus : 0.51580E-04 0.24794E-01 Friction thermal sca. tstar : -0.34330E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.36227E-04 0.17414E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.26707E-08 6 0.88239E-05 0.23151E-09 0.34952E+02 c Velocity[X] 0.33571E-28 c Velocity[Y] 0.11576E-09 c Velocity[Z] 0.11576E-09 c Pressure 0.67716E-12 26 0.57408E-07 0.57394E-05 0.27163E+02 c k 0.23809E-05 3 0.64974E-06 0.31407E-05 0.77661E+01 c omega 0.13153E+02 1 0.15410E-06 0.36742E+03 0.99787E-01 c TempK 0.94189E+02 2 0.27874E-06 0.27431E+01 0.18493E+00 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -2.3e-13 1.6288e-13 -3.9631e-17 -9.7477e-18 v Velocity[Y] -0.00016699 0.0001675 -4.865e-11 -5.505e-12 v Velocity[Z] -0.0001675 0.00016698 4.1379e-11 -1.4825e-12 v ǁVelocityǁ 1.2762e-11 0.00020102 8.0607e-06 3.4282e-06 v Pressure -4.6797e-05 0.0040992 0.00010843 -3.2284e-20 v k 4.2323e-07 0.010632 0.0066884 0.0071808 v omega 74.143 1.0313e+05 2704.8 551.33 v TempK 288 338.86 289.99 288.58 v Density 1.205 1.205 1.205 1.205 v TurbVisc 5.0742e-12 0.00016942 0.00010048 0.00011335 v CourantNb 1.0894e-10 0.00026006 1.2945e-05 5.4738e-06 v FourierNb 0.1534 0.902 0.33935 0.25951 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.6531 4.653 0.00017557 2.3033e-08 v volume_forces[Z] -4.6531 4.653 -0.00017555 -1.5189e-08 v ǁvolume_forcesǁ 3.9909e-10 4.6556 0.17917 0.052021 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 290.21 288.72 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.024794 8.4233e-05 4.8257e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.1534 0.902 0.33937 0.25951 INSTANT 0.279270000E-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 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.99859E-07 0.37449E-02 Friction velocity uk : 0.76435E-05 0.37434E-02 Dimensionless distance yplus : 0.50892E-04 0.24905E-01 Friction thermal sca. tstar : -0.34516E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.35744E-04 0.17492E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.99859E-07 0.37449E-02 Friction velocity uk : 0.76435E-05 0.37434E-02 Dimensionless distance yplus : 0.50892E-04 0.24905E-01 Friction thermal sca. tstar : -0.34516E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.35744E-04 0.17492E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.27545E-08 6 0.82150E-05 0.22277E-09 0.33291E+02 c Velocity[X] 0.29639E-28 c Velocity[Y] 0.11139E-09 c Velocity[Z] 0.11139E-09 c Pressure 0.65981E-12 26 0.55728E-07 0.55808E-05 0.26334E+02 c k 0.23649E-05 3 0.61761E-06 0.30651E-05 0.77271E+01 c omega 0.13153E+02 1 0.14395E-06 0.33879E+03 0.95819E-01 c TempK 0.94190E+02 2 0.26754E-06 0.25945E+01 0.17984E+00 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -2.3325e-13 1.6581e-13 -3.9509e-17 -9.7198e-18 v Velocity[Y] -0.00017089 0.00017135 -5.1269e-11 -5.3873e-12 v Velocity[Z] -0.00017134 0.00017089 4.4158e-11 -1.4531e-12 v ǁVelocityǁ 1.4692e-11 0.0002058 8.3089e-06 3.546e-06 v Pressure -4.8292e-05 0.0041744 0.00011146 7.6267e-21 v k 4.1259e-07 0.010528 0.0066347 0.0071302 v omega 73.712 1.0313e+05 2704.8 551.04 v TempK 288 338.92 290.01 288.59 v Density 1.205 1.205 1.205 1.205 v TurbVisc 4.9471e-12 0.00016847 0.00010014 0.00011315 v CourantNb 1.1265e-10 0.0002669 1.3328e-05 5.6533e-06 v FourierNb 0.15334 0.88897 0.33745 0.25858 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.6596 4.6596 0.00017792 2.2678e-08 v volume_forces[Z] -4.6596 4.6596 -0.0001779 -1.4679e-08 v ǁvolume_forcesǁ 4.6136e-10 4.6621 0.18155 0.05289 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 290.24 288.73 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.024905 8.4604e-05 4.8468e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.15334 0.88897 0.33746 0.25859 INSTANT 0.288900000E-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 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15865E-06 0.37604E-02 Friction velocity uk : 0.75312E-05 0.37589E-02 Dimensionless distance yplus : 0.50145E-04 0.25008E-01 Friction thermal sca. tstar : -0.34794E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.35219E-04 0.17564E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15865E-06 0.37604E-02 Friction velocity uk : 0.75312E-05 0.37589E-02 Dimensionless distance yplus : 0.50145E-04 0.25008E-01 Friction thermal sca. tstar : -0.34794E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.35219E-04 0.17564E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.28368E-08 6 0.76647E-05 0.21427E-09 0.31749E+02 c Velocity[X] 0.26192E-28 c Velocity[Y] 0.10714E-09 c Velocity[Z] 0.10714E-09 c Pressure 0.64303E-12 28 0.54114E-07 0.54284E-05 0.25555E+02 c k 0.23490E-05 3 0.58802E-06 0.29914E-05 0.76880E+01 c omega 0.13153E+02 1 0.13469E-06 0.31348E+03 0.92171E-01 c TempK 0.94191E+02 2 0.25710E-06 0.24591E+01 0.17508E+00 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -2.3627e-13 1.6857e-13 -3.9369e-17 -9.6876e-18 v Velocity[Y] -0.00017472 0.00017501 -5.4043e-11 -5.3431e-12 v Velocity[Z] -0.000175 0.00017472 4.6918e-11 -1.5164e-12 v ǁVelocityǁ 1.6976e-11 0.00021036 8.5516e-06 3.6619e-06 v Pressure -4.9794e-05 0.0042484 0.00011447 6.8453e-21 v k 4.0218e-07 0.010427 0.0065816 0.0070803 v omega 73.286 1.0313e+05 2704.7 550.75 v TempK 288 338.99 290.04 288.6 v Density 1.205 1.205 1.205 1.205 v TurbVisc 4.8227e-12 0.0001677 9.9817e-05 0.00011294 v CourantNb 1.1647e-10 0.00027349 1.3702e-05 5.8296e-06 v FourierNb 0.15328 0.87629 0.3356 0.25768 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.6658 4.6657 0.00018021 2.2351e-08 v volume_forces[Z] -4.6658 4.6657 -0.00018019 -1.4209e-08 v ǁvolume_forcesǁ 5.3111e-10 4.6683 0.18389 0.053744 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 290.26 288.74 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.025008 8.4947e-05 4.8663e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.15328 0.87629 0.33561 0.25769 INSTANT 0.298530000E-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 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.22095E-06 0.37747E-02 Friction velocity uk : 0.74228E-05 0.37733E-02 Dimensionless distance yplus : 0.49423E-04 0.25104E-01 Friction thermal sca. tstar : -0.35170E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.34712E-04 0.17631E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.22095E-06 0.37747E-02 Friction velocity uk : 0.74228E-05 0.37733E-02 Dimensionless distance yplus : 0.49423E-04 0.25104E-01 Friction thermal sca. tstar : -0.35170E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.34712E-04 0.17631E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.29176E-08 6 0.71696E-05 0.20601E-09 0.30313E+02 c Velocity[X] 0.23166E-28 c Velocity[Y] 0.10301E-09 c Velocity[Z] 0.10301E-09 c Pressure 0.62646E-12 26 0.52536E-07 0.52788E-05 0.24823E+02 c k 0.23334E-05 3 0.56074E-06 0.29194E-05 0.76490E+01 c omega 0.13153E+02 1 0.12624E-06 0.29105E+03 0.88812E-01 c TempK 0.94192E+02 2 0.24733E-06 0.23353E+01 0.17061E+00 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -2.391e-13 1.7119e-13 -3.9215e-17 -9.6517e-18 v Velocity[Y] -0.00017837 0.00017849 -5.686e-11 -5.2667e-12 v Velocity[Z] -0.00017848 0.00017837 4.9831e-11 -1.5062e-12 v ǁVelocityǁ 1.9161e-11 0.00021471 8.789e-06 3.776e-06 v Pressure -5.13e-05 0.0043211 0.00011747 1.8897e-20 v k 3.92e-07 0.010327 0.0065292 0.0070309 v omega 72.866 1.0313e+05 2704.7 550.47 v TempK 288 339.05 290.06 288.61 v Density 1.205 1.205 1.205 1.205 v TurbVisc 4.7011e-12 0.00016701 9.9497e-05 0.00011274 v CourantNb 1.2028e-10 0.00027984 1.4067e-05 6.0027e-06 v FourierNb 0.15323 0.86393 0.3338 0.2568 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.6716 4.6716 0.00018245 2.2028e-08 v volume_forces[Z] -4.6716 4.6716 -0.00018242 -1.3749e-08 v ǁvolume_forcesǁ 6.1368e-10 4.6741 0.18616 0.054585 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 290.29 288.75 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.025104 8.5264e-05 4.8843e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.15323 0.86393 0.33382 0.25681 INSTANT 0.308160000E-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 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.27639E-06 0.37880E-02 Friction velocity uk : 0.73131E-05 0.37866E-02 Dimensionless distance yplus : 0.48693E-04 0.25192E-01 Friction thermal sca. tstar : -0.35653E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.34199E-04 0.17693E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.27639E-06 0.37880E-02 Friction velocity uk : 0.73131E-05 0.37866E-02 Dimensionless distance yplus : 0.48693E-04 0.25192E-01 Friction thermal sca. tstar : -0.35653E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.34199E-04 0.17693E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.29970E-08 6 0.67231E-05 0.19799E-09 0.28973E+02 c Velocity[X] 0.20503E-28 c Velocity[Y] 0.98997E-10 c Velocity[Z] 0.98997E-10 c Pressure 0.61041E-12 26 0.51015E-07 0.51347E-05 0.24133E+02 c k 0.23179E-05 3 0.53557E-06 0.28493E-05 0.76099E+01 c omega 0.13153E+02 1 0.11853E-06 0.27111E+03 0.85716E-01 c TempK 0.94193E+02 2 0.23818E-06 0.22218E+01 0.16641E+00 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -2.4174e-13 1.7367e-13 -3.905e-17 -9.6129e-18 v Velocity[Y] -0.00018186 0.0001818 -5.9731e-11 -5.1654e-12 v Velocity[Z] -0.0001818 0.00018186 5.2843e-11 -1.4799e-12 v ǁVelocityǁ 2.1106e-11 0.00021887 9.021e-06 3.8882e-06 v Pressure -5.2812e-05 0.0043928 0.00012046 -7.0108e-21 v k 3.8207e-07 0.010229 0.0064774 0.0069821 v omega 72.449 1.0313e+05 2704.6 550.18 v TempK 288 339.1 290.09 288.62 v Density 1.205 1.205 1.205 1.205 v TurbVisc 4.5822e-12 0.00016632 9.9183e-05 0.00011255 v CourantNb 1.2411e-10 0.00028596 1.4423e-05 6.1725e-06 v FourierNb 0.15317 0.85191 0.33206 0.25594 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.6772 4.6771 0.00018463 2.1715e-08 v volume_forces[Z] -4.6772 4.6771 -0.00018461 -1.3303e-08 v ǁvolume_forcesǁ 6.9268e-10 4.6796 0.18839 0.055412 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 290.31 288.76 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.025192 8.5557e-05 4.9009e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.15317 0.85191 0.33207 0.25595 INSTANT 0.317790000E-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 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.31692E-06 0.38003E-02 Friction velocity uk : 0.72035E-05 0.37989E-02 Dimensionless distance yplus : 0.47963E-04 0.25274E-01 Friction thermal sca. tstar : -0.36254E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.33686E-04 0.17751E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.31692E-06 0.38003E-02 Friction velocity uk : 0.72035E-05 0.37989E-02 Dimensionless distance yplus : 0.47963E-04 0.25274E-01 Friction thermal sca. tstar : -0.36254E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.33686E-04 0.17751E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.30748E-08 6 0.63127E-05 0.19022E-09 0.27719E+02 c Velocity[X] 0.18154E-28 c Velocity[Y] 0.95109E-10 c Velocity[Z] 0.95109E-10 c Pressure 0.59473E-12 26 0.49544E-07 0.49947E-05 0.23481E+02 c k 0.23026E-05 3 0.51230E-06 0.27809E-05 0.75707E+01 c omega 0.13153E+02 1 0.11150E-06 0.25335E+03 0.82860E-01 c TempK 0.94194E+02 2 0.22958E-06 0.21174E+01 0.16244E+00 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -2.442e-13 1.7602e-13 -3.8876e-17 -9.5716e-18 v Velocity[Y] -0.0001852 0.00018496 -6.2683e-11 -5.0697e-12 v Velocity[Z] -0.00018495 0.0001852 5.5931e-11 -1.4535e-12 v ǁVelocityǁ 2.1457e-11 0.00022285 9.2477e-06 3.9985e-06 v Pressure -5.4329e-05 0.0044634 0.00012344 -1.8685e-20 v k 3.7237e-07 0.010132 0.0064262 0.0069339 v omega 72.038 1.0313e+05 2704.5 549.89 v TempK 288 339.16 290.11 288.62 v Density 1.205 1.205 1.205 1.205 v TurbVisc 4.466e-12 0.00016563 9.8875e-05 0.00011235 v CourantNb 1.2793e-10 0.00029185 1.477e-05 6.339e-06 v FourierNb 0.15312 0.8416 0.33036 0.2551 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.6824 4.6823 0.00018677 2.1411e-08 v volume_forces[Z] -4.6824 4.6823 -0.00018675 -1.2869e-08 v ǁvolume_forcesǁ 7.6299e-10 4.6849 0.19056 0.056228 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 290.34 288.77 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.025274 8.5828e-05 4.9163e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.15312 0.8416 0.33037 0.25511 INSTANT 0.327420000E-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 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.32589E-06 0.38117E-02 Friction velocity uk : 0.70922E-05 0.38103E-02 Dimensionless distance yplus : 0.47222E-04 0.25350E-01 Friction thermal sca. tstar : -0.36988E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.33165E-04 0.17804E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.32589E-06 0.38117E-02 Friction velocity uk : 0.70922E-05 0.38103E-02 Dimensionless distance yplus : 0.47222E-04 0.25350E-01 Friction thermal sca. tstar : -0.36988E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.33165E-04 0.17804E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.31512E-08 6 0.59410E-05 0.18268E-09 0.26544E+02 c Velocity[X] 0.16079E-28 c Velocity[Y] 0.91340E-10 c Velocity[Z] 0.91340E-10 c Pressure 0.57937E-12 26 0.48126E-07 0.48582E-05 0.22865E+02 c k 0.22875E-05 3 0.49077E-06 0.27142E-05 0.75316E+01 c omega 0.13153E+02 1 0.10507E-06 0.23747E+03 0.80223E-01 c TempK 0.94195E+02 2 0.22149E-06 0.20211E+01 0.15870E+00 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -2.465e-13 1.7825e-13 -3.8693e-17 -9.5281e-18 v Velocity[Y] -0.00018838 0.00018796 -6.5716e-11 -4.9794e-12 v Velocity[Z] -0.00018796 0.00018838 5.909e-11 -1.4276e-12 v ǁVelocityǁ 2.139e-11 0.00022666 9.4691e-06 4.107e-06 v Pressure -5.5851e-05 0.004533 0.00012641 -4.872e-21 v k 3.6291e-07 0.010037 0.0063757 0.0068863 v omega 71.631 1.0313e+05 2704.4 549.6 v TempK 288 339.21 290.13 288.63 v Density 1.205 1.205 1.205 1.205 v TurbVisc 4.3527e-12 0.00016493 9.8574e-05 0.00011216 v CourantNb 1.3176e-10 0.00029753 1.5108e-05 6.5022e-06 v FourierNb 0.15306 0.83213 0.32871 0.25428 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.6874 4.6873 0.00018887 2.1115e-08 v volume_forces[Z] -4.6874 4.6873 -0.00018884 -1.2448e-08 v ǁvolume_forcesǁ 7.7567e-10 4.6899 0.1927 0.057032 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 290.36 288.78 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.02535 8.6077e-05 4.9304e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.15306 0.83213 0.32872 0.25429 INSTANT 0.337050000E-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 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.33549E-06 0.38222E-02 Friction velocity uk : 0.69582E-05 0.38208E-02 Dimensionless distance yplus : 0.46329E-04 0.25420E-01 Friction thermal sca. tstar : -0.37875E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.32539E-04 0.17853E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.33549E-06 0.38222E-02 Friction velocity uk : 0.69582E-05 0.38208E-02 Dimensionless distance yplus : 0.46329E-04 0.25420E-01 Friction thermal sca. tstar : -0.37875E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.32539E-04 0.17853E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.32262E-08 6 0.56055E-05 0.17538E-09 0.25441E+02 c Velocity[X] 0.14242E-28 c Velocity[Y] 0.87688E-10 c Velocity[Z] 0.87688E-10 c Pressure 0.56452E-12 26 0.46742E-07 0.47267E-05 0.22281E+02 c k 0.22726E-05 3 0.47082E-06 0.26492E-05 0.74925E+01 c omega 0.13153E+02 1 0.99205E-07 0.22325E+03 0.77783E-01 c TempK 0.94196E+02 2 0.21386E-06 0.19320E+01 0.15516E+00 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -2.4864e-13 1.8036e-13 -3.8502e-17 -9.4827e-18 v Velocity[Y] -0.00019141 0.00019082 -6.8824e-11 -4.8931e-12 v Velocity[Z] -0.00019082 0.00019141 6.2322e-11 -1.4013e-12 v ǁVelocityǁ 2.1283e-11 0.0002303 9.6854e-06 4.2135e-06 v Pressure -5.7378e-05 0.0046016 0.00012936 1.7594e-20 v k 3.537e-07 0.0099439 0.0063258 0.0068392 v omega 71.229 1.0313e+05 2704.4 549.31 v TempK 288 339.26 290.15 288.64 v Density 1.205 1.205 1.205 1.205 v TurbVisc 4.2422e-12 0.00016424 9.8278e-05 0.00011197 v CourantNb 1.356e-10 0.00030298 1.5439e-05 6.6622e-06 v FourierNb 0.15301 0.82285 0.3271 0.25348 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.6922 4.6921 0.00019092 2.0826e-08 v volume_forces[Z] -4.6922 4.6921 -0.0001909 -1.2038e-08 v ǁvolume_forcesǁ 7.7327e-10 4.6947 0.19478 0.057824 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 290.38 288.79 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.02542 8.6308e-05 4.9435e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.15301 0.82285 0.32712 0.25348 INSTANT 0.346680000E-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 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.34573E-06 0.38319E-02 Friction velocity uk : 0.68264E-05 0.38305E-02 Dimensionless distance yplus : 0.45452E-04 0.25484E-01 Friction thermal sca. tstar : -0.38945E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.31923E-04 0.17899E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.34573E-06 0.38319E-02 Friction velocity uk : 0.68264E-05 0.38305E-02 Dimensionless distance yplus : 0.45452E-04 0.25484E-01 Friction thermal sca. tstar : -0.38945E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.31923E-04 0.17899E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.32996E-08 6 0.52919E-05 0.16831E-09 0.24402E+02 c Velocity[X] 0.12615E-28 c Velocity[Y] 0.84153E-10 c Velocity[Z] 0.84153E-10 c Pressure 0.55006E-12 26 0.45410E-07 0.45992E-05 0.21726E+02 c k 0.22579E-05 3 0.45232E-06 0.25858E-05 0.74535E+01 c omega 0.13153E+02 1 0.93845E-07 0.21047E+03 0.75524E-01 c TempK 0.94197E+02 2 0.20665E-06 0.18495E+01 0.15181E+00 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -2.5064e-13 1.8236e-13 -3.8306e-17 -9.4359e-18 v Velocity[Y] -0.00019431 0.00019355 -7.2009e-11 -4.8103e-12 v Velocity[Z] -0.00019355 0.00019431 6.5629e-11 -1.3745e-12 v ǁVelocityǁ 2.1213e-11 0.00023377 9.8966e-06 4.3181e-06 v Pressure -5.8912e-05 0.0046693 0.00013231 2.2007e-20 v k 3.4472e-07 0.009852 0.0062766 0.0067927 v omega 70.831 1.0313e+05 2704.3 549.03 v TempK 288 339.31 290.18 288.65 v Density 1.205 1.205 1.205 1.205 v TurbVisc 4.1344e-12 0.00016355 9.7987e-05 0.00011178 v CourantNb 1.3943e-10 0.00030824 1.576e-05 6.819e-06 v FourierNb 0.15295 0.81374 0.32554 0.25269 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.6967 4.6967 0.00019293 2.0544e-08 v volume_forces[Z] -4.6967 4.6967 -0.00019291 -1.164e-08 v ǁvolume_forcesǁ 7.694e-10 4.6993 0.19683 0.058606 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 290.4 288.8 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.025484 8.652e-05 4.9555e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.15295 0.81374 0.32555 0.2527 INSTANT 0.356310000E-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 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.35338E-06 0.38408E-02 Friction velocity uk : 0.66971E-05 0.38394E-02 Dimensionless distance yplus : 0.44591E-04 0.25544E-01 Friction thermal sca. tstar : -0.40234E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.31318E-04 0.17940E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.35338E-06 0.38408E-02 Friction velocity uk : 0.66971E-05 0.38394E-02 Dimensionless distance yplus : 0.44591E-04 0.25544E-01 Friction thermal sca. tstar : -0.40234E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.31318E-04 0.17940E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.33717E-08 5 0.49840E-05 0.16147E-09 0.23423E+02 c Velocity[X] 0.11171E-28 c Velocity[Y] 0.80733E-10 c Velocity[Z] 0.80733E-10 c Pressure 0.53379E-12 26 0.43988E-07 0.44572E-05 0.21199E+02 c k 0.22433E-05 3 0.43513E-06 0.25240E-05 0.74145E+01 c omega 0.13153E+02 1 0.88949E-07 0.19896E+03 0.73430E-01 c TempK 0.94198E+02 2 0.19984E-06 0.17728E+01 0.14862E+00 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -2.525e-13 1.8425e-13 -3.8106e-17 -9.3877e-18 v Velocity[Y] -0.00019707 0.00019614 -7.5434e-11 -4.8894e-12 v Velocity[Z] -0.00019615 0.00019707 6.9059e-11 -1.3008e-12 v ǁVelocityǁ 2.0915e-11 0.00023708 1.0103e-05 4.4209e-06 v Pressure -6.0453e-05 0.0047362 0.00013524 -3.4931e-21 v k 3.3598e-07 0.0097616 0.0062279 0.0067468 v omega 70.438 1.0313e+05 2704.1 548.74 v TempK 288 339.35 290.2 288.66 v Density 1.205 1.205 1.205 1.205 v TurbVisc 4.0295e-12 0.00016285 9.7702e-05 0.0001116 v CourantNb 1.4327e-10 0.00031329 1.6074e-05 6.9726e-06 v FourierNb 0.1529 0.80482 0.32401 0.25192 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.7011 4.701 0.0001949 2.027e-08 v volume_forces[Z] -4.7011 4.701 -0.00019488 -1.1253e-08 v ǁvolume_forcesǁ 7.6683e-10 4.7036 0.19884 0.059378 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 290.43 288.8 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.025544 8.6715e-05 4.9665e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.1529 0.80482 0.32403 0.25193 INSTANT 0.365940000E-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 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.33880E-06 0.38490E-02 Friction velocity uk : 0.65657E-05 0.38477E-02 Dimensionless distance yplus : 0.43716E-04 0.25599E-01 Friction thermal sca. tstar : -0.41807E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.30704E-04 0.17979E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.33880E-06 0.38490E-02 Friction velocity uk : 0.65657E-05 0.38477E-02 Dimensionless distance yplus : 0.43716E-04 0.25599E-01 Friction thermal sca. tstar : -0.41807E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.30704E-04 0.17979E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34423E-08 5 0.47261E-05 0.15485E-09 0.22499E+02 c Velocity[X] 0.98895E-29 c Velocity[Y] 0.77425E-10 c Velocity[Z] 0.77425E-10 c Pressure 0.52012E-12 26 0.42748E-07 0.43376E-05 0.20697E+02 c k 0.22289E-05 3 0.41916E-06 0.24638E-05 0.73756E+01 c omega 0.13153E+02 1 0.84474E-07 0.18856E+03 0.71484E-01 c TempK 0.94199E+02 2 0.19338E-06 0.17015E+01 0.14560E+00 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -2.5424e-13 1.8605e-13 -3.7901e-17 -9.3386e-18 v Velocity[Y] -0.00019971 0.00019861 -7.8771e-11 -4.8159e-12 v Velocity[Z] -0.00019862 0.00019971 7.2528e-11 -1.2583e-12 v ǁVelocityǁ 2.0944e-11 0.00024025 1.0304e-05 4.5218e-06 v Pressure -6.1998e-05 0.0048021 0.00013817 8.1139e-21 v k 3.2747e-07 0.0096725 0.0061799 0.0067013 v omega 70.049 1.0313e+05 2704 548.45 v TempK 288 339.4 290.22 288.67 v Density 1.205 1.205 1.205 1.205 v TurbVisc 3.9273e-12 0.00016215 9.7422e-05 0.00011141 v CourantNb 1.471e-10 0.00031815 1.6379e-05 7.123e-06 v FourierNb 0.15285 0.79607 0.32253 0.25117 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.7053 4.7052 0.00019684 2.0005e-08 v volume_forces[Z] -4.7053 4.7052 -0.00019682 -1.0871e-08 v ǁvolume_forcesǁ 7.5609e-10 4.7078 0.2008 0.06014 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 290.45 288.81 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.025599 8.6894e-05 4.9765e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.15285 0.79607 0.32254 0.25118 INSTANT 0.375570000E-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 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.33312E-06 0.38566E-02 Friction velocity uk : 0.64414E-05 0.38552E-02 Dimensionless distance yplus : 0.42888E-04 0.25649E-01 Friction thermal sca. tstar : -0.43726E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.30122E-04 0.18014E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.33312E-06 0.38566E-02 Friction velocity uk : 0.64414E-05 0.38552E-02 Dimensionless distance yplus : 0.42888E-04 0.25649E-01 Friction thermal sca. tstar : -0.43726E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.30122E-04 0.18014E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.35114E-08 5 0.44895E-05 0.14846E-09 0.21626E+02 c Velocity[X] 0.87503E-29 c Velocity[Y] 0.74228E-10 c Velocity[Z] 0.74228E-10 c Pressure 0.50694E-12 26 0.41567E-07 0.42226E-05 0.20219E+02 c k 0.22146E-05 3 0.40428E-06 0.24052E-05 0.73368E+01 c omega 0.13153E+02 1 0.80386E-07 0.17913E+03 0.69675E-01 c TempK 0.94200E+02 2 0.18726E-06 0.16349E+01 0.14271E+00 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -2.5585e-13 1.8775e-13 -3.7693e-17 -9.2887e-18 v Velocity[Y] -0.00020223 0.00020096 -8.2168e-11 -4.7399e-12 v Velocity[Z] -0.00020097 0.00020223 7.6043e-11 -1.2333e-12 v ǁVelocityǁ 2.099e-11 0.00024327 1.0501e-05 4.6208e-06 v Pressure -6.3548e-05 0.0048673 0.00014108 1.8195e-20 v k 3.1919e-07 0.0095885 0.0061325 0.0066564 v omega 69.664 1.0313e+05 2703.9 548.17 v TempK 288 339.44 290.24 288.68 v Density 1.205 1.205 1.205 1.205 v TurbVisc 3.8278e-12 0.00016146 9.7147e-05 0.00011123 v CourantNb 1.5095e-10 0.00032282 1.6677e-05 7.2704e-06 v FourierNb 0.1528 0.7875 0.32108 0.25043 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.7093 4.7092 0.00019874 1.9745e-08 v volume_forces[Z] -4.7093 4.7092 -0.00019872 -1.0505e-08 v ǁvolume_forcesǁ 7.5714e-10 4.7118 0.20274 0.060893 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 290.47 288.82 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.025649 8.7057e-05 4.9857e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.1528 0.7875 0.32109 0.25044 INSTANT 0.385200000E-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 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.32609E-06 0.38635E-02 Friction velocity uk : 0.63188E-05 0.38622E-02 Dimensionless distance yplus : 0.42073E-04 0.25695E-01 Friction thermal sca. tstar : -0.46108E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.29549E-04 0.18047E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.32609E-06 0.38635E-02 Friction velocity uk : 0.63188E-05 0.38622E-02 Dimensionless distance yplus : 0.42073E-04 0.25695E-01 Friction thermal sca. tstar : -0.46108E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.29549E-04 0.18047E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.35792E-08 5 0.42715E-05 0.14228E-09 0.20798E+02 c Velocity[X] 0.77367E-29 c Velocity[Y] 0.71139E-10 c Velocity[Z] 0.71139E-10 c Pressure 0.49400E-12 26 0.40408E-07 0.41100E-05 0.19763E+02 c k 0.22006E-05 3 0.39042E-06 0.23480E-05 0.72981E+01 c omega 0.13153E+02 1 0.76649E-07 0.17057E+03 0.67990E-01 c TempK 0.94201E+02 2 0.18145E-06 0.15726E+01 0.13997E+00 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -2.5735e-13 1.8935e-13 -3.7483e-17 -9.2381e-18 v Velocity[Y] -0.00020463 0.00020319 -8.564e-11 -4.6669e-12 v Velocity[Z] -0.0002032 0.00020463 7.963e-11 -1.2066e-12 v ǁVelocityǁ 2.0997e-11 0.00024615 1.0693e-05 4.718e-06 v Pressure -6.5103e-05 0.0049316 0.00014398 -4.3707e-20 v k 3.1114e-07 0.0095075 0.0060857 0.0066121 v omega 69.284 1.0313e+05 2703.8 547.88 v TempK 288 339.48 290.26 288.68 v Density 1.205 1.205 1.205 1.205 v TurbVisc 3.7311e-12 0.00016076 9.6876e-05 0.00011105 v CourantNb 1.548e-10 0.0003273 1.6968e-05 7.4149e-06 v FourierNb 0.15275 0.7791 0.31966 0.24971 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.7131 4.713 0.00020061 1.9492e-08 v volume_forces[Z] -4.7131 4.713 -0.00020058 -1.015e-08 v ǁvolume_forcesǁ 7.5879e-10 4.7156 0.20464 0.061636 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 290.49 288.83 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.025695 8.7207e-05 4.9941e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.15275 0.7791 0.31968 0.24971 INSTANT 0.394830000E-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 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.31661E-06 0.38698E-02 Friction velocity uk : 0.61975E-05 0.38685E-02 Dimensionless distance yplus : 0.41265E-04 0.25737E-01 Friction thermal sca. tstar : -0.49132E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.28982E-04 0.18076E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.31661E-06 0.38698E-02 Friction velocity uk : 0.61975E-05 0.38685E-02 Dimensionless distance yplus : 0.41265E-04 0.25737E-01 Friction thermal sca. tstar : -0.49132E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.28982E-04 0.18076E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.36455E-08 5 0.40702E-05 0.13631E-09 0.20014E+02 c Velocity[X] 0.68351E-29 c Velocity[Y] 0.68157E-10 c Velocity[Z] 0.68157E-10 c Pressure 0.48153E-12 25 0.39303E-07 0.40019E-05 0.19327E+02 c k 0.21867E-05 3 0.37748E-06 0.22923E-05 0.72595E+01 c omega 0.13153E+02 1 0.73232E-07 0.16277E+03 0.66417E-01 c TempK 0.94202E+02 2 0.17592E-06 0.15143E+01 0.13734E+00 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -2.5875e-13 1.9088e-13 -3.7272e-17 -9.1871e-18 v Velocity[Y] -0.00020691 0.00020531 -8.9302e-11 -4.7152e-12 v Velocity[Z] -0.00020531 0.00020691 8.3221e-11 -1.2393e-12 v ǁVelocityǁ 2.1012e-11 0.00024889 1.088e-05 4.8135e-06 v Pressure -6.6662e-05 0.0049952 0.00014688 1.1632e-20 v k 3.0331e-07 0.0094275 0.0060394 0.0065682 v omega 68.907 1.0313e+05 2703.7 547.6 v TempK 288 339.52 290.28 288.69 v Density 1.205 1.205 1.205 1.205 v TurbVisc 3.637e-12 0.00016006 9.6611e-05 0.00011088 v CourantNb 1.5867e-10 0.00033162 1.7251e-05 7.5565e-06 v FourierNb 0.15269 0.77088 0.31828 0.249 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.7168 4.7167 0.00020244 1.9245e-08 v volume_forces[Z] -4.7168 4.7167 -0.00020242 -9.8061e-09 v ǁvolume_forcesǁ 7.5903e-10 4.7193 0.2065 0.062371 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 290.51 288.84 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.025737 8.7342e-05 5.0017e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.1527 0.77088 0.3183 0.24901 INSTANT 0.404460000E-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 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.30683E-06 0.38756E-02 Friction velocity uk : 0.60785E-05 0.38743E-02 Dimensionless distance yplus : 0.40472E-04 0.25776E-01 Friction thermal sca. tstar : -0.53091E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.28425E-04 0.18103E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.30683E-06 0.38756E-02 Friction velocity uk : 0.60785E-05 0.38743E-02 Dimensionless distance yplus : 0.40472E-04 0.25776E-01 Friction thermal sca. tstar : -0.53091E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.28425E-04 0.18103E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.37105E-08 5 0.38844E-05 0.13056E-09 0.19269E+02 c Velocity[X] 0.60323E-29 c Velocity[Y] 0.65278E-10 c Velocity[Z] 0.65278E-10 c Pressure 0.46924E-12 25 0.38208E-07 0.38956E-05 0.18910E+02 c k 0.21729E-05 3 0.36538E-06 0.22381E-05 0.72211E+01 c omega 0.13153E+02 1 0.70108E-07 0.15564E+03 0.64947E-01 c TempK 0.94203E+02 2 0.17066E-06 0.14596E+01 0.13484E+00 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -2.6004e-13 1.9232e-13 -3.7059e-17 -9.1357e-18 v Velocity[Y] -0.00020909 0.00020732 -9.2908e-11 -4.6463e-12 v Velocity[Z] -0.00020733 0.00020909 8.6946e-11 -1.2106e-12 v ǁVelocityǁ 2.1046e-11 0.00025151 1.1064e-05 4.9073e-06 v Pressure -6.8225e-05 0.0050581 0.00014976 -4.4491e-21 v k 2.9571e-07 0.0093486 0.0059938 0.0065249 v omega 68.535 1.0313e+05 2703.5 547.32 v TempK 288 339.56 290.3 288.7 v Density 1.205 1.205 1.205 1.205 v TurbVisc 3.5455e-12 0.00015936 9.6349e-05 0.0001107 v CourantNb 1.6252e-10 0.00033576 1.7528e-05 7.6954e-06 v FourierNb 0.15264 0.76282 0.31693 0.2483 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.7203 4.7203 0.00020425 1.9003e-08 v volume_forces[Z] -4.7203 4.7203 -0.00020422 -9.4675e-09 v ǁvolume_forcesǁ 7.5959e-10 4.7229 0.20833 0.063098 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 290.53 288.84 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.025776 8.7465e-05 5.0086e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.15264 0.76282 0.31695 0.24831 INSTANT 0.414090000E-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 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.29357E-06 0.38808E-02 Friction velocity uk : 0.59602E-05 0.38795E-02 Dimensionless distance yplus : 0.39685E-04 0.25811E-01 Friction thermal sca. tstar : -0.58520E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.27872E-04 0.18128E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.29357E-06 0.38808E-02 Friction velocity uk : 0.59602E-05 0.38795E-02 Dimensionless distance yplus : 0.39685E-04 0.25811E-01 Friction thermal sca. tstar : -0.58520E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.27872E-04 0.18128E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.37741E-08 5 0.37138E-05 0.12500E-09 0.18561E+02 c Velocity[X] 0.53172E-29 c Velocity[Y] 0.62500E-10 c Velocity[Z] 0.62500E-10 c Pressure 0.45738E-12 25 0.37158E-07 0.37933E-05 0.18511E+02 c k 0.21593E-05 3 0.35407E-06 0.21853E-05 0.71828E+01 c omega 0.13153E+02 1 0.67251E-07 0.14912E+03 0.63570E-01 c TempK 0.94204E+02 2 0.16565E-06 0.14083E+01 0.13244E+00 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -2.6124e-13 1.9368e-13 -3.6846e-17 -9.0843e-18 v Velocity[Y] -0.00021117 0.00020929 -9.6578e-11 -4.5799e-12 v Velocity[Z] -0.00020929 0.00021117 9.0733e-11 -1.1819e-12 v ǁVelocityǁ 2.1111e-11 0.00025401 1.1243e-05 4.9994e-06 v Pressure -6.9792e-05 0.0051203 0.00015263 -8.9167e-21 v k 2.8832e-07 0.0092707 0.0059487 0.0064821 v omega 68.167 1.0313e+05 2703.4 547.03 v TempK 288 339.59 290.32 288.71 v Density 1.205 1.205 1.205 1.205 v TurbVisc 3.4566e-12 0.00015866 9.6092e-05 0.00011053 v CourantNb 1.6639e-10 0.00033973 1.7799e-05 7.8318e-06 v FourierNb 0.15259 0.75494 0.31561 0.24762 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.7237 4.7237 0.00020602 1.877e-08 v volume_forces[Z] -4.7237 4.7237 -0.000206 -9.1431e-09 v ǁvolume_forcesǁ 7.6082e-10 4.7263 0.21014 0.063816 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 290.55 288.85 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.025811 8.7576e-05 5.0147e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.15259 0.75494 0.31563 0.24763 INSTANT 0.423720000E-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 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.28048E-06 0.38855E-02 Friction velocity uk : 0.58444E-05 0.38842E-02 Dimensionless distance yplus : 0.38914E-04 0.25842E-01 Friction thermal sca. tstar : -0.66519E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.27330E-04 0.18150E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.28048E-06 0.38855E-02 Friction velocity uk : 0.58444E-05 0.38842E-02 Dimensionless distance yplus : 0.38914E-04 0.25842E-01 Friction thermal sca. tstar : -0.66519E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.27330E-04 0.18150E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.38363E-08 5 0.35552E-05 0.11964E-09 0.17887E+02 c Velocity[X] 0.46809E-29 c Velocity[Y] 0.59821E-10 c Velocity[Z] 0.59821E-10 c Pressure 0.44570E-12 25 0.36152E-07 0.36928E-05 0.18128E+02 c k 0.21459E-05 3 0.34346E-06 0.21338E-05 0.71447E+01 c omega 0.13153E+02 1 0.64636E-07 0.14312E+03 0.62278E-01 c TempK 0.94205E+02 2 0.16087E-06 0.13599E+01 0.13014E+00 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -2.6235e-13 1.9499e-13 -3.6632e-17 -9.0326e-18 v Velocity[Y] -0.00021315 0.00021128 -1.0086e-10 -5.037e-12 v Velocity[Z] -0.00021128 0.00021315 9.4729e-11 -1.0113e-12 v ǁVelocityǁ 2.0967e-11 0.00025639 1.1417e-05 5.0897e-06 v Pressure -7.1364e-05 0.0051818 0.00015549 -5.6197e-21 v k 2.8114e-07 0.0091937 0.0059042 0.0064397 v omega 67.802 1.0313e+05 2703.2 546.75 v TempK 288 339.63 290.34 288.71 v Density 1.205 1.205 1.205 1.205 v TurbVisc 3.3702e-12 0.00015796 9.5839e-05 0.00011036 v CourantNb 1.7022e-10 0.00034355 1.8064e-05 7.9656e-06 v FourierNb 0.15254 0.74721 0.31433 0.24695 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.727 4.727 0.00020777 1.8543e-08 v volume_forces[Z] -4.727 4.727 -0.00020774 -8.8284e-09 v ǁvolume_forcesǁ 7.6315e-10 4.7296 0.21191 0.064527 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 290.57 288.86 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.025842 8.7675e-05 5.0202e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.15254 0.74721 0.31435 0.24696 INSTANT 0.433350000E-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 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.25163E-06 0.38897E-02 Friction velocity uk : 0.57230E-05 0.38885E-02 Dimensionless distance yplus : 0.38105E-04 0.25870E-01 Friction thermal sca. tstar : -0.79847E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.26763E-04 0.18170E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.25163E-06 0.38897E-02 Friction velocity uk : 0.57230E-05 0.38885E-02 Dimensionless distance yplus : 0.38105E-04 0.25870E-01 Friction thermal sca. tstar : -0.79847E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.26763E-04 0.18170E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.38971E-08 5 0.34091E-05 0.11448E-09 0.17245E+02 c Velocity[X] 0.41138E-29 c Velocity[Y] 0.57238E-10 c Velocity[Z] 0.57238E-10 c Pressure 0.43438E-12 25 0.35165E-07 0.35956E-05 0.17761E+02 c k 0.21326E-05 3 0.33352E-06 0.20837E-05 0.71068E+01 c omega 0.13153E+02 1 0.62242E-07 0.13759E+03 0.61064E-01 c TempK 0.94206E+02 2 0.15630E-06 0.13143E+01 0.12794E+00 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -2.6337e-13 1.9622e-13 -3.6418e-17 -8.9809e-18 v Velocity[Y] -0.00021503 0.00021317 -1.048e-10 -5.1167e-12 v Velocity[Z] -0.00021317 0.00021503 9.8664e-11 -9.643e-13 v ǁVelocityǁ 2.1032e-11 0.00025866 1.1588e-05 5.1783e-06 v Pressure -7.2938e-05 0.0052427 0.00015835 2.8582e-20 v k 2.7416e-07 0.0091177 0.0058603 0.0063979 v omega 67.442 1.0313e+05 2703.1 546.47 v TempK 288 339.66 290.36 288.72 v Density 1.205 1.205 1.205 1.205 v TurbVisc 3.2863e-12 0.00015726 9.559e-05 0.00011019 v CourantNb 1.7405e-10 0.00034773 1.8322e-05 8.0967e-06 v FourierNb 0.1525 0.73964 0.31307 0.24629 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.7302 4.7301 0.00020949 1.8327e-08 v volume_forces[Z] -4.7302 4.7301 -0.00020946 -8.5042e-09 v ǁvolume_forcesǁ 7.5796e-10 4.7328 0.21366 0.065231 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 290.59 288.87 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.02587 8.7764e-05 5.0251e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.1525 0.73964 0.31309 0.2463 INSTANT 0.442980000E-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 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.22941E-06 0.38935E-02 Friction velocity uk : 0.56074E-05 0.38923E-02 Dimensionless distance yplus : 0.37336E-04 0.25896E-01 Friction thermal sca. tstar : -0.10870E+05 0.00000E+00 Dim-less thermal sca. tplus : 0.26222E-04 0.18187E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.22941E-06 0.38935E-02 Friction velocity uk : 0.56074E-05 0.38923E-02 Dimensionless distance yplus : 0.37336E-04 0.25896E-01 Friction thermal sca. tstar : -0.10870E+05 0.00000E+00 Dim-less thermal sca. tplus : 0.26222E-04 0.18187E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.39567E-08 5 0.33179E-05 0.10950E-09 0.16633E+02 c Velocity[X] 0.36093E-29 c Velocity[Y] 0.54748E-10 c Velocity[Z] 0.54748E-10 c Pressure 0.42354E-12 25 0.34215E-07 0.35027E-05 0.17408E+02 c k 0.21195E-05 3 0.32417E-06 0.20349E-05 0.70691E+01 c omega 0.13153E+02 1 0.60049E-07 0.13249E+03 0.59921E-01 c TempK 0.94207E+02 2 0.15195E-06 0.12713E+01 0.12583E+00 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -2.6431e-13 1.9739e-13 -3.6204e-17 -8.9292e-18 v Velocity[Y] -0.00021682 0.00021497 -1.0865e-10 -5.0485e-12 v Velocity[Z] -0.00021497 0.00021682 1.0264e-10 -9.4029e-13 v ǁVelocityǁ 2.1291e-11 0.00026082 1.1754e-05 5.2651e-06 v Pressure -7.4518e-05 0.0053029 0.00016119 -7.0659e-21 v k 2.6739e-07 0.0090427 0.0058169 0.0063565 v omega 67.085 1.0313e+05 2702.9 546.19 v TempK 288 339.69 290.38 288.73 v Density 1.205 1.205 1.205 1.205 v TurbVisc 3.2048e-12 0.00015656 9.5345e-05 0.00011003 v CourantNb 1.7792e-10 0.00035224 1.8574e-05 8.225e-06 v FourierNb 0.15245 0.73223 0.31184 0.24565 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.7333 4.7332 0.00021118 1.8112e-08 v volume_forces[Z] -4.7333 4.7332 -0.00021115 -8.2029e-09 v ǁvolume_forcesǁ 7.6029e-10 4.7359 0.21538 0.065927 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 290.61 288.88 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.025896 8.7841e-05 5.0294e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.15245 0.73223 0.31186 0.24566 INSTANT 0.452610000E-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 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.21714E-06 0.38969E-02 Friction velocity uk : 0.54992E-05 0.38956E-02 Dimensionless distance yplus : 0.36616E-04 0.25918E-01 Friction thermal sca. tstar : -0.32572E+05 0.00000E+00 Dim-less thermal sca. tplus : 0.25716E-04 0.18203E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.21714E-06 0.38969E-02 Friction velocity uk : 0.54992E-05 0.38956E-02 Dimensionless distance yplus : 0.36616E-04 0.25918E-01 Friction thermal sca. tstar : -0.32572E+05 0.00000E+00 Dim-less thermal sca. tplus : 0.25716E-04 0.18203E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.40148E-08 5 0.31489E-05 0.10470E-09 0.16048E+02 c Velocity[X] 0.31603E-29 c Velocity[Y] 0.52349E-10 c Velocity[Z] 0.52350E-10 c Pressure 0.41265E-12 26 0.33421E-07 0.34096E-05 0.17070E+02 c k 0.21065E-05 3 0.31538E-06 0.19874E-05 0.70316E+01 c omega 0.13153E+02 1 0.58039E-07 0.12776E+03 0.58843E-01 c TempK 0.94208E+02 2 0.14778E-06 0.12307E+01 0.12379E+00 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -2.6517e-13 1.9848e-13 -3.599e-17 -8.8775e-18 v Velocity[Y] -0.00021852 0.00021669 -1.1468e-10 -7.0887e-12 v Velocity[Z] -0.00021669 0.00021852 1.0397e-10 -3.4943e-12 v ǁVelocityǁ 2.0468e-11 0.00026287 1.1916e-05 5.3502e-06 v Pressure -7.6105e-05 0.0053625 0.00016402 -2.8251e-21 v k 2.6082e-07 0.0089686 0.0057741 0.0063156 v omega 66.732 1.0313e+05 2702.8 545.92 v TempK 288 339.72 290.39 288.74 v Density 1.205 1.205 1.205 1.205 v TurbVisc 3.1256e-12 0.00015588 9.5104e-05 0.00010986 v CourantNb 1.8258e-10 0.00035659 1.8819e-05 8.3505e-06 v FourierNb 0.1524 0.72497 0.31063 0.24501 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.7363 4.7362 0.00021285 1.7903e-08 v volume_forces[Z] -4.7363 4.7362 -0.00021282 -7.9161e-09 v ǁvolume_forcesǁ 7.6967e-10 4.7388 0.21707 0.066616 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 290.62 288.88 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.025918 8.7908e-05 5.033e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.1524 0.72497 0.31065 0.24502 INSTANT 0.462240000E-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 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.68557E-07 0.38998E-02 Friction velocity uk : 0.53244E-05 0.38986E-02 Dimensionless distance yplus : 0.35451E-04 0.25938E-01 Friction thermal sca. tstar : -0.13627E+05 0.00000E+00 Dim-less thermal sca. tplus : 0.24899E-04 0.18217E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.68557E-07 0.38998E-02 Friction velocity uk : 0.53244E-05 0.38986E-02 Dimensionless distance yplus : 0.35451E-04 0.25938E-01 Friction thermal sca. tstar : -0.13627E+05 0.00000E+00 Dim-less thermal sca. tplus : 0.24899E-04 0.18217E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.40717E-08 5 0.30421E-05 0.10008E-09 0.15490E+02 c Velocity[X] 0.27613E-29 c Velocity[Y] 0.50040E-10 c Velocity[Z] 0.50040E-10 c Pressure 0.40224E-12 26 0.32517E-07 0.33208E-05 0.16744E+02 c k 0.20936E-05 3 0.30710E-06 0.19412E-05 0.69943E+01 c omega 0.13153E+02 1 0.56194E-07 0.12338E+03 0.57824E-01 c TempK 0.94209E+02 2 0.14379E-06 0.11922E+01 0.12184E+00 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -2.6596e-13 1.9952e-13 -3.5777e-17 -8.8259e-18 v Velocity[Y] -0.00022014 0.00021832 -1.1859e-10 -7.0077e-12 v Velocity[Z] -0.00021832 0.00022014 1.0811e-10 -3.4434e-12 v ǁVelocityǁ 2.0978e-11 0.00026482 1.2074e-05 5.4335e-06 v Pressure -7.7692e-05 0.0054215 0.00016684 7.9668e-22 v k 2.5443e-07 0.0088954 0.0057318 0.0062751 v omega 66.383 1.0313e+05 2702.6 545.64 v TempK 288 339.75 290.41 288.75 v Density 1.205 1.205 1.205 1.205 v TurbVisc 3.0487e-12 0.00015538 9.4866e-05 0.0001097 v CourantNb 1.8638e-10 0.0003608 1.9057e-05 8.4732e-06 v FourierNb 0.15235 0.71787 0.30945 0.24439 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.7391 4.7391 0.00021449 1.7606e-08 v volume_forces[Z] -4.7391 4.7391 -0.00021446 -7.5617e-09 v ǁvolume_forcesǁ 7.3991e-10 4.7417 0.21874 0.067299 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 290.64 288.89 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.025938 8.7971e-05 5.0364e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.15235 0.71787 0.30947 0.2444 INSTANT 0.471870000E-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 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.70120E-07 0.39024E-02 Friction velocity uk : 0.52279E-05 0.39012E-02 Dimensionless distance yplus : 0.34809E-04 0.25955E-01 Friction thermal sca. tstar : -0.86280E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.24448E-04 0.18229E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.70120E-07 0.39024E-02 Friction velocity uk : 0.52279E-05 0.39012E-02 Dimensionless distance yplus : 0.34809E-04 0.25955E-01 Friction thermal sca. tstar : -0.86280E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.24448E-04 0.18229E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.41273E-08 5 0.29230E-05 0.95633E-10 0.14955E+02 c Velocity[X] 0.24068E-29 c Velocity[Y] 0.47816E-10 c Velocity[Z] 0.47816E-10 c Pressure 0.39214E-12 26 0.31643E-07 0.32347E-05 0.16430E+02 c k 0.20809E-05 3 0.29929E-06 0.18962E-05 0.69573E+01 c omega 0.13153E+02 1 0.54499E-07 0.11929E+03 0.56859E-01 c TempK 0.94210E+02 2 0.13997E-06 0.11557E+01 0.11996E+00 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -2.6668e-13 2.0049e-13 -3.5564e-17 -8.7743e-18 v Velocity[Y] -0.00022168 0.00021988 -1.2256e-10 -6.9149e-12 v Velocity[Z] -0.00021988 0.00022168 1.1231e-10 -3.3942e-12 v ǁVelocityǁ 2.1465e-11 0.00026668 1.2228e-05 5.5151e-06 v Pressure -7.9285e-05 0.00548 0.00016966 1.3544e-20 v k 2.4824e-07 0.0088231 0.00569 0.0062352 v omega 66.037 1.0313e+05 2702.5 545.37 v TempK 288 339.78 290.43 288.75 v Density 1.205 1.205 1.205 1.205 v TurbVisc 2.9741e-12 0.00015487 9.4632e-05 0.00010954 v CourantNb 1.9037e-10 0.00036486 1.9289e-05 8.593e-06 v FourierNb 0.1523 0.7109 0.3083 0.24378 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.7419 4.7419 0.00021611 1.7409e-08 v volume_forces[Z] -4.7419 4.7419 -0.00021608 -7.2927e-09 v ǁvolume_forcesǁ 7.5836e-10 4.7445 0.22039 0.067974 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 290.66 288.9 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.025955 8.8025e-05 5.0393e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.1523 0.7109 0.30832 0.24379 INSTANT 0.481500000E-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 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.65353E-07 0.39045E-02 Friction velocity uk : 0.51305E-05 0.39033E-02 Dimensionless distance yplus : 0.34160E-04 0.25969E-01 Friction thermal sca. tstar : -0.67796E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.23992E-04 0.18239E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.65353E-07 0.39045E-02 Friction velocity uk : 0.51305E-05 0.39033E-02 Dimensionless distance yplus : 0.34160E-04 0.25969E-01 Friction thermal sca. tstar : -0.67796E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.23992E-04 0.18239E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.41816E-08 5 0.28273E-05 0.91353E-10 0.14444E+02 c Velocity[X] 0.20921E-29 c Velocity[Y] 0.45676E-10 c Velocity[Z] 0.45676E-10 c Pressure 0.38238E-12 26 0.30791E-07 0.31518E-05 0.16128E+02 c k 0.20684E-05 3 0.29192E-06 0.18523E-05 0.69205E+01 c omega 0.13153E+02 1 0.52939E-07 0.11548E+03 0.55943E-01 c TempK 0.94211E+02 2 0.13631E-06 0.11212E+01 0.11815E+00 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -2.6733e-13 2.0141e-13 -3.5352e-17 -8.723e-18 v Velocity[Y] -0.00022314 0.00022135 -1.2659e-10 -6.8289e-12 v Velocity[Z] -0.00022135 0.00022314 1.1656e-10 -3.3462e-12 v ǁVelocityǁ 2.1949e-11 0.00026844 1.2378e-05 5.595e-06 v Pressure -8.0881e-05 0.0055379 0.00017246 -9.0025e-21 v k 2.4222e-07 0.0087517 0.0056488 0.0061956 v omega 65.695 1.0313e+05 2702.3 545.1 v TempK 288 339.81 290.45 288.76 v Density 1.205 1.205 1.205 1.205 v TurbVisc 2.9017e-12 0.00015437 9.4402e-05 0.00010938 v CourantNb 1.9435e-10 0.00036878 1.9515e-05 8.7101e-06 v FourierNb 0.15226 0.70408 0.30717 0.24318 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.7446 4.7445 0.00021771 1.7218e-08 v volume_forces[Z] -4.7446 4.7445 -0.00021768 -7.0324e-09 v ǁvolume_forcesǁ 7.7596e-10 4.7472 0.22201 0.068644 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 290.68 288.91 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.025969 8.807e-05 5.0417e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.15226 0.70408 0.30719 0.24319 INSTANT 0.491130000E-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 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.57347E-07 0.39064E-02 Friction velocity uk : 0.50336E-05 0.39052E-02 Dimensionless distance yplus : 0.33515E-04 0.25981E-01 Friction thermal sca. tstar : -0.57402E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.23539E-04 0.18248E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.57347E-07 0.39064E-02 Friction velocity uk : 0.50336E-05 0.39052E-02 Dimensionless distance yplus : 0.33515E-04 0.25981E-01 Friction thermal sca. tstar : -0.57402E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.23539E-04 0.18248E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.42346E-08 5 0.27291E-05 0.87235E-10 0.13954E+02 c Velocity[X] 0.18135E-29 c Velocity[Y] 0.43618E-10 c Velocity[Z] 0.43618E-10 c Pressure 0.37281E-12 26 0.29966E-07 0.30705E-05 0.15837E+02 c k 0.20559E-05 3 0.28494E-06 0.18097E-05 0.68839E+01 c omega 0.13153E+02 1 0.51503E-07 0.11192E+03 0.55073E-01 c TempK 0.94212E+02 2 0.13281E-06 0.10883E+01 0.11640E+00 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -2.6792e-13 2.0227e-13 -3.5141e-17 -8.6718e-18 v Velocity[Y] -0.00022453 0.00022275 -1.3068e-10 -6.7451e-12 v Velocity[Z] -0.00022275 0.00022453 1.2086e-10 -3.2976e-12 v ǁVelocityǁ 2.2438e-11 0.00027011 1.2524e-05 5.6731e-06 v Pressure -8.2481e-05 0.0055952 0.00017525 1.3801e-20 v k 2.3638e-07 0.0086811 0.0056081 0.0061565 v omega 65.356 1.0313e+05 2702.2 544.82 v TempK 288 339.84 290.47 288.77 v Density 1.205 1.205 1.205 1.205 v TurbVisc 2.8314e-12 0.00015386 9.4174e-05 0.00010922 v CourantNb 1.9831e-10 0.00037257 1.9734e-05 8.8244e-06 v FourierNb 0.15221 0.6974 0.30606 0.24259 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.7472 4.7472 0.00021928 1.7031e-08 v volume_forces[Z] -4.7472 4.7472 -0.00021925 -6.78e-09 v ǁvolume_forcesǁ 7.9346e-10 4.7498 0.22361 0.069308 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 290.7 288.91 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.025981 8.8107e-05 5.0436e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.15221 0.6974 0.30608 0.2426 INSTANT 0.500760000E-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 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.47554E-07 0.39079E-02 Friction velocity uk : 0.49380E-05 0.39067E-02 Dimensionless distance yplus : 0.32879E-04 0.25991E-01 Friction thermal sca. tstar : -0.50507E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.23092E-04 0.18255E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.47554E-07 0.39079E-02 Friction velocity uk : 0.49380E-05 0.39067E-02 Dimensionless distance yplus : 0.32879E-04 0.25991E-01 Friction thermal sca. tstar : -0.50507E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.23092E-04 0.18255E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.42864E-08 5 0.26431E-05 0.83275E-10 0.13484E+02 c Velocity[X] 0.15671E-29 c Velocity[Y] 0.41638E-10 c Velocity[Z] 0.41638E-10 c Pressure 0.36362E-12 26 0.29164E-07 0.29926E-05 0.15555E+02 c k 0.20437E-05 3 0.27834E-06 0.17681E-05 0.68476E+01 c omega 0.13153E+02 1 0.50178E-07 0.10857E+03 0.54244E-01 c TempK 0.94213E+02 2 0.12944E-06 0.10571E+01 0.11472E+00 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -2.6845e-13 2.0308e-13 -3.4931e-17 -8.621e-18 v Velocity[Y] -0.00022584 0.00022408 -1.3482e-10 -6.6627e-12 v Velocity[Z] -0.00022408 0.00022584 1.252e-10 -3.2509e-12 v ǁVelocityǁ 2.2934e-11 0.0002717 1.2666e-05 5.7495e-06 v Pressure -8.4084e-05 0.0056521 0.00017804 6.5389e-21 v k 2.3071e-07 0.0086114 0.0055678 0.0061179 v omega 65.021 1.0313e+05 2702 544.56 v TempK 288 339.87 290.48 288.77 v Density 1.205 1.205 1.205 1.205 v TurbVisc 2.7631e-12 0.00015335 9.395e-05 0.00010907 v CourantNb 2.0226e-10 0.00037622 1.9947e-05 8.9359e-06 v FourierNb 0.15216 0.69086 0.30497 0.242 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.7498 4.7497 0.00022084 1.685e-08 v volume_forces[Z] -4.7498 4.7497 -0.00022081 -6.5354e-09 v ǁvolume_forcesǁ 8.1112e-10 4.7524 0.22518 0.069965 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 290.71 288.92 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.025991 8.8136e-05 5.0451e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.15216 0.69086 0.30499 0.24201 INSTANT 0.510390000E-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 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.36565E-07 0.39090E-02 Friction velocity uk : 0.48440E-05 0.39079E-02 Dimensionless distance yplus : 0.32253E-04 0.25999E-01 Friction thermal sca. tstar : -0.45498E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.22652E-04 0.18260E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.36565E-07 0.39090E-02 Friction velocity uk : 0.48440E-05 0.39079E-02 Dimensionless distance yplus : 0.32253E-04 0.25999E-01 Friction thermal sca. tstar : -0.45498E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.22652E-04 0.18260E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.43369E-08 5 0.25622E-05 0.79469E-10 0.13033E+02 c Velocity[X] 0.13496E-29 c Velocity[Y] 0.39734E-10 c Velocity[Z] 0.39734E-10 c Pressure 0.35462E-12 26 0.28389E-07 0.29164E-05 0.15284E+02 c k 0.20315E-05 3 0.27207E-06 0.17277E-05 0.68116E+01 c omega 0.13153E+02 1 0.48954E-07 0.10543E+03 0.53453E-01 c TempK 0.94214E+02 2 0.12621E-06 0.10274E+01 0.11309E+00 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -2.6892e-13 2.0384e-13 -3.4722e-17 -8.5704e-18 v Velocity[Y] -0.00022708 0.00022534 -1.3901e-10 -6.5834e-12 v Velocity[Z] -0.00022534 0.00022708 1.2964e-10 -3.1688e-12 v ǁVelocityǁ 2.3437e-11 0.0002732 1.2804e-05 5.8242e-06 v Pressure -8.5691e-05 0.0057084 0.00018081 5.2949e-21 v k 2.2521e-07 0.0085424 0.0055281 0.0060797 v omega 64.689 1.0313e+05 2701.8 544.29 v TempK 288 339.89 290.5 288.78 v Density 1.205 1.205 1.205 1.205 v TurbVisc 2.6968e-12 0.00015284 9.3729e-05 0.00010891 v CourantNb 2.0621e-10 0.00037974 2.0154e-05 9.0446e-06 v FourierNb 0.15212 0.68444 0.30391 0.24143 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.7522 4.7522 0.00022237 1.6674e-08 v volume_forces[Z] -4.7522 4.7522 -0.00022234 -6.2985e-09 v ǁvolume_forcesǁ 8.2905e-10 4.7549 0.22674 0.070617 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 290.73 288.93 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.025999 8.8158e-05 5.0461e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.15212 0.68444 0.30393 0.24144 INSTANT 0.520020000E-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 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.31585E-07 0.39099E-02 Friction velocity uk : 0.47550E-05 0.39087E-02 Dimensionless distance yplus : 0.31660E-04 0.26005E-01 Friction thermal sca. tstar : -0.41645E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.22236E-04 0.18264E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.31585E-07 0.39099E-02 Friction velocity uk : 0.47550E-05 0.39087E-02 Dimensionless distance yplus : 0.31660E-04 0.26005E-01 Friction thermal sca. tstar : -0.41645E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.22236E-04 0.18264E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.43862E-08 5 0.24943E-05 0.75810E-10 0.12600E+02 c Velocity[X] 0.11582E-29 c Velocity[Y] 0.37905E-10 c Velocity[Z] 0.37905E-10 c Pressure 0.34595E-12 26 0.27639E-07 0.28431E-05 0.15022E+02 c k 0.20195E-05 3 0.26612E-06 0.16883E-05 0.67758E+01 c omega 0.13153E+02 1 0.47820E-07 0.10247E+03 0.52698E-01 c TempK 0.94215E+02 2 0.12311E-06 0.99905E+00 0.11152E+00 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -2.6934e-13 2.0455e-13 -3.4514e-17 -8.52e-18 v Velocity[Y] -0.00022826 0.00022653 -1.4325e-10 -6.5045e-12 v Velocity[Z] -0.00022653 0.00022826 1.3408e-10 -3.1231e-12 v ǁVelocityǁ 2.3949e-11 0.00027463 1.2939e-05 5.8972e-06 v Pressure -8.7301e-05 0.0057642 0.00018358 -2.8803e-21 v k 2.1987e-07 0.0084743 0.0054889 0.0060419 v omega 64.36 1.0313e+05 2701.7 544.02 v TempK 288 339.92 290.52 288.79 v Density 1.205 1.205 1.205 1.205 v TurbVisc 2.6325e-12 0.00015233 9.3512e-05 0.00010876 v CourantNb 2.1017e-10 0.00038313 2.0354e-05 9.1507e-06 v FourierNb 0.15207 0.67815 0.30287 0.24087 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.7546 4.7546 0.00022388 1.6504e-08 v volume_forces[Z] -4.7546 4.7546 -0.00022385 -6.0689e-09 v ǁvolume_forcesǁ 8.4725e-10 4.7573 0.22828 0.071263 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 290.75 288.93 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.026005 8.8173e-05 5.0468e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.15207 0.67815 0.30289 0.24088 INSTANT 0.529650000E-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 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.32154E-07 0.39104E-02 Friction velocity uk : 0.46709E-05 0.39093E-02 Dimensionless distance yplus : 0.31100E-04 0.26009E-01 Friction thermal sca. tstar : -0.38562E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.21843E-04 0.18267E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.32154E-07 0.39104E-02 Friction velocity uk : 0.46709E-05 0.39093E-02 Dimensionless distance yplus : 0.31100E-04 0.26009E-01 Friction thermal sca. tstar : -0.38562E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.21843E-04 0.18267E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.44343E-08 5 0.24149E-05 0.72295E-10 0.12184E+02 c Velocity[X] 0.99027E-30 c Velocity[Y] 0.36147E-10 c Velocity[Z] 0.36148E-10 c Pressure 0.33740E-12 26 0.26900E-07 0.27710E-05 0.14769E+02 c k 0.20076E-05 3 0.26047E-06 0.16500E-05 0.67402E+01 c omega 0.13153E+02 1 0.46768E-07 0.99678E+02 0.51974E-01 c TempK 0.94216E+02 2 0.12012E-06 0.97204E+00 0.11000E+00 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -2.697e-13 2.0521e-13 -3.4308e-17 -8.47e-18 v Velocity[Y] -0.00022937 0.00022766 -1.4754e-10 -6.4284e-12 v Velocity[Z] -0.00022766 0.00022937 1.3857e-10 -3.0784e-12 v ǁVelocityǁ 2.4468e-11 0.00027597 1.3069e-05 5.9686e-06 v Pressure -8.8914e-05 0.0058196 0.00018633 -1.0332e-20 v k 2.1468e-07 0.008407 0.0054501 0.0060045 v omega 64.035 1.0313e+05 2701.5 543.76 v TempK 288 339.94 290.53 288.8 v Density 1.205 1.205 1.205 1.205 v TurbVisc 2.5701e-12 0.00015182 9.3297e-05 0.00010861 v CourantNb 2.1412e-10 0.0003864 2.0549e-05 9.254e-06 v FourierNb 0.15203 0.67199 0.30184 0.24031 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.757 4.7569 0.00022538 1.6337e-08 v volume_forces[Z] -4.757 4.7569 -0.00022534 -5.8467e-09 v ǁvolume_forcesǁ 8.6575e-10 4.7596 0.22979 0.071903 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 290.76 288.94 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.026009 8.8181e-05 5.0471e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.15203 0.67199 0.30186 0.24032 INSTANT 0.539280000E-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 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.32730E-07 0.39107E-02 Friction velocity uk : 0.45888E-05 0.39096E-02 Dimensionless distance yplus : 0.30553E-04 0.26011E-01 Friction thermal sca. tstar : -0.36021E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.21459E-04 0.18268E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.32730E-07 0.39107E-02 Friction velocity uk : 0.45888E-05 0.39096E-02 Dimensionless distance yplus : 0.30553E-04 0.26011E-01 Friction thermal sca. tstar : -0.36021E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.21459E-04 0.18268E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.44812E-08 5 0.23511E-05 0.68919E-10 0.11784E+02 c Velocity[X] 0.84326E-30 c Velocity[Y] 0.34459E-10 c Velocity[Z] 0.34460E-10 c Pressure 0.32932E-12 26 0.26203E-07 0.27029E-05 0.14524E+02 c k 0.19958E-05 3 0.25508E-06 0.16126E-05 0.67050E+01 c omega 0.13153E+02 1 0.45790E-07 0.97035E+02 0.51281E-01 c TempK 0.94217E+02 2 0.11725E-06 0.94626E+00 0.10853E+00 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -2.7002e-13 2.0582e-13 -3.4103e-17 -8.4202e-18 v Velocity[Y] -0.00023042 0.00022873 -1.5204e-10 -6.5158e-12 v Velocity[Z] -0.00022873 0.00023042 1.4302e-10 -3.1203e-12 v ǁVelocityǁ 2.5031e-11 0.00027724 1.3196e-05 6.0382e-06 v Pressure -9.053e-05 0.0058744 0.00018908 8.2364e-21 v k 2.0965e-07 0.0083405 0.0054119 0.0059675 v omega 63.713 1.0313e+05 2701.3 543.49 v TempK 288 339.97 290.55 288.8 v Density 1.205 1.205 1.205 1.205 v TurbVisc 2.5095e-12 0.00015131 9.3085e-05 0.00010846 v CourantNb 2.1806e-10 0.00038956 2.0737e-05 9.3548e-06 v FourierNb 0.15198 0.66596 0.30084 0.23977 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.7592 4.7592 0.00022685 1.6175e-08 v volume_forces[Z] -4.7592 4.7592 -0.00022682 -5.6314e-09 v ǁvolume_forcesǁ 8.8453e-10 4.7619 0.23129 0.072539 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 290.78 288.95 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.026011 8.8183e-05 5.047e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.15198 0.66596 0.30086 0.23978 INSTANT 0.548910000E-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 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.33312E-07 0.39108E-02 Friction velocity uk : 0.45085E-05 0.39097E-02 Dimensionless distance yplus : 0.30019E-04 0.26011E-01 Friction thermal sca. tstar : -0.33874E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.21084E-04 0.18269E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.33312E-07 0.39108E-02 Friction velocity uk : 0.45085E-05 0.39097E-02 Dimensionless distance yplus : 0.30019E-04 0.26011E-01 Friction thermal sca. tstar : -0.33874E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.21084E-04 0.18269E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.45269E-08 5 0.22878E-05 0.65678E-10 0.11399E+02 c Velocity[X] 0.71528E-30 c Velocity[Y] 0.32839E-10 c Velocity[Z] 0.32839E-10 c Pressure 0.32123E-12 26 0.25517E-07 0.26348E-05 0.14287E+02 c k 0.19842E-05 3 0.24995E-06 0.15763E-05 0.66700E+01 c omega 0.13153E+02 1 0.44878E-07 0.94531E+02 0.50615E-01 c TempK 0.94218E+02 2 0.11449E-06 0.92164E+00 0.10710E+00 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -2.7028e-13 2.0639e-13 -3.3899e-17 -8.3708e-18 v Velocity[Y] -0.0002314 0.00022974 -1.5643e-10 -6.443e-12 v Velocity[Z] -0.00022974 0.0002314 1.4761e-10 -3.0754e-12 v ǁVelocityǁ 2.5577e-11 0.00027844 1.3319e-05 6.1062e-06 v Pressure -9.2149e-05 0.0059289 0.00019182 2.4146e-21 v k 2.0477e-07 0.0082747 0.0053741 0.005931 v omega 63.395 1.0313e+05 2701.1 543.23 v TempK 288 339.99 290.57 288.81 v Density 1.205 1.205 1.205 1.205 v TurbVisc 2.4507e-12 0.0001508 9.2876e-05 0.00010831 v CourantNb 2.2199e-10 0.00039259 2.092e-05 9.4528e-06 v FourierNb 0.15194 0.66021 0.29985 0.23923 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.7614 4.7614 0.00022831 1.6015e-08 v volume_forces[Z] -4.7614 4.7614 -0.00022828 -5.4171e-09 v ǁvolume_forcesǁ 9.0489e-10 4.7641 0.23277 0.073169 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 290.8 288.96 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.026011 8.8178e-05 5.0465e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.15194 0.66021 0.29987 0.23924 INSTANT 0.558540000E-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 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.45642E-07 0.39105E-02 Friction velocity uk : 0.44361E-05 0.39094E-02 Dimensionless distance yplus : 0.29537E-04 0.26010E-01 Friction thermal sca. tstar : -0.32036E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.20745E-04 0.18268E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.45642E-07 0.39105E-02 Friction velocity uk : 0.44361E-05 0.39094E-02 Dimensionless distance yplus : 0.29537E-04 0.26010E-01 Friction thermal sca. tstar : -0.32036E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.20745E-04 0.18268E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.45714E-08 5 0.22977E-05 0.62568E-10 0.11029E+02 c Velocity[X] 0.60426E-30 c Velocity[Y] 0.31284E-10 c Velocity[Z] 0.31284E-10 c Pressure 0.31357E-12 26 0.24846E-07 0.25704E-05 0.14057E+02 c k 0.19726E-05 3 0.24505E-06 0.15409E-05 0.66352E+01 c omega 0.13153E+02 1 0.44026E-07 0.92153E+02 0.49974E-01 c TempK 0.94218E+02 2 0.11183E-06 0.89809E+00 0.10572E+00 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -2.705e-13 2.0692e-13 -3.3697e-17 -8.3217e-18 v Velocity[Y] -0.00023233 0.00023069 -1.6091e-10 -6.4199e-12 v Velocity[Z] -0.00023069 0.00023234 1.523e-10 -2.9713e-12 v ǁVelocityǁ 2.6134e-11 0.00027957 1.3439e-05 6.1726e-06 v Pressure -9.3771e-05 0.0059828 0.00019455 1.6056e-20 v k 2.0002e-07 0.0082097 0.0053367 0.0058948 v omega 63.079 1.0313e+05 2701 542.97 v TempK 288 340.01 290.58 288.82 v Density 1.205 1.205 1.205 1.205 v TurbVisc 2.3936e-12 0.00015029 9.267e-05 0.00010816 v CourantNb 2.259e-10 0.00039551 2.1097e-05 9.5483e-06 v FourierNb 0.15189 0.65515 0.29889 0.2387 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.7636 4.7635 0.00022975 1.5862e-08 v volume_forces[Z] -4.7636 4.7635 -0.00022971 -5.2152e-09 v ǁvolume_forcesǁ 9.2462e-10 4.7662 0.23423 0.073794 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 290.81 288.96 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.02601 8.8168e-05 5.0458e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.15189 0.65515 0.29891 0.23871 INSTANT 0.568170000E-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 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.63718E-07 0.39100E-02 Friction velocity uk : 0.43685E-05 0.39090E-02 Dimensionless distance yplus : 0.29086E-04 0.26007E-01 Friction thermal sca. tstar : -0.30448E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.20428E-04 0.18265E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.63718E-07 0.39100E-02 Friction velocity uk : 0.43685E-05 0.39090E-02 Dimensionless distance yplus : 0.29086E-04 0.26007E-01 Friction thermal sca. tstar : -0.30448E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.20428E-04 0.18265E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.46148E-08 5 0.21778E-05 0.59584E-10 0.10672E+02 c Velocity[X] 0.50863E-30 c Velocity[Y] 0.29792E-10 c Velocity[Z] 0.29792E-10 c Pressure 0.30602E-12 26 0.24203E-07 0.25070E-05 0.13834E+02 c k 0.19613E-05 3 0.24037E-06 0.15065E-05 0.66008E+01 c omega 0.13153E+02 1 0.43228E-07 0.89890E+02 0.49357E-01 c TempK 0.94219E+02 2 0.10927E-06 0.87555E+00 0.10438E+00 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -2.7068e-13 2.074e-13 -3.3496e-17 -8.273e-18 v Velocity[Y] -0.00023321 0.00023158 -1.6537e-10 -6.3325e-12 v Velocity[Z] -0.00023158 0.00023321 1.5696e-10 -2.951e-12 v ǁVelocityǁ 2.6677e-11 0.00028064 1.3555e-05 6.2374e-06 v Pressure -9.5396e-05 0.0060364 0.00019727 -6.4715e-21 v k 1.9542e-07 0.0081454 0.0052999 0.0058591 v omega 62.767 1.0313e+05 2700.8 542.71 v TempK 288 340.04 290.6 288.82 v Density 1.205 1.205 1.205 1.205 v TurbVisc 2.3381e-12 0.00014977 9.2466e-05 0.00010802 v CourantNb 2.2985e-10 0.00039831 2.1269e-05 9.6412e-06 v FourierNb 0.15185 0.65016 0.29794 0.23818 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.7657 4.7656 0.00023117 1.5715e-08 v volume_forces[Z] -4.7657 4.7656 -0.00023114 -5.0181e-09 v ǁvolume_forcesǁ 9.4474e-10 4.7683 0.23567 0.074414 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 290.83 288.97 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.026007 8.8153e-05 5.0447e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.15185 0.65016 0.29796 0.23819 INSTANT 0.577800000E-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 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.76603E-07 0.39093E-02 Friction velocity uk : 0.43000E-05 0.39083E-02 Dimensionless distance yplus : 0.28631E-04 0.26002E-01 Friction thermal sca. tstar : -0.29045E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.20108E-04 0.18262E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.76603E-07 0.39093E-02 Friction velocity uk : 0.43000E-05 0.39083E-02 Dimensionless distance yplus : 0.28631E-04 0.26002E-01 Friction thermal sca. tstar : -0.29045E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.20108E-04 0.18262E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.46570E-08 5 0.21973E-05 0.56722E-10 0.10328E+02 c Velocity[X] 0.42681E-30 c Velocity[Y] 0.28361E-10 c Velocity[Z] 0.28361E-10 c Pressure 0.29876E-12 26 0.23576E-07 0.24461E-05 0.13619E+02 c k 0.19500E-05 3 0.23589E-06 0.14729E-05 0.65666E+01 c omega 0.13153E+02 1 0.42479E-07 0.87734E+02 0.48761E-01 c TempK 0.94220E+02 2 0.10680E-06 0.85397E+00 0.10309E+00 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -2.7082e-13 2.0785e-13 -3.3297e-17 -8.2246e-18 v Velocity[Y] -0.00023403 0.00023242 -1.699e-10 -6.2787e-12 v Velocity[Z] -0.00023242 0.00023403 1.617e-10 -2.8842e-12 v ǁVelocityǁ 2.724e-11 0.00028164 1.3668e-05 6.3005e-06 v Pressure -9.7025e-05 0.0060895 0.00019998 1.4328e-20 v k 1.9095e-07 0.0080819 0.0052634 0.0058237 v omega 62.458 1.0313e+05 2700.6 542.46 v TempK 288 340.06 290.61 288.83 v Density 1.205 1.205 1.205 1.205 v TurbVisc 2.2843e-12 0.00014926 9.2265e-05 0.00010787 v CourantNb 2.3379e-10 0.00040101 2.1435e-05 9.7316e-06 v FourierNb 0.1518 0.64525 0.297 0.23767 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.7677 4.7677 0.00023258 1.557e-08 v volume_forces[Z] -4.7677 4.7677 -0.00023254 -4.8297e-09 v ǁvolume_forcesǁ 9.6438e-10 4.7704 0.2371 0.075029 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 290.84 288.98 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.026002 8.8132e-05 5.0433e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.15181 0.64525 0.29702 0.23768 INSTANT 0.587430000E-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 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.93915E-07 0.39084E-02 Friction velocity uk : 0.42356E-05 0.39073E-02 Dimensionless distance yplus : 0.28201E-04 0.25996E-01 Friction thermal sca. tstar : -0.27798E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.19807E-04 0.18258E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.93915E-07 0.39084E-02 Friction velocity uk : 0.42356E-05 0.39073E-02 Dimensionless distance yplus : 0.28201E-04 0.25996E-01 Friction thermal sca. tstar : -0.27798E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.19807E-04 0.18258E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.46982E-08 5 0.21523E-05 0.53978E-10 0.99962E+01 c Velocity[X] 0.35731E-30 c Velocity[Y] 0.26989E-10 c Velocity[Z] 0.26989E-10 c Pressure 0.29177E-12 26 0.22972E-07 0.23875E-05 0.13410E+02 c k 0.19388E-05 3 0.23160E-06 0.14403E-05 0.65327E+01 c omega 0.13153E+02 1 0.41774E-07 0.85676E+02 0.48186E-01 c TempK 0.94221E+02 2 0.10443E-06 0.83328E+00 0.10183E+00 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -2.7091e-13 2.0826e-13 -3.3099e-17 -8.1767e-18 v Velocity[Y] -0.0002348 0.00023321 -1.7446e-10 -6.2093e-12 v Velocity[Z] -0.00023321 0.0002348 1.6647e-10 -2.8423e-12 v ǁVelocityǁ 2.78e-11 0.00028257 1.3777e-05 6.3621e-06 v Pressure -9.8656e-05 0.0061422 0.00020268 3.3093e-22 v k 1.866e-07 0.0080192 0.0052274 0.0057887 v omega 62.151 1.0313e+05 2700.5 542.2 v TempK 288 340.08 290.63 288.84 v Density 1.205 1.205 1.205 1.205 v TurbVisc 2.232e-12 0.00014875 9.2067e-05 0.00010773 v CourantNb 2.3775e-10 0.0004036 2.1596e-05 9.8195e-06 v FourierNb 0.15176 0.64043 0.29609 0.23716 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.7697 4.7697 0.00023397 1.543e-08 v volume_forces[Z] -4.7697 4.7697 -0.00023393 -4.6461e-09 v ǁvolume_forcesǁ 9.8471e-10 4.7724 0.23851 0.07564 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 290.86 288.98 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.025996 8.8106e-05 5.0416e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.15176 0.64043 0.29611 0.23717 INSTANT 0.597060000E-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 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11003E-06 0.39072E-02 Friction velocity uk : 0.41722E-05 0.39062E-02 Dimensionless distance yplus : 0.27780E-04 0.25988E-01 Friction thermal sca. tstar : -0.26680E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.19511E-04 0.18252E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11003E-06 0.39072E-02 Friction velocity uk : 0.41722E-05 0.39062E-02 Dimensionless distance yplus : 0.27780E-04 0.25988E-01 Friction thermal sca. tstar : -0.26680E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.19511E-04 0.18252E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.47382E-08 5 0.20348E-05 0.51349E-10 0.96764E+01 c Velocity[X] 0.29894E-30 c Velocity[Y] 0.25675E-10 c Velocity[Z] 0.25675E-10 c Pressure 0.28489E-12 26 0.22435E-07 0.23299E-05 0.13207E+02 c k 0.19278E-05 3 0.22749E-06 0.14084E-05 0.64991E+01 c omega 0.13153E+02 1 0.41108E-07 0.83708E+02 0.47629E-01 c TempK 0.94222E+02 2 0.10213E-06 0.81343E+00 0.10061E+00 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -2.7097e-13 2.0863e-13 -3.2903e-17 -8.1291e-18 v Velocity[Y] -0.00023552 0.00023395 -1.7983e-10 -6.8584e-12 v Velocity[Z] -0.00023395 0.00023552 1.7094e-10 -3.1246e-12 v ǁVelocityǁ 2.8891e-11 0.00028345 1.3883e-05 6.4222e-06 v Pressure -0.00010029 0.0061945 0.00020538 -7.0475e-21 v k 1.8239e-07 0.0079572 0.0051919 0.0057541 v omega 61.848 1.0313e+05 2700.3 541.95 v TempK 288 340.1 290.64 288.84 v Density 1.205 1.205 1.205 1.205 v TurbVisc 2.1813e-12 0.00014824 9.1871e-05 0.00010759 v CourantNb 2.4177e-10 0.00040609 2.1751e-05 9.905e-06 v FourierNb 0.15172 0.63567 0.29519 0.23666 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.7717 4.7716 0.00023534 1.5294e-08 v volume_forces[Z] -4.7717 4.7716 -0.0002353 -4.4691e-09 v ǁvolume_forcesǁ 1.005e-09 4.7743 0.2399 0.076246 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 290.87 288.99 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.025988 8.8075e-05 5.0396e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.15172 0.63567 0.29521 0.23667 INSTANT 0.606690000E-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 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.21188E-06 0.39059E-02 Friction velocity uk : 0.41543E-05 0.39048E-02 Dimensionless distance yplus : 0.27661E-04 0.25979E-01 Friction thermal sca. tstar : -0.25670E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.19427E-04 0.18246E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.21188E-06 0.39059E-02 Friction velocity uk : 0.41543E-05 0.39048E-02 Dimensionless distance yplus : 0.27661E-04 0.25979E-01 Friction thermal sca. tstar : -0.25670E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.19427E-04 0.18246E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.47771E-08 5 0.19931E-05 0.48830E-10 0.93678E+01 c Velocity[X] 0.25063E-30 c Velocity[Y] 0.24415E-10 c Velocity[Z] 0.24415E-10 c Pressure 0.27824E-12 26 0.21862E-07 0.22743E-05 0.13010E+02 c k 0.19168E-05 3 0.22354E-06 0.13775E-05 0.64658E+01 c omega 0.13153E+02 1 0.40478E-07 0.81823E+02 0.47090E-01 c TempK 0.94223E+02 2 0.99915E-07 0.79438E+00 0.99418E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -2.71e-13 2.0907e-13 -3.2708e-17 -8.0819e-18 v Velocity[Y] -0.00023619 0.00023464 -1.8448e-10 -6.7919e-12 v Velocity[Z] -0.00023464 0.00023619 1.7581e-10 -3.0815e-12 v ǁVelocityǁ 2.9521e-11 0.00028426 1.3985e-05 6.4807e-06 v Pressure -0.00010193 0.0062464 0.00020806 1.1834e-20 v k 1.7829e-07 0.0078959 0.0051567 0.0057198 v omega 61.548 1.0313e+05 2700.1 541.7 v TempK 288 340.12 290.66 288.85 v Density 1.205 1.205 1.205 1.205 v TurbVisc 2.132e-12 0.00014773 9.1678e-05 0.00010745 v CourantNb 2.4564e-10 0.00040847 2.1901e-05 9.988e-06 v FourierNb 0.15168 0.63099 0.2943 0.23617 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.7736 4.7735 0.0002367 1.5149e-08 v volume_forces[Z] -4.7736 4.7735 -0.00023666 -4.272e-09 v ǁvolume_forcesǁ 1.0444e-09 4.7762 0.24128 0.076847 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 290.89 289 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.025979 8.804e-05 5.0374e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.15168 0.63099 0.29432 0.23618 INSTANT 0.616320000E-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 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.23048E-06 0.39043E-02 Friction velocity uk : 0.40957E-05 0.39033E-02 Dimensionless distance yplus : 0.27270E-04 0.25969E-01 Friction thermal sca. tstar : -0.24753E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.19153E-04 0.18239E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.23048E-06 0.39043E-02 Friction velocity uk : 0.40957E-05 0.39033E-02 Dimensionless distance yplus : 0.27270E-04 0.25969E-01 Friction thermal sca. tstar : -0.24753E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.19153E-04 0.18239E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.48149E-08 5 0.19536E-05 0.46418E-10 0.90699E+01 c Velocity[X] 0.21131E-30 c Velocity[Y] 0.23209E-10 c Velocity[Z] 0.23209E-10 c Pressure 0.27181E-12 26 0.21306E-07 0.22205E-05 0.12819E+02 c k 0.19060E-05 3 0.21974E-06 0.13473E-05 0.64328E+01 c omega 0.13153E+02 1 0.39880E-07 0.80016E+02 0.46567E-01 c TempK 0.94224E+02 2 0.97777E-07 0.77608E+00 0.98264E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -2.7098e-13 2.0961e-13 -3.2516e-17 -8.0351e-18 v Velocity[Y] -0.00023681 0.00023528 -1.8916e-10 -6.7059e-12 v Velocity[Z] -0.00023528 0.00023681 1.8069e-10 -3.0644e-12 v ǁVelocityǁ 3.0126e-11 0.00028503 1.4085e-05 6.5376e-06 v Pressure -0.00010357 0.006298 0.00021074 -1.2618e-20 v k 1.7431e-07 0.0078353 0.005122 0.005686 v omega 61.25 1.0313e+05 2699.9 541.45 v TempK 288 340.14 290.67 288.86 v Density 1.205 1.205 1.205 1.205 v TurbVisc 2.0841e-12 0.00014721 9.1487e-05 0.00010731 v CourantNb 2.4962e-10 0.00041076 2.2047e-05 1.0069e-05 v FourierNb 0.15163 0.62818 0.29343 0.23568 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.7754 4.7754 0.00023804 1.502e-08 v volume_forces[Z] -4.7754 4.7754 -0.00023801 -4.1063e-09 v ǁvolume_forcesǁ 1.0672e-09 4.7781 0.24264 0.077444 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 290.9 289 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.025969 8.8e-05 5.0349e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.15163 0.62818 0.29345 0.23569 INSTANT 0.625950000E-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 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.24851E-06 0.39026E-02 Friction velocity uk : 0.40384E-05 0.39016E-02 Dimensionless distance yplus : 0.26889E-04 0.25957E-01 Friction thermal sca. tstar : -0.23915E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.18885E-04 0.18231E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.24851E-06 0.39026E-02 Friction velocity uk : 0.40384E-05 0.39016E-02 Dimensionless distance yplus : 0.26889E-04 0.25957E-01 Friction thermal sca. tstar : -0.23915E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.18885E-04 0.18231E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.48517E-08 5 0.19172E-05 0.44109E-10 0.87821E+01 c Velocity[X] 0.18001E-30 c Velocity[Y] 0.22054E-10 c Velocity[Z] 0.22054E-10 c Pressure 0.26576E-12 26 0.20777E-07 0.21700E-05 0.12633E+02 c k 0.18953E-05 3 0.21609E-06 0.13179E-05 0.64000E+01 c omega 0.13153E+02 1 0.39311E-07 0.78281E+02 0.46059E-01 c TempK 0.94225E+02 2 0.95711E-07 0.75850E+00 0.97142E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -2.7094e-13 2.1012e-13 -3.2325e-17 -7.9888e-18 v Velocity[Y] -0.00023739 0.00023588 -1.9389e-10 -6.6389e-12 v Velocity[Z] -0.00023588 0.00023739 1.8563e-10 -3.0212e-12 v ǁVelocityǁ 3.0742e-11 0.00028573 1.4181e-05 6.5931e-06 v Pressure -0.00010521 0.0063491 0.00021341 2.4446e-20 v k 1.7045e-07 0.0077754 0.0050877 0.0056524 v omega 60.956 1.0313e+05 2699.8 541.2 v TempK 288 340.16 290.69 288.86 v Density 1.205 1.205 1.205 1.205 v TurbVisc 2.0376e-12 0.0001467 9.1298e-05 0.00010717 v CourantNb 2.536e-10 0.00041296 2.2187e-05 1.0147e-05 v FourierNb 0.15159 0.62818 0.29258 0.23521 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.7772 4.7772 0.00023937 1.4894e-08 v volume_forces[Z] -4.7772 4.7772 -0.00023934 -3.9468e-09 v ǁvolume_forcesǁ 1.089e-09 4.7799 0.24399 0.078037 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 290.92 289.01 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.025957 8.7956e-05 5.0322e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.15159 0.62818 0.2926 0.23522 INSTANT 0.635580000E-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 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.26917E-06 0.39006E-02 Friction velocity uk : 0.39841E-05 0.38996E-02 Dimensionless distance yplus : 0.26527E-04 0.25945E-01 Friction thermal sca. tstar : -0.23147E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.18631E-04 0.18222E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.26917E-06 0.39006E-02 Friction velocity uk : 0.39841E-05 0.38996E-02 Dimensionless distance yplus : 0.26527E-04 0.25945E-01 Friction thermal sca. tstar : -0.23147E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.18631E-04 0.18222E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.48874E-08 5 0.18826E-05 0.41899E-10 0.85041E+01 c Velocity[X] 0.15595E-30 c Velocity[Y] 0.20950E-10 c Velocity[Z] 0.20950E-10 c Pressure 0.25960E-12 26 0.20255E-07 0.21186E-05 0.12452E+02 c k 0.18847E-05 3 0.21257E-06 0.12893E-05 0.63675E+01 c omega 0.13153E+02 1 0.38768E-07 0.76612E+02 0.45566E-01 c TempK 0.94226E+02 2 0.93715E-07 0.74158E+00 0.96051E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -2.7086e-13 2.1058e-13 -3.2135e-17 -7.9428e-18 v Velocity[Y] -0.00023792 0.00023644 -1.9866e-10 -6.5742e-12 v Velocity[Z] -0.00023644 0.00023792 1.9062e-10 -2.9807e-12 v ǁVelocityǁ 3.1358e-11 0.00028639 1.4274e-05 6.6471e-06 v Pressure -0.00010685 0.0063999 0.00021607 -1.3151e-20 v k 1.667e-07 0.0077162 0.0050538 0.0056193 v omega 60.664 1.0313e+05 2699.6 540.96 v TempK 288 340.18 290.7 288.87 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.9924e-12 0.00014619 9.1111e-05 0.00010703 v CourantNb 2.5759e-10 0.00041505 2.2322e-05 1.0223e-05 v FourierNb 0.15155 0.62817 0.29173 0.23473 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.779 4.7789 0.00024069 1.4772e-08 v volume_forces[Z] -4.779 4.7789 -0.00024065 -3.7919e-09 v ǁvolume_forcesǁ 1.1113e-09 4.7817 0.24533 0.078626 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 290.93 289.02 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.025945 8.7908e-05 5.0292e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.15155 0.62817 0.29176 0.23474 INSTANT 0.645210000E-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 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.29011E-06 0.38985E-02 Friction velocity uk : 0.39314E-05 0.38975E-02 Dimensionless distance yplus : 0.26176E-04 0.25931E-01 Friction thermal sca. tstar : -0.22440E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.18384E-04 0.18212E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.29011E-06 0.38985E-02 Friction velocity uk : 0.39314E-05 0.38975E-02 Dimensionless distance yplus : 0.26176E-04 0.25931E-01 Friction thermal sca. tstar : -0.22440E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.18384E-04 0.18212E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.49221E-08 5 0.18505E-05 0.39786E-10 0.82355E+01 c Velocity[X] 0.13835E-30 c Velocity[Y] 0.19893E-10 c Velocity[Z] 0.19893E-10 c Pressure 0.25376E-12 26 0.19754E-07 0.20699E-05 0.12277E+02 c k 0.18743E-05 3 0.20918E-06 0.12614E-05 0.63353E+01 c omega 0.13153E+02 1 0.38250E-07 0.75006E+02 0.45086E-01 c TempK 0.94227E+02 2 0.91786E-07 0.72530E+00 0.94988E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -2.7075e-13 2.1101e-13 -3.1948e-17 -7.8973e-18 v Velocity[Y] -0.00023842 0.00023695 -2.0362e-10 -6.6505e-12 v Velocity[Z] -0.00023695 0.00023842 1.9554e-10 -3.0417e-12 v ǁVelocityǁ 3.2022e-11 0.00028699 1.4364e-05 6.6997e-06 v Pressure -0.0001085 0.0064503 0.00021872 -2.6107e-21 v k 1.6305e-07 0.0076612 0.0050203 0.0055865 v omega 60.375 1.0313e+05 2699.4 540.71 v TempK 288 340.2 290.72 288.88 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.9485e-12 0.00014569 9.0927e-05 0.0001069 v CourantNb 2.6153e-10 0.00041706 2.2453e-05 1.0297e-05 v FourierNb 0.15151 0.62817 0.29091 0.23427 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.7807 4.7807 0.00024199 1.4653e-08 v volume_forces[Z] -4.7807 4.7807 -0.00024195 -3.6421e-09 v ǁvolume_forcesǁ 1.1336e-09 4.7834 0.24664 0.079211 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 290.95 289.02 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.025931 8.7856e-05 5.0261e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.15151 0.62817 0.29093 0.23428 INSTANT 0.654840000E-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 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.31667E-06 0.38962E-02 Friction velocity uk : 0.38831E-05 0.38953E-02 Dimensionless distance yplus : 0.25855E-04 0.25916E-01 Friction thermal sca. tstar : -0.21785E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.18159E-04 0.18201E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.31667E-06 0.38962E-02 Friction velocity uk : 0.38831E-05 0.38953E-02 Dimensionless distance yplus : 0.25855E-04 0.25916E-01 Friction thermal sca. tstar : -0.21785E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.18159E-04 0.18201E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.49558E-08 5 0.18190E-05 0.37765E-10 0.79757E+01 c Velocity[X] 0.12650E-30 c Velocity[Y] 0.18883E-10 c Velocity[Z] 0.18883E-10 c Pressure 0.24816E-12 26 0.19270E-07 0.20233E-05 0.12106E+02 c k 0.18639E-05 3 0.20591E-06 0.12342E-05 0.63033E+01 c omega 0.13153E+02 1 0.37752E-07 0.73458E+02 0.44618E-01 c TempK 0.94228E+02 2 0.89920E-07 0.70962E+00 0.93953E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -2.7061e-13 2.1141e-13 -3.1762e-17 -7.8522e-18 v Velocity[Y] -0.00023887 0.00023743 -2.0847e-10 -6.5886e-12 v Velocity[Z] -0.00023743 0.00023887 2.0061e-10 -3.0005e-12 v ǁVelocityǁ 3.2686e-11 0.00028754 1.4451e-05 6.7508e-06 v Pressure -0.00011015 0.0065004 0.00022136 -2.512e-20 v k 1.595e-07 0.007607 0.0049872 0.005554 v omega 60.089 1.0313e+05 2699.2 540.47 v TempK 288 340.21 290.73 288.88 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.9059e-12 0.00014518 9.0745e-05 0.00010676 v CourantNb 2.6552e-10 0.00041898 2.2578e-05 1.0368e-05 v FourierNb 0.15147 0.62817 0.29009 0.23381 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.7824 4.7824 0.00024328 1.4534e-08 v volume_forces[Z] -4.7824 4.7824 -0.00024324 -3.4923e-09 v ǁvolume_forcesǁ 1.1576e-09 4.7851 0.24795 0.079791 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 290.96 289.03 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.025916 8.78e-05 5.0227e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.15147 0.62817 0.29012 0.23382 INSTANT 0.664470000E-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 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.34356E-06 0.38938E-02 Friction velocity uk : 0.38365E-05 0.38929E-02 Dimensionless distance yplus : 0.25545E-04 0.25899E-01 Friction thermal sca. tstar : -0.21493E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.17941E-04 0.18190E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.34356E-06 0.38938E-02 Friction velocity uk : 0.38365E-05 0.38929E-02 Dimensionless distance yplus : 0.25545E-04 0.25899E-01 Friction thermal sca. tstar : -0.21493E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.17941E-04 0.18190E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.49885E-08 5 0.17897E-05 0.35834E-10 0.77245E+01 c Velocity[X] 0.11980E-30 c Velocity[Y] 0.17917E-10 c Velocity[Z] 0.17917E-10 c Pressure 0.24269E-12 26 0.18790E-07 0.19777E-05 0.11940E+02 c k 0.18536E-05 3 0.20275E-06 0.12077E-05 0.62717E+01 c omega 0.13153E+02 1 0.37275E-07 0.71964E+02 0.44162E-01 c TempK 0.94229E+02 2 0.88115E-07 0.69451E+00 0.92946E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -2.7045e-13 2.1177e-13 -3.1578e-17 -7.8075e-18 v Velocity[Y] -0.00023928 0.00023786 -2.1336e-10 -6.5274e-12 v Velocity[Z] -0.00023786 0.00023928 2.0571e-10 -2.9619e-12 v ǁVelocityǁ 3.3338e-11 0.00028805 1.4535e-05 6.8004e-06 v Pressure -0.0001118 0.0065501 0.00022399 -4.5288e-21 v k 1.5606e-07 0.0075533 0.0049545 0.0055219 v omega 59.805 1.0313e+05 2699.1 540.23 v TempK 288 340.23 290.74 288.89 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.8644e-12 0.00014468 9.0565e-05 0.00010663 v CourantNb 2.6953e-10 0.00042081 2.27e-05 1.0438e-05 v FourierNb 0.15143 0.62817 0.28929 0.23336 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.7841 4.784 0.00024455 1.4422e-08 v volume_forces[Z] -4.7841 4.784 -0.00024451 -3.3522e-09 v ǁvolume_forcesǁ 1.1816e-09 4.7867 0.24924 0.080368 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 290.98 289.03 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.025899 8.7741e-05 5.0191e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.15143 0.62817 0.28931 0.23337 INSTANT 0.674100000E-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 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.36895E-06 0.38912E-02 Friction velocity uk : 0.37906E-05 0.38903E-02 Dimensionless distance yplus : 0.25239E-04 0.25882E-01 Friction thermal sca. tstar : -0.21697E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.17726E-04 0.18178E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.36895E-06 0.38912E-02 Friction velocity uk : 0.37906E-05 0.38903E-02 Dimensionless distance yplus : 0.25239E-04 0.25882E-01 Friction thermal sca. tstar : -0.21697E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.17726E-04 0.18178E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.50202E-08 5 0.17672E-05 0.33989E-10 0.74815E+01 c Velocity[X] 0.11769E-30 c Velocity[Y] 0.16994E-10 c Velocity[Z] 0.16994E-10 c Pressure 0.23742E-12 29 0.19784E-07 0.19339E-05 0.11778E+02 c k 0.18434E-05 3 0.19969E-06 0.11819E-05 0.62403E+01 c omega 0.13153E+02 1 0.36815E-07 0.70522E+02 0.43717E-01 c TempK 0.94229E+02 2 0.86368E-07 0.67994E+00 0.91964E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -2.7025e-13 2.1209e-13 -3.1395e-17 -7.7632e-18 v Velocity[Y] -0.00023966 0.00023826 -2.1925e-10 -7.5261e-12 v Velocity[Z] -0.00023826 0.00023966 2.1093e-10 -2.7344e-12 v ǁVelocityǁ 3.3909e-11 0.00028851 1.4616e-05 6.8487e-06 v Pressure -0.00011345 0.0065995 0.00022662 -1.5725e-20 v k 1.5271e-07 0.0075001 0.0049221 0.0054901 v omega 59.524 1.0313e+05 2698.9 539.99 v TempK 288 340.25 290.76 288.89 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.8241e-12 0.00014426 9.0387e-05 0.0001065 v CourantNb 2.7509e-10 0.00042256 2.2816e-05 1.0505e-05 v FourierNb 0.15139 0.62817 0.2885 0.23291 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.7857 4.7857 0.00024581 1.4313e-08 v volume_forces[Z] -4.7857 4.7857 -0.00024577 -3.2169e-09 v ǁvolume_forcesǁ 1.2052e-09 4.7884 0.25052 0.080941 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 290.99 289.04 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.025882 8.7678e-05 5.0153e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.15139 0.62817 0.28853 0.23292 INSTANT 0.683730000E-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 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.39877E-06 0.38885E-02 Friction velocity uk : 0.37484E-05 0.38876E-02 Dimensionless distance yplus : 0.24958E-04 0.25864E-01 Friction thermal sca. tstar : -0.21913E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.17529E-04 0.18165E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.39877E-06 0.38885E-02 Friction velocity uk : 0.37484E-05 0.38876E-02 Dimensionless distance yplus : 0.24958E-04 0.25864E-01 Friction thermal sca. tstar : -0.21913E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.17529E-04 0.18165E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.50509E-08 5 0.17367E-05 0.32226E-10 0.72464E+01 c Velocity[X] 0.11959E-30 c Velocity[Y] 0.16113E-10 c Velocity[Z] 0.16113E-10 c Pressure 0.23241E-12 29 0.19433E-07 0.18922E-05 0.11621E+02 c k 0.18334E-05 3 0.19673E-06 0.11568E-05 0.62092E+01 c omega 0.13153E+02 1 0.36372E-07 0.69127E+02 0.43283E-01 c TempK 0.94230E+02 2 0.84677E-07 0.66589E+00 0.91006E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -2.7004e-13 2.1239e-13 -3.1214e-17 -7.7193e-18 v Velocity[Y] -0.00023999 0.00023862 -2.242e-10 -7.4472e-12 v Velocity[Z] -0.00023862 0.00024 2.1612e-10 -2.6791e-12 v ǁVelocityǁ 3.4525e-11 0.00028893 1.4694e-05 6.8956e-06 v Pressure -0.0001151 0.0066486 0.00022924 1.6485e-20 v k 1.4945e-07 0.0074475 0.0048902 0.0054586 v omega 59.246 1.0313e+05 2698.7 539.75 v TempK 288 340.27 290.77 288.9 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.785e-12 0.00014389 9.0211e-05 0.00010637 v CourantNb 2.7908e-10 0.00042423 2.2929e-05 1.057e-05 v FourierNb 0.15135 0.62817 0.28773 0.23247 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.7873 4.7873 0.00024706 1.4214e-08 v volume_forces[Z] -4.7873 4.7873 -0.00024702 -3.0478e-09 v ǁvolume_forcesǁ 1.2258e-09 4.79 0.25179 0.08151 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 291 289.05 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.025864 8.7612e-05 5.0113e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.15135 0.62817 0.28775 0.23248 INSTANT 0.693360000E-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 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.42001E-06 0.38856E-02 Friction velocity uk : 0.37031E-05 0.38847E-02 Dimensionless distance yplus : 0.24656E-04 0.25845E-01 Friction thermal sca. tstar : -0.22141E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.17317E-04 0.18152E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.42001E-06 0.38856E-02 Friction velocity uk : 0.37031E-05 0.38847E-02 Dimensionless distance yplus : 0.24656E-04 0.25845E-01 Friction thermal sca. tstar : -0.22141E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.17317E-04 0.18152E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.50807E-08 5 0.17190E-05 0.30544E-10 0.70189E+01 c Velocity[X] 0.12511E-30 c Velocity[Y] 0.15272E-10 c Velocity[Z] 0.15272E-10 c Pressure 0.22740E-12 29 0.19082E-07 0.18506E-05 0.11467E+02 c k 0.18234E-05 3 0.19387E-06 0.11323E-05 0.61784E+01 c omega 0.13153E+02 1 0.35943E-07 0.67778E+02 0.42858E-01 c TempK 0.94231E+02 2 0.83039E-07 0.65232E+00 0.90073E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -2.6979e-13 2.1265e-13 -3.1035e-17 -7.6758e-18 v Velocity[Y] -0.0002403 0.00023894 -2.2919e-10 -7.3797e-12 v Velocity[Z] -0.00023894 0.0002403 2.2132e-10 -2.6513e-12 v ǁVelocityǁ 3.5161e-11 0.0002893 1.477e-05 6.9412e-06 v Pressure -0.00011676 0.0066973 0.00023185 3.248e-20 v k 1.4628e-07 0.0073954 0.0048586 0.0054274 v omega 58.97 1.0313e+05 2698.6 539.52 v TempK 288 340.28 290.79 288.91 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.7469e-12 0.00014352 9.0037e-05 0.00010624 v CourantNb 2.8307e-10 0.00042582 2.3037e-05 1.0633e-05 v FourierNb 0.15131 0.62817 0.28696 0.23203 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.7888 4.7888 0.0002483 1.4111e-08 v volume_forces[Z] -4.7888 4.7888 -0.00024826 -2.9221e-09 v ǁvolume_forcesǁ 1.2481e-09 4.7915 0.25304 0.082076 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 291.02 289.05 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.025845 8.7543e-05 5.0071e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.15131 0.62817 0.28699 0.23204 INSTANT 0.702990000E-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 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.44338E-06 0.38826E-02 Friction velocity uk : 0.36602E-05 0.38817E-02 Dimensionless distance yplus : 0.24371E-04 0.25825E-01 Friction thermal sca. tstar : -0.22381E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.17117E-04 0.18138E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.44338E-06 0.38826E-02 Friction velocity uk : 0.36602E-05 0.38817E-02 Dimensionless distance yplus : 0.24371E-04 0.25825E-01 Friction thermal sca. tstar : -0.22381E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.17117E-04 0.18138E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.51095E-08 5 0.16900E-05 0.28940E-10 0.67987E+01 c Velocity[X] 0.13380E-30 c Velocity[Y] 0.14470E-10 c Velocity[Z] 0.14470E-10 c Pressure 0.22262E-12 29 0.18745E-07 0.18110E-05 0.11318E+02 c k 0.18135E-05 3 0.19109E-06 0.11084E-05 0.61478E+01 c omega 0.13153E+02 1 0.35528E-07 0.66471E+02 0.42443E-01 c TempK 0.94232E+02 2 0.81452E-07 0.63922E+00 0.89162E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -2.6953e-13 2.1288e-13 -3.0858e-17 -7.6327e-18 v Velocity[Y] -0.00024057 0.00023923 -2.3422e-10 -7.31e-12 v Velocity[Z] -0.00023923 0.00024057 2.2656e-10 -2.6144e-12 v ǁVelocityǁ 3.5803e-11 0.0002897 1.4842e-05 6.9854e-06 v Pressure -0.00011842 0.0067457 0.00023445 1.3188e-20 v k 1.432e-07 0.0073439 0.0048273 0.0053966 v omega 58.697 1.0313e+05 2698.4 539.28 v TempK 288 340.3 290.8 288.91 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.7099e-12 0.00014315 8.9865e-05 0.00010611 v CourantNb 2.8706e-10 0.00042733 2.3141e-05 1.0694e-05 v FourierNb 0.15127 0.62816 0.28621 0.2316 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.7904 4.7904 0.00024952 1.4011e-08 v volume_forces[Z] -4.7904 4.7904 -0.00024949 -2.8004e-09 v ǁvolume_forcesǁ 1.2711e-09 4.793 0.25429 0.082638 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 291.03 289.06 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.025825 8.7471e-05 5.0028e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.15127 0.62816 0.28623 0.23161 INSTANT 0.712620000E-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 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.46770E-06 0.38795E-02 Friction velocity uk : 0.36192E-05 0.38786E-02 Dimensionless distance yplus : 0.24097E-04 0.25804E-01 Friction thermal sca. tstar : -0.22635E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.16925E-04 0.18123E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.46770E-06 0.38795E-02 Friction velocity uk : 0.36192E-05 0.38786E-02 Dimensionless distance yplus : 0.24097E-04 0.25804E-01 Friction thermal sca. tstar : -0.22635E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.16925E-04 0.18123E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.51374E-08 5 0.16658E-05 0.27409E-10 0.65855E+01 c Velocity[X] 0.14525E-30 c Velocity[Y] 0.13705E-10 c Velocity[Z] 0.13705E-10 c Pressure 0.21801E-12 29 0.18416E-07 0.17727E-05 0.11172E+02 c k 0.18037E-05 3 0.18840E-06 0.10852E-05 0.61175E+01 c omega 0.13153E+02 1 0.35125E-07 0.65204E+02 0.42037E-01 c TempK 0.94233E+02 2 0.79914E-07 0.62657E+00 0.88273E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -2.6924e-13 2.1308e-13 -3.0682e-17 -7.59e-18 v Velocity[Y] -0.0002408 0.00023977 -2.3928e-10 -7.2415e-12 v Velocity[Z] -0.00023977 0.0002408 2.3184e-10 -2.5794e-12 v ǁVelocityǁ 3.6452e-11 0.00029058 1.4913e-05 7.0283e-06 v Pressure -0.00012008 0.0067938 0.00023705 8.5919e-21 v k 1.4021e-07 0.0072928 0.0047965 0.0053661 v omega 58.426 1.0313e+05 2698.2 539.05 v TempK 288 340.32 290.81 288.92 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.6739e-12 0.00014278 8.9695e-05 0.00010598 v CourantNb 2.9106e-10 0.00042876 2.324e-05 1.0753e-05 v FourierNb 0.15123 0.62816 0.28547 0.23117 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.7919 4.7919 0.00025074 1.3913e-08 v volume_forces[Z] -4.7919 4.7919 -0.0002507 -2.6829e-09 v ǁvolume_forcesǁ 1.2943e-09 4.7945 0.25552 0.083196 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 291.04 289.07 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.025804 8.7395e-05 4.9983e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.15123 0.62816 0.28549 0.23119 INSTANT 0.722250000E-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 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.49280E-06 0.38762E-02 Friction velocity uk : 0.35798E-05 0.38753E-02 Dimensionless distance yplus : 0.23835E-04 0.25783E-01 Friction thermal sca. tstar : -0.22903E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.16740E-04 0.18108E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.49280E-06 0.38762E-02 Friction velocity uk : 0.35798E-05 0.38753E-02 Dimensionless distance yplus : 0.23835E-04 0.25783E-01 Friction thermal sca. tstar : -0.22903E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.16740E-04 0.18108E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.51643E-08 5 0.16445E-05 0.25951E-10 0.63791E+01 c Velocity[X] 0.15911E-30 c Velocity[Y] 0.12975E-10 c Velocity[Z] 0.12975E-10 c Pressure 0.21354E-12 29 0.18104E-07 0.17356E-05 0.11030E+02 c k 0.17941E-05 3 0.18578E-06 0.10625E-05 0.60875E+01 c omega 0.13153E+02 1 0.34734E-07 0.63975E+02 0.41639E-01 c TempK 0.94234E+02 2 0.78423E-07 0.61433E+00 0.87405E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -2.6893e-13 2.1326e-13 -3.0508e-17 -7.5477e-18 v Velocity[Y] -0.00024101 0.00024049 -2.4436e-10 -7.1723e-12 v Velocity[Z] -0.00024049 0.00024101 2.3714e-10 -2.5442e-12 v ǁVelocityǁ 3.7106e-11 0.00029142 1.498e-05 7.07e-06 v Pressure -0.00012174 0.0068416 0.00023963 8.0526e-21 v k 1.373e-07 0.0072422 0.0047659 0.0053359 v omega 58.158 1.0313e+05 2698 538.82 v TempK 288 340.33 290.83 288.93 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.6389e-12 0.00014241 8.9526e-05 0.00010585 v CourantNb 2.9506e-10 0.00043012 2.3336e-05 1.081e-05 v FourierNb 0.15119 0.62816 0.28474 0.23075 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.7933 4.7933 0.00025194 1.3818e-08 v volume_forces[Z] -4.7933 4.7933 -0.0002519 -2.5694e-09 v ǁvolume_forcesǁ 1.3177e-09 4.796 0.25673 0.083751 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 291.06 289.07 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.025783 8.7317e-05 4.9936e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.15119 0.62816 0.28476 0.23077 INSTANT 0.731880000E-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 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.51861E-06 0.38728E-02 Friction velocity uk : 0.35421E-05 0.38719E-02 Dimensionless distance yplus : 0.23584E-04 0.25760E-01 Friction thermal sca. tstar : -0.23187E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.16564E-04 0.18092E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.51861E-06 0.38728E-02 Friction velocity uk : 0.35421E-05 0.38719E-02 Dimensionless distance yplus : 0.23584E-04 0.25760E-01 Friction thermal sca. tstar : -0.23187E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.16564E-04 0.18092E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.51904E-08 5 0.16278E-05 0.24561E-10 0.61792E+01 c Velocity[X] 0.17509E-30 c Velocity[Y] 0.12281E-10 c Velocity[Z] 0.12281E-10 c Pressure 0.20927E-12 29 0.17784E-07 0.17003E-05 0.10891E+02 c k 0.17845E-05 3 0.18324E-06 0.10404E-05 0.60577E+01 c omega 0.13153E+02 1 0.34354E-07 0.62782E+02 0.41249E-01 c TempK 0.94235E+02 2 0.76977E-07 0.60250E+00 0.86557E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -2.686e-13 2.1341e-13 -3.0335e-17 -7.5058e-18 v Velocity[Y] -0.0002412 0.00024118 -2.4948e-10 -7.1064e-12 v Velocity[Z] -0.00024118 0.00024121 2.4248e-10 -2.511e-12 v ǁVelocityǁ 3.7765e-11 0.0002922 1.5045e-05 7.1103e-06 v Pressure -0.00012341 0.0068891 0.00024221 -4.5717e-21 v k 1.3446e-07 0.0071922 0.0047357 0.005306 v omega 57.892 1.0313e+05 2697.9 538.59 v TempK 288 340.35 290.84 288.93 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.6048e-12 0.00014204 8.936e-05 0.00010573 v CourantNb 2.9906e-10 0.00043141 2.3428e-05 1.0865e-05 v FourierNb 0.15116 0.62816 0.28402 0.23034 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.7948 4.7948 0.00025313 1.3726e-08 v volume_forces[Z] -4.7948 4.7948 -0.00025309 -2.4599e-09 v ǁvolume_forcesǁ 1.3414e-09 4.7974 0.25794 0.084303 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 291.07 289.08 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.02576 8.7237e-05 4.9888e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.15116 0.62816 0.28405 0.23035 INSTANT 0.741510000E-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 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.54508E-06 0.38693E-02 Friction velocity uk : 0.35059E-05 0.38684E-02 Dimensionless distance yplus : 0.23344E-04 0.25737E-01 Friction thermal sca. tstar : -0.23486E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.16395E-04 0.18076E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.54508E-06 0.38693E-02 Friction velocity uk : 0.35059E-05 0.38684E-02 Dimensionless distance yplus : 0.23344E-04 0.25737E-01 Friction thermal sca. tstar : -0.23486E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.16395E-04 0.18076E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.52156E-08 4 0.17311E-05 0.23240E-10 0.59859E+01 c Velocity[X] 0.18893E-30 c Velocity[Y] 0.11620E-10 c Velocity[Z] 0.11620E-10 c Pressure 0.20233E-12 29 0.17307E-07 0.16432E-05 0.10756E+02 c k 0.17750E-05 3 0.18077E-06 0.10188E-05 0.60282E+01 c omega 0.13153E+02 1 0.33983E-07 0.61623E+02 0.40866E-01 c TempK 0.94236E+02 2 0.75574E-07 0.59105E+00 0.85729E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -2.6825e-13 2.1353e-13 -3.0165e-17 -7.4644e-18 v Velocity[Y] -0.00024183 0.00024182 -2.5463e-10 -7.0382e-12 v Velocity[Z] -0.00024182 0.00024183 2.4785e-10 -2.4768e-12 v ǁVelocityǁ 3.8498e-11 0.00029294 1.5108e-05 7.1494e-06 v Pressure -0.00012507 0.0069363 0.00024478 6.8269e-21 v k 1.317e-07 0.0071426 0.0047059 0.0052764 v omega 57.629 1.0313e+05 2697.7 538.36 v TempK 288 340.36 290.85 288.94 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.5717e-12 0.00014167 8.9195e-05 0.0001056 v CourantNb 3.0307e-10 0.00043262 2.3516e-05 1.0918e-05 v FourierNb 0.15112 0.62816 0.28331 0.22993 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.7962 4.7962 0.00025431 1.3636e-08 v volume_forces[Z] -4.7962 4.7962 -0.00025427 -2.3541e-09 v ǁvolume_forcesǁ 1.3652e-09 4.7989 0.25914 0.084851 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 291.08 289.08 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.025737 8.7154e-05 4.9838e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.15112 0.62816 0.28334 0.22994 INSTANT 0.751140000E-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 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.57782E-06 0.38657E-02 Friction velocity uk : 0.34744E-05 0.38648E-02 Dimensionless distance yplus : 0.23134E-04 0.25713E-01 Friction thermal sca. tstar : -0.23801E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.16248E-04 0.18059E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.57782E-06 0.38657E-02 Friction velocity uk : 0.34744E-05 0.38648E-02 Dimensionless distance yplus : 0.23134E-04 0.25713E-01 Friction thermal sca. tstar : -0.23801E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.16248E-04 0.18059E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.52399E-08 4 0.17047E-05 0.21980E-10 0.57984E+01 c Velocity[X] 0.20945E-30 c Velocity[Y] 0.10990E-10 c Velocity[Z] 0.10990E-10 c Pressure 0.19856E-12 29 0.17020E-07 0.16120E-05 0.10624E+02 c k 0.17656E-05 3 0.17837E-06 0.99780E-06 0.59990E+01 c omega 0.13153E+02 1 0.33621E-07 0.60497E+02 0.40491E-01 c TempK 0.94237E+02 2 0.74212E-07 0.57997E+00 0.84920E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -2.6788e-13 2.1362e-13 -2.9996e-17 -7.4234e-18 v Velocity[Y] -0.00024241 0.00024243 -2.598e-10 -6.9728e-12 v Velocity[Z] -0.00024243 0.00024241 2.5326e-10 -2.4442e-12 v ǁVelocityǁ 3.9201e-11 0.00029363 1.5168e-05 7.1873e-06 v Pressure -0.00012674 0.0069832 0.00024734 9.695e-21 v k 1.2902e-07 0.0070936 0.0046764 0.0052471 v omega 57.368 1.0313e+05 2697.5 538.14 v TempK 288 340.38 290.87 288.94 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.5395e-12 0.0001413 8.9032e-05 0.00010548 v CourantNb 3.0709e-10 0.00043377 2.3601e-05 1.0969e-05 v FourierNb 0.15108 0.62816 0.28262 0.22952 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.7976 4.7976 0.00025548 1.3549e-08 v volume_forces[Z] -4.7976 4.7976 -0.00025544 -2.2521e-09 v ǁvolume_forcesǁ 1.3917e-09 4.8002 0.26032 0.085396 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 291.1 289.09 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.025713 8.7068e-05 4.9787e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.15108 0.62816 0.28264 0.22954 INSTANT 0.760770000E-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 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.60801E-06 0.38620E-02 Friction velocity uk : 0.34427E-05 0.38611E-02 Dimensionless distance yplus : 0.22923E-04 0.25688E-01 Friction thermal sca. tstar : -0.24135E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.16099E-04 0.18042E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.60801E-06 0.38620E-02 Friction velocity uk : 0.34427E-05 0.38611E-02 Dimensionless distance yplus : 0.22923E-04 0.25688E-01 Friction thermal sca. tstar : -0.24135E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.16099E-04 0.18042E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.52633E-08 4 0.16793E-05 0.20782E-10 0.56168E+01 c Velocity[X] 0.23090E-30 c Velocity[Y] 0.10391E-10 c Velocity[Z] 0.10391E-10 c Pressure 0.19484E-12 29 0.16729E-07 0.15811E-05 0.10495E+02 c k 0.17563E-05 3 0.17603E-06 0.97731E-06 0.59700E+01 c omega 0.13153E+02 1 0.33267E-07 0.59402E+02 0.40123E-01 c TempK 0.94238E+02 2 0.72890E-07 0.56924E+00 0.84128E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -2.675e-13 2.1369e-13 -2.9828e-17 -7.3828e-18 v Velocity[Y] -0.00024295 0.00024299 -2.6497e-10 -6.8743e-12 v Velocity[Z] -0.00024299 0.00024295 2.5878e-10 -2.3237e-12 v ǁVelocityǁ 3.988e-11 0.00029427 1.5225e-05 7.224e-06 v Pressure -0.00012841 0.0070298 0.0002499 -7.354e-21 v k 1.2641e-07 0.007045 0.0046472 0.0052181 v omega 57.109 1.0313e+05 2697.4 537.92 v TempK 288 340.39 290.88 288.95 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.5081e-12 0.00014093 8.8871e-05 0.00010536 v CourantNb 3.1112e-10 0.00043486 2.3682e-05 1.1019e-05 v FourierNb 0.15104 0.62816 0.28193 0.22912 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.7989 4.7989 0.00025664 1.3463e-08 v volume_forces[Z] -4.7989 4.7989 -0.0002566 -2.1535e-09 v ǁvolume_forcesǁ 1.4171e-09 4.8016 0.2615 0.085938 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 291.11 289.1 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.025688 8.698e-05 4.9735e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.15104 0.62816 0.28195 0.22913 INSTANT 0.770400000E-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 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.63632E-06 0.38581E-02 Friction velocity uk : 0.34111E-05 0.38573E-02 Dimensionless distance yplus : 0.22712E-04 0.25663E-01 Friction thermal sca. tstar : -0.24489E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.15952E-04 0.18024E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.63632E-06 0.38581E-02 Friction velocity uk : 0.34111E-05 0.38573E-02 Dimensionless distance yplus : 0.22712E-04 0.25663E-01 Friction thermal sca. tstar : -0.24489E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.15952E-04 0.18024E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.52859E-08 4 0.16613E-05 0.19643E-10 0.54410E+01 c Velocity[X] 0.25319E-30 c Velocity[Y] 0.98215E-11 c Velocity[Z] 0.98215E-11 c Pressure 0.19122E-12 29 0.16446E-07 0.15512E-05 0.10369E+02 c k 0.17471E-05 3 0.17375E-06 0.95732E-06 0.59413E+01 c omega 0.13153E+02 1 0.32921E-07 0.58336E+02 0.39761E-01 c TempK 0.94238E+02 2 0.71607E-07 0.55884E+00 0.83355E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -2.6709e-13 2.1373e-13 -2.9663e-17 -7.3425e-18 v Velocity[Y] -0.00024346 0.00024352 -2.7039e-10 -6.9906e-12 v Velocity[Z] -0.00024352 0.00024346 2.642e-10 -2.3359e-12 v ǁVelocityǁ 4.0791e-11 0.00029487 1.5281e-05 7.2595e-06 v Pressure -0.00013009 0.0070762 0.00025245 1.2588e-20 v k 1.2387e-07 0.0069969 0.0046184 0.0051894 v omega 56.853 1.0313e+05 2697.2 537.69 v TempK 288 340.41 290.89 288.96 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.4775e-12 0.00014056 8.8711e-05 0.00010523 v CourantNb 3.1513e-10 0.00043587 2.3759e-05 1.1067e-05 v FourierNb 0.151 0.62816 0.28125 0.22873 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.8003 4.8003 0.00025779 1.3384e-08 v volume_forces[Z] -4.8003 4.8003 -0.00025775 -2.0597e-09 v ǁvolume_forcesǁ 1.4417e-09 4.8029 0.26266 0.086476 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 291.12 289.1 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.025663 8.689e-05 4.9681e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.15101 0.62816 0.28127 0.22874 INSTANT 0.780030000E-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 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.68680E-06 0.38542E-02 Friction velocity uk : 0.33930E-05 0.38534E-02 Dimensionless distance yplus : 0.22592E-04 0.25637E-01 Friction thermal sca. tstar : -0.24864E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.15867E-04 0.18006E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.68680E-06 0.38542E-02 Friction velocity uk : 0.33930E-05 0.38534E-02 Dimensionless distance yplus : 0.22592E-04 0.25637E-01 Friction thermal sca. tstar : -0.24864E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.15867E-04 0.18006E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.53077E-08 4 0.16328E-05 0.18561E-10 0.52707E+01 c Velocity[X] 0.27622E-30 c Velocity[Y] 0.92803E-11 c Velocity[Z] 0.92804E-11 c Pressure 0.18775E-12 29 0.16174E-07 0.15225E-05 0.10246E+02 c k 0.17380E-05 3 0.17154E-06 0.93782E-06 0.59128E+01 c omega 0.13153E+02 1 0.32583E-07 0.57298E+02 0.39406E-01 c TempK 0.94239E+02 2 0.70360E-07 0.54876E+00 0.82598E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -2.6667e-13 2.1376e-13 -2.9498e-17 -7.3026e-18 v Velocity[Y] -0.00024393 0.00024401 -2.7566e-10 -6.9304e-12 v Velocity[Z] -0.00024401 0.00024393 2.697e-10 -2.304e-12 v ǁVelocityǁ 4.1487e-11 0.00029542 1.5334e-05 7.2939e-06 v Pressure -0.00013176 0.0071223 0.00025499 -3.123e-20 v k 1.2139e-07 0.0069492 0.0045899 0.005161 v omega 56.599 1.0313e+05 2697 537.47 v TempK 288 340.42 290.9 288.96 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.4478e-12 0.00014018 8.8553e-05 0.00010511 v CourantNb 3.1914e-10 0.00043683 2.3833e-05 1.1113e-05 v FourierNb 0.15097 0.62815 0.28058 0.22834 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.8016 4.8016 0.00025893 1.3302e-08 v volume_forces[Z] -4.8016 4.8016 -0.00025889 -1.9615e-09 v ǁvolume_forcesǁ 1.4746e-09 4.8043 0.26382 0.087012 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 291.13 289.11 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.025637 8.6797e-05 4.9626e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.15097 0.62815 0.2806 0.22835 INSTANT 0.789660000E-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 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.71623E-06 0.38502E-02 Friction velocity uk : 0.33644E-05 0.38494E-02 Dimensionless distance yplus : 0.22401E-04 0.25610E-01 Friction thermal sca. tstar : -0.25261E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.15733E-04 0.17987E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.71623E-06 0.38502E-02 Friction velocity uk : 0.33644E-05 0.38494E-02 Dimensionless distance yplus : 0.22401E-04 0.25610E-01 Friction thermal sca. tstar : -0.25261E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.15733E-04 0.17987E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.53286E-08 4 0.16115E-05 0.17533E-10 0.51059E+01 c Velocity[X] 0.29989E-30 c Velocity[Y] 0.87665E-11 c Velocity[Z] 0.87665E-11 c Pressure 0.18450E-12 29 0.15919E-07 0.14956E-05 0.10125E+02 c k 0.17289E-05 3 0.16937E-06 0.91881E-06 0.58846E+01 c omega 0.13153E+02 1 0.32251E-07 0.56287E+02 0.39057E-01 c TempK 0.94240E+02 1 0.16340E-05 0.50456E+00 0.79200E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -2.6623e-13 2.1376e-13 -2.9335e-17 -7.263e-18 v Velocity[Y] -0.00024437 0.00024447 -2.8096e-10 -6.8696e-12 v Velocity[Z] -0.00024447 0.00024437 2.7523e-10 -2.2735e-12 v ǁVelocityǁ 4.2187e-11 0.00029593 1.5385e-05 7.3272e-06 v Pressure -0.00013343 0.0071681 0.00025752 -1.2539e-20 v k 1.1898e-07 0.006902 0.0045617 0.0051328 v omega 56.347 1.0313e+05 2696.9 537.25 v TempK 288 340.43 290.92 288.97 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.4189e-12 0.00013981 8.8396e-05 0.00010499 v CourantNb 3.2317e-10 0.00043772 2.3903e-05 1.1157e-05 v FourierNb 0.15093 0.62815 0.27992 0.22795 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.8029 4.8029 0.00026006 1.3223e-08 v volume_forces[Z] -4.8029 4.8029 -0.00026002 -1.8729e-09 v ǁvolume_forcesǁ 1.4998e-09 4.8055 0.26496 0.087544 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 291.15 289.11 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.02561 8.6703e-05 4.957e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.15093 0.62815 0.27994 0.22796 INSTANT 0.799290000E-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 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.74638E-06 0.38461E-02 Friction velocity uk : 0.33372E-05 0.38453E-02 Dimensionless distance yplus : 0.22220E-04 0.25583E-01 Friction thermal sca. tstar : -0.25688E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.15606E-04 0.17968E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.74638E-06 0.38461E-02 Friction velocity uk : 0.33372E-05 0.38453E-02 Dimensionless distance yplus : 0.22220E-04 0.25583E-01 Friction thermal sca. tstar : -0.25688E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.15606E-04 0.17968E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.53487E-08 4 0.15806E-05 0.16535E-10 0.49429E+01 c Velocity[X] 0.32427E-30 c Velocity[Y] 0.82675E-11 c Velocity[Z] 0.82675E-11 c Pressure 0.17939E-12 27 0.16735E-07 0.14537E-05 0.97089E+01 c k 0.17200E-05 3 0.16726E-06 0.90026E-06 0.58567E+01 c omega 0.13153E+02 1 0.31926E-07 0.55302E+02 0.38713E-01 c TempK 0.94241E+02 1 0.16134E-05 0.49625E+00 0.78543E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -2.6578e-13 2.1373e-13 -2.9177e-17 -7.2244e-18 v Velocity[Y] -0.00024477 0.00024489 -2.8615e-10 -6.732e-12 v Velocity[Z] -0.00024489 0.00024477 2.807e-10 -2.2553e-12 v ǁVelocityǁ 4.2897e-11 0.0002964 1.5434e-05 7.3594e-06 v Pressure -0.00013506 0.0072121 0.00025997 8.1752e-21 v k 1.1663e-07 0.0068553 0.0045338 0.005105 v omega 56.098 1.0313e+05 2696.7 537.04 v TempK 288 340.45 290.93 288.97 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.3907e-12 0.00013944 8.8241e-05 0.00010487 v CourantNb 3.268e-10 0.00043856 2.397e-05 1.12e-05 v FourierNb 0.15089 0.62815 0.27927 0.22757 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.8041 4.8041 0.00026114 1.0288e-08 v volume_forces[Z] -4.8041 4.8041 -0.00026109 1.621e-09 v ǁvolume_forcesǁ 1.5251e-09 4.8068 0.26605 0.088056 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 291.16 289.12 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.025583 8.6606e-05 4.9512e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.1509 0.62815 0.27929 0.22758 INSTANT 0.808920000E-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 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.78039E-06 0.38419E-02 Friction velocity uk : 0.33134E-05 0.38411E-02 Dimensionless distance yplus : 0.22061E-04 0.25555E-01 Friction thermal sca. tstar : -0.26147E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.15494E-04 0.17948E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.78039E-06 0.38419E-02 Friction velocity uk : 0.33134E-05 0.38411E-02 Dimensionless distance yplus : 0.22061E-04 0.25555E-01 Friction thermal sca. tstar : -0.26147E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.15494E-04 0.17948E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.53680E-08 4 0.15440E-05 0.15591E-10 0.47853E+01 c Velocity[X] 0.34811E-30 c Velocity[Y] 0.77955E-11 c Velocity[Z] 0.77955E-11 c Pressure 0.17597E-12 27 0.16453E-07 0.14255E-05 0.96028E+01 c k 0.17111E-05 3 0.16520E-06 0.88217E-06 0.58289E+01 c omega 0.13153E+02 1 0.31606E-07 0.54341E+02 0.38376E-01 c TempK 0.94242E+02 1 0.15930E-05 0.48817E+00 0.77900E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -2.6531e-13 2.1369e-13 -2.9019e-17 -7.1861e-18 v Velocity[Y] -0.00024513 0.00024528 -2.914e-10 -6.6728e-12 v Velocity[Z] -0.00024528 0.00024514 2.8614e-10 -2.2256e-12 v ǁVelocityǁ 4.3876e-11 0.00029683 1.5481e-05 7.3904e-06 v Pressure -0.00013669 0.007256 0.00026241 -3.628e-20 v k 1.1435e-07 0.0068091 0.0045062 0.0050774 v omega 55.851 1.0313e+05 2696.5 536.82 v TempK 288 340.46 290.94 288.98 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.3633e-12 0.00013907 8.8088e-05 0.00010475 v CourantNb 3.3077e-10 0.00043933 2.4034e-05 1.1241e-05 v FourierNb 0.15086 0.62815 0.27863 0.22719 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.8052 4.8053 0.0002622 7.3858e-09 v volume_forces[Z] -4.8052 4.8053 -0.00026216 5.0834e-09 v ǁvolume_forcesǁ 1.5507e-09 4.8079 0.26714 0.088566 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 291.17 289.12 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.025555 8.6508e-05 4.9455e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.15086 0.62815 0.27865 0.2272 INSTANT 0.818550000E-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 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.83725E-06 0.38377E-02 Friction velocity uk : 0.33036E-05 0.38369E-02 Dimensionless distance yplus : 0.21997E-04 0.25527E-01 Friction thermal sca. tstar : -0.26640E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.15449E-04 0.17929E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.83725E-06 0.38377E-02 Friction velocity uk : 0.33036E-05 0.38369E-02 Dimensionless distance yplus : 0.21997E-04 0.25527E-01 Friction thermal sca. tstar : -0.26640E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.15449E-04 0.17929E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.53866E-08 4 0.15399E-05 0.14698E-10 0.46331E+01 c Velocity[X] 0.37118E-30 c Velocity[Y] 0.73491E-11 c Velocity[Z] 0.73492E-11 c Pressure 0.17272E-12 27 0.16169E-07 0.13988E-05 0.94988E+01 c k 0.17023E-05 3 0.16319E-06 0.86451E-06 0.58015E+01 c omega 0.13153E+02 1 0.31293E-07 0.53404E+02 0.38043E-01 c TempK 0.94243E+02 1 0.15730E-05 0.48031E+00 0.77269E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -2.6483e-13 2.1362e-13 -2.8863e-17 -7.1482e-18 v Velocity[Y] -0.00024547 0.00024564 -2.9649e-10 -6.4882e-12 v Velocity[Z] -0.00024564 0.00024547 2.9166e-10 -2.0925e-12 v ǁVelocityǁ 4.5021e-11 0.00029722 1.5525e-05 7.4203e-06 v Pressure -0.00013833 0.0072996 0.00026485 4.2469e-20 v k 1.1212e-07 0.0067632 0.0044789 0.00505 v omega 55.606 1.0313e+05 2696.4 536.61 v TempK 288 340.47 290.95 288.98 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.3365e-12 0.0001387 8.7936e-05 0.00010464 v CourantNb 3.348e-10 0.00044005 2.4094e-05 1.128e-05 v FourierNb 0.15082 0.62815 0.278 0.22682 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.8064 4.8064 0.00026326 4.5158e-09 v volume_forces[Z] -4.8064 4.8064 -0.00026322 8.5198e-09 v ǁvolume_forcesǁ 1.5861e-09 4.8091 0.26822 0.089073 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 291.18 289.13 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.025527 8.641e-05 4.9396e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.15082 0.62815 0.27802 0.22683 INSTANT 0.828180000E-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 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.90217E-06 0.38334E-02 Friction velocity uk : 0.32999E-05 0.38326E-02 Dimensionless distance yplus : 0.21971E-04 0.25499E-01 Friction thermal sca. tstar : -0.27164E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.15431E-04 0.17909E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.90217E-06 0.38334E-02 Friction velocity uk : 0.32999E-05 0.38326E-02 Dimensionless distance yplus : 0.21971E-04 0.25499E-01 Friction thermal sca. tstar : -0.27164E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.15431E-04 0.17909E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.54043E-08 4 0.15060E-05 0.13855E-10 0.44860E+01 c Velocity[X] 0.39401E-30 c Velocity[Y] 0.69272E-11 c Velocity[Z] 0.69273E-11 c Pressure 0.16969E-12 27 0.15905E-07 0.13737E-05 0.93971E+01 c k 0.16936E-05 3 0.16122E-06 0.84728E-06 0.57742E+01 c omega 0.13153E+02 1 0.30984E-07 0.52489E+02 0.37716E-01 c TempK 0.94244E+02 1 0.15534E-05 0.47267E+00 0.76650E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -2.6434e-13 2.1354e-13 -2.8708e-17 -7.1106e-18 v Velocity[Y] -0.00024577 0.00024596 -3.0168e-10 -6.4329e-12 v Velocity[Z] -0.00024596 0.00024577 2.9701e-10 -2.0653e-12 v ǁVelocityǁ 4.6358e-11 0.00029757 1.5567e-05 7.4492e-06 v Pressure -0.00013996 0.0073429 0.00026728 -4.2285e-21 v k 1.0995e-07 0.0067179 0.0044519 0.005023 v omega 55.363 1.0313e+05 2696.2 536.39 v TempK 288 340.48 290.96 288.99 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.3105e-12 0.00013833 8.7786e-05 0.00010452 v CourantNb 3.3886e-10 0.00044071 2.4152e-05 1.1318e-05 v FourierNb 0.15079 0.62815 0.27737 0.22645 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.8075 4.8076 0.00026431 1.6791e-09 v volume_forces[Z] -4.8075 4.8076 -0.00026427 1.1923e-08 v ǁvolume_forcesǁ 1.6275e-09 4.8102 0.26929 0.089577 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 291.19 289.14 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.025499 8.6309e-05 4.9337e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.15079 0.62815 0.2774 0.22646 INSTANT 0.837810000E-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 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.98200E-06 0.38291E-02 Friction velocity uk : 0.33062E-05 0.38283E-02 Dimensionless distance yplus : 0.22014E-04 0.25470E-01 Friction thermal sca. tstar : -0.27734E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.15461E-04 0.17888E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.98200E-06 0.38291E-02 Friction velocity uk : 0.33062E-05 0.38283E-02 Dimensionless distance yplus : 0.22014E-04 0.25470E-01 Friction thermal sca. tstar : -0.27734E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.15461E-04 0.17888E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.54213E-08 4 0.14893E-05 0.13058E-10 0.43440E+01 c Velocity[X] 0.41683E-30 c Velocity[Y] 0.65288E-11 c Velocity[Z] 0.65289E-11 c Pressure 0.16686E-12 27 0.15656E-07 0.13504E-05 0.92974E+01 c k 0.16850E-05 3 0.15930E-06 0.83047E-06 0.57473E+01 c omega 0.13153E+02 1 0.30681E-07 0.51597E+02 0.37394E-01 c TempK 0.94244E+02 1 0.15341E-05 0.46523E+00 0.76043E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -2.6384e-13 2.1343e-13 -2.8555e-17 -7.0734e-18 v Velocity[Y] -0.00024605 0.00024625 -3.0685e-10 -6.3805e-12 v Velocity[Z] -0.00024626 0.00024605 3.0233e-10 -2.0367e-12 v ǁVelocityǁ 4.776e-11 0.00029788 1.5608e-05 7.477e-06 v Pressure -0.0001416 0.0073861 0.0002697 8.0281e-21 v k 1.0783e-07 0.0066729 0.0044252 0.0049962 v omega 55.122 1.0313e+05 2696 536.18 v TempK 288 340.5 290.97 288.99 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.2851e-12 0.00013796 8.7637e-05 0.0001044 v CourantNb 3.4289e-10 0.00044132 2.4207e-05 1.1354e-05 v FourierNb 0.15075 0.62815 0.27675 0.22608 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.8086 4.8087 0.00026536 -1.1332e-09 v volume_forces[Z] -4.8086 4.8087 -0.00026531 1.5302e-08 v ǁvolume_forcesǁ 1.6758e-09 4.8113 0.27035 0.090079 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 291.21 289.14 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.02547 8.6208e-05 4.9276e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.15075 0.62815 0.27678 0.22609 INSTANT 0.847440000E-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 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10636E-05 0.38246E-02 Friction velocity uk : 0.33152E-05 0.38239E-02 Dimensionless distance yplus : 0.22074E-04 0.25441E-01 Friction thermal sca. tstar : -0.28344E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.15503E-04 0.17868E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10636E-05 0.38246E-02 Friction velocity uk : 0.33152E-05 0.38239E-02 Dimensionless distance yplus : 0.22074E-04 0.25441E-01 Friction thermal sca. tstar : -0.28344E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.15503E-04 0.17868E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.54376E-08 4 0.14735E-05 0.12306E-10 0.42068E+01 c Velocity[X] 0.43967E-30 c Velocity[Y] 0.61527E-11 c Velocity[Z] 0.61528E-11 c Pressure 0.16409E-12 27 0.15419E-07 0.13276E-05 0.91997E+01 c k 0.16765E-05 3 0.15742E-06 0.81407E-06 0.57205E+01 c omega 0.13153E+02 1 0.30383E-07 0.50725E+02 0.37077E-01 c TempK 0.94245E+02 1 0.15152E-05 0.45799E+00 0.75447E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -2.6333e-13 2.1331e-13 -2.8403e-17 -7.0365e-18 v Velocity[Y] -0.00024629 0.00024652 -3.1199e-10 -6.3278e-12 v Velocity[Z] -0.00024652 0.00024629 3.076e-10 -2.0097e-12 v ǁVelocityǁ 4.925e-11 0.00029816 1.5646e-05 7.5037e-06 v Pressure -0.00014323 0.007429 0.00027212 -1.3445e-20 v k 1.0577e-07 0.0066284 0.0043987 0.0049696 v omega 54.883 1.0313e+05 2695.9 535.97 v TempK 288 340.51 290.99 289 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.2604e-12 0.00013759 8.7489e-05 0.00010429 v CourantNb 3.4692e-10 0.00044187 2.4258e-05 1.1389e-05 v FourierNb 0.15072 0.62815 0.27615 0.22572 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.8097 4.8098 0.00026639 -3.9182e-09 v volume_forces[Z] -4.8097 4.8098 -0.00026635 1.8653e-08 v ǁvolume_forcesǁ 1.7265e-09 4.8124 0.2714 0.090579 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 291.22 289.15 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.025441 8.6104e-05 4.9215e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.15072 0.62815 0.27617 0.22573 INSTANT 0.857070000E-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 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11480E-05 0.38202E-02 Friction velocity uk : 0.33275E-05 0.38194E-02 Dimensionless distance yplus : 0.22155E-04 0.25411E-01 Friction thermal sca. tstar : -0.28998E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.15561E-04 0.17847E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11480E-05 0.38202E-02 Friction velocity uk : 0.33275E-05 0.38194E-02 Dimensionless distance yplus : 0.22155E-04 0.25411E-01 Friction thermal sca. tstar : -0.28998E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.15561E-04 0.17847E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.54531E-08 4 0.14579E-05 0.11596E-10 0.40743E+01 c Velocity[X] 0.46288E-30 c Velocity[Y] 0.57980E-11 c Velocity[Z] 0.57981E-11 c Pressure 0.16144E-12 26 0.14569E-07 0.13058E-05 0.91040E+01 c k 0.16680E-05 3 0.15558E-06 0.79805E-06 0.56940E+01 c omega 0.13153E+02 1 0.30089E-07 0.49874E+02 0.36765E-01 c TempK 0.94246E+02 1 0.14967E-05 0.45093E+00 0.74862E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -2.628e-13 2.1317e-13 -2.8253e-17 -7e-18 v Velocity[Y] -0.00024651 0.00024675 -3.1772e-10 -6.861e-12 v Velocity[Z] -0.00024676 0.00024651 3.127e-10 -2.0948e-12 v ǁVelocityǁ 5.1734e-11 0.0002984 1.5683e-05 7.5294e-06 v Pressure -0.00014487 0.0074718 0.00027453 -2.819e-20 v k 1.0376e-07 0.0065845 0.0043726 0.0049434 v omega 54.646 1.0313e+05 2695.7 535.76 v TempK 288 340.52 291 289.01 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.2363e-12 0.00013722 8.7343e-05 0.00010418 v CourantNb 3.5085e-10 0.00044238 2.4307e-05 1.1422e-05 v FourierNb 0.15068 0.62815 0.27555 0.22536 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.8108 4.8109 0.00026742 -6.6769e-09 v volume_forces[Z] -4.8108 4.8109 -0.00026737 2.1975e-08 v ǁvolume_forcesǁ 1.7804e-09 4.8135 0.27245 0.091076 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 291.23 289.15 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.025411 8.5999e-05 4.9153e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.15068 0.62815 0.27557 0.22537 INSTANT 0.866700000E-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 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12927E-05 0.38156E-02 Friction velocity uk : 0.33786E-05 0.38149E-02 Dimensionless distance yplus : 0.22496E-04 0.25380E-01 Friction thermal sca. tstar : -0.29707E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.15800E-04 0.17826E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12927E-05 0.38156E-02 Friction velocity uk : 0.33786E-05 0.38149E-02 Dimensionless distance yplus : 0.22496E-04 0.25380E-01 Friction thermal sca. tstar : -0.29707E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.15800E-04 0.17826E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.54679E-08 4 0.14426E-05 0.10927E-10 0.39465E+01 c Velocity[X] 0.48529E-30 c Velocity[Y] 0.54636E-11 c Velocity[Z] 0.54638E-11 c Pressure 0.15878E-12 26 0.14261E-07 0.12839E-05 0.90103E+01 c k 0.16596E-05 3 0.15378E-06 0.78242E-06 0.56677E+01 c omega 0.13153E+02 1 0.29800E-07 0.49042E+02 0.36457E-01 c TempK 0.94247E+02 1 0.14785E-05 0.44406E+00 0.74288E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -2.6227e-13 2.1302e-13 -2.8104e-17 -6.9638e-18 v Velocity[Y] -0.0002467 0.00024696 -3.2281e-10 -6.8061e-12 v Velocity[Z] -0.00024696 0.0002467 3.1791e-10 -2.0647e-12 v ǁVelocityǁ 5.3432e-11 0.00029861 1.5717e-05 7.5541e-06 v Pressure -0.00014651 0.0075143 0.00027693 3.1058e-20 v k 1.0181e-07 0.0065409 0.0043467 0.0049173 v omega 54.411 1.0313e+05 2695.5 535.56 v TempK 288 340.53 291.01 289.01 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.2128e-12 0.00013685 8.7198e-05 0.00010406 v CourantNb 3.548e-10 0.00044284 2.4353e-05 1.1454e-05 v FourierNb 0.15065 0.62815 0.27495 0.22501 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.8119 4.8119 0.00026844 -9.414e-09 v volume_forces[Z] -4.8119 4.8119 -0.00026839 2.5291e-08 v ǁvolume_forcesǁ 1.8702e-09 4.8146 0.27348 0.091571 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 291.24 289.16 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.02538 8.5893e-05 4.909e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.15065 0.62815 0.27498 0.22502 INSTANT 0.876330000E-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 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.13795E-05 0.38110E-02 Friction velocity uk : 0.33964E-05 0.38102E-02 Dimensionless distance yplus : 0.22614E-04 0.25350E-01 Friction thermal sca. tstar : -0.30477E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.15883E-04 0.17804E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.13795E-05 0.38110E-02 Friction velocity uk : 0.33964E-05 0.38102E-02 Dimensionless distance yplus : 0.22614E-04 0.25350E-01 Friction thermal sca. tstar : -0.30477E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.15883E-04 0.17804E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.54820E-08 4 0.14341E-05 0.10298E-10 0.38233E+01 c Velocity[X] 0.50780E-30 c Velocity[Y] 0.51488E-11 c Velocity[Z] 0.51489E-11 c Pressure 0.15632E-12 26 0.13964E-07 0.12636E-05 0.89183E+01 c k 0.16513E-05 3 0.15202E-06 0.76716E-06 0.56417E+01 c omega 0.13153E+02 1 0.29515E-07 0.48228E+02 0.36153E-01 c TempK 0.94248E+02 1 0.14607E-05 0.43737E+00 0.73725E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -2.6172e-13 2.1285e-13 -2.7957e-17 -6.9281e-18 v Velocity[Y] -0.00024686 0.00024714 -3.2788e-10 -6.7506e-12 v Velocity[Z] -0.00024715 0.00024686 3.2307e-10 -2.0384e-12 v ǁVelocityǁ 5.5247e-11 0.00029879 1.575e-05 7.5777e-06 v Pressure -0.00014815 0.0075566 0.00027933 -9.266e-21 v k 9.9897e-08 0.0064978 0.0043212 0.0048915 v omega 54.179 1.0313e+05 2695.4 535.35 v TempK 288 340.54 291.02 289.02 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.1899e-12 0.00013649 8.7055e-05 0.00010395 v CourantNb 3.5883e-10 0.00044324 2.4396e-05 1.1484e-05 v FourierNb 0.15061 0.62814 0.27437 0.22466 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.8129 4.813 0.00026945 -1.2122e-08 v volume_forces[Z] -4.8129 4.813 -0.00026941 2.8558e-08 v ǁvolume_forcesǁ 1.9316e-09 4.8156 0.27451 0.092064 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 291.25 289.16 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.02535 8.5786e-05 4.9027e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.15061 0.62814 0.27439 0.22467 INSTANT 0.885960000E-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 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.14697E-05 0.38063E-02 Friction velocity uk : 0.34179E-05 0.38056E-02 Dimensionless distance yplus : 0.22758E-04 0.25319E-01 Friction thermal sca. tstar : -0.31315E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.15983E-04 0.17782E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.14697E-05 0.38063E-02 Friction velocity uk : 0.34179E-05 0.38056E-02 Dimensionless distance yplus : 0.22758E-04 0.25319E-01 Friction thermal sca. tstar : -0.31315E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.15983E-04 0.17782E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.54954E-08 4 0.14160E-05 0.97050E-11 0.37045E+01 c Velocity[X] 0.53016E-30 c Velocity[Y] 0.48524E-11 c Velocity[Z] 0.48526E-11 c Pressure 0.15388E-12 26 0.13670E-07 0.12435E-05 0.88282E+01 c k 0.16431E-05 3 0.15029E-06 0.75227E-06 0.56159E+01 c omega 0.13153E+02 1 0.29234E-07 0.47433E+02 0.35854E-01 c TempK 0.94249E+02 1 0.14431E-05 0.43084E+00 0.73171E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -2.6117e-13 2.1266e-13 -2.7811e-17 -6.8927e-18 v Velocity[Y] -0.000247 0.0002473 -3.3292e-10 -6.6952e-12 v Velocity[Z] -0.0002473 0.000247 3.282e-10 -2.0127e-12 v ǁVelocityǁ 5.7161e-11 0.00029894 1.578e-05 7.6004e-06 v Pressure -0.0001498 0.0075987 0.00028172 8.3222e-21 v k 9.8035e-08 0.0064551 0.0042958 0.004866 v omega 53.948 1.0313e+05 2695.2 535.15 v TempK 288 340.55 291.03 289.02 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.1676e-12 0.00013612 8.6913e-05 0.00010384 v CourantNb 3.6286e-10 0.00044361 2.4437e-05 1.1513e-05 v FourierNb 0.15057 0.62814 0.27379 0.22431 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.814 4.8141 0.00027046 -1.4805e-08 v volume_forces[Z] -4.814 4.8141 -0.00027041 3.1797e-08 v ǁvolume_forcesǁ 1.9972e-09 4.8167 0.27554 0.092554 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 291.26 289.17 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.025319 8.5677e-05 4.8963e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.15057 0.62814 0.27382 0.22432 INSTANT 0.895590000E-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 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15616E-05 0.38016E-02 Friction velocity uk : 0.34423E-05 0.38008E-02 Dimensionless distance yplus : 0.22920E-04 0.25287E-01 Friction thermal sca. tstar : -0.32232E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.16098E-04 0.17760E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15616E-05 0.38016E-02 Friction velocity uk : 0.34423E-05 0.38008E-02 Dimensionless distance yplus : 0.22920E-04 0.25287E-01 Friction thermal sca. tstar : -0.32232E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.16098E-04 0.17760E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.55081E-08 4 0.14036E-05 0.91479E-11 0.35901E+01 c Velocity[X] 0.55230E-30 c Velocity[Y] 0.45739E-11 c Velocity[Z] 0.45740E-11 c Pressure 0.15184E-12 26 0.13405E-07 0.12267E-05 0.87398E+01 c k 0.16349E-05 2 0.13241E-05 0.73739E-06 0.55890E+01 c omega 0.13153E+02 1 0.28958E-07 0.46656E+02 0.35559E-01 c TempK 0.94250E+02 1 0.14260E-05 0.42448E+00 0.72628E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -2.606e-13 2.1246e-13 -2.7667e-17 -6.8578e-18 v Velocity[Y] -0.00024711 0.00024743 -3.3806e-10 -6.7702e-12 v Velocity[Z] -0.00024743 0.00024711 3.3326e-10 -2.0163e-12 v ǁVelocityǁ 5.9509e-11 0.00029906 1.5809e-05 7.6222e-06 v Pressure -0.00015144 0.0076406 0.00028411 2.2479e-20 v k 9.622e-08 0.0064128 0.0042708 0.0048407 v omega 53.719 1.0313e+05 2695.1 534.95 v TempK 288 340.57 291.04 289.03 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.1458e-12 0.00013576 8.6772e-05 0.00010373 v CourantNb 3.6694e-10 0.00044392 2.4474e-05 1.1541e-05 v FourierNb 0.15053 0.62814 0.27322 0.22397 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.815 4.8151 0.00027146 -1.7465e-08 v volume_forces[Z] -4.815 4.8151 -0.00027141 3.5009e-08 v ǁvolume_forcesǁ 2.0664e-09 4.8177 0.27655 0.093042 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 291.27 289.17 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.025287 8.5567e-05 4.8898e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.15053 0.62814 0.27325 0.22398 INSTANT 0.905220000E-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 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.16710E-05 0.37968E-02 Friction velocity uk : 0.34801E-05 0.37961E-02 Dimensionless distance yplus : 0.23172E-04 0.25256E-01 Friction thermal sca. tstar : -0.33240E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.16274E-04 0.17738E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.16710E-05 0.37968E-02 Friction velocity uk : 0.34801E-05 0.37961E-02 Dimensionless distance yplus : 0.23172E-04 0.25256E-01 Friction thermal sca. tstar : -0.33240E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.16274E-04 0.17738E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.55202E-08 4 0.13912E-05 0.86244E-11 0.34800E+01 c Velocity[X] 0.57407E-30 c Velocity[Y] 0.43121E-11 c Velocity[Z] 0.43123E-11 c Pressure 0.14943E-12 26 0.13123E-07 0.12069E-05 0.86531E+01 c k 0.16268E-05 2 0.12958E-05 0.72320E-06 0.55637E+01 c omega 0.13153E+02 1 0.28685E-07 0.45895E+02 0.35268E-01 c TempK 0.94250E+02 1 0.14091E-05 0.41828E+00 0.72094E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -2.6003e-13 2.1224e-13 -2.7525e-17 -6.8231e-18 v Velocity[Y] -0.0002472 0.00024754 -3.4305e-10 -6.7153e-12 v Velocity[Z] -0.00024754 0.0002472 3.3831e-10 -1.9903e-12 v ǁVelocityǁ 6.1625e-11 0.00029915 1.5837e-05 7.643e-06 v Pressure -0.00015309 0.0076824 0.00028649 -7.7339e-21 v k 9.445e-08 0.0063709 0.004246 0.0048156 v omega 53.492 1.0313e+05 2694.9 534.75 v TempK 288 340.58 291.05 289.03 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.1246e-12 0.00013539 8.6633e-05 0.00010362 v CourantNb 3.7097e-10 0.00044419 2.4509e-05 1.1567e-05 v FourierNb 0.15049 0.62814 0.27266 0.22363 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.816 4.8161 0.00027245 -2.0103e-08 v volume_forces[Z] -4.816 4.8161 -0.0002724 3.8199e-08 v ǁvolume_forcesǁ 2.1513e-09 4.8187 0.27756 0.093528 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 291.28 289.18 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.025256 8.5456e-05 4.8832e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.15049 0.62814 0.27268 0.22364 INSTANT 0.914850000E-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 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.17644E-05 0.37919E-02 Friction velocity uk : 0.35094E-05 0.37912E-02 Dimensionless distance yplus : 0.23367E-04 0.25223E-01 Friction thermal sca. tstar : -0.34355E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.16411E-04 0.17715E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.17644E-05 0.37919E-02 Friction velocity uk : 0.35094E-05 0.37912E-02 Dimensionless distance yplus : 0.23367E-04 0.25223E-01 Friction thermal sca. tstar : -0.34355E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.16411E-04 0.17715E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.55316E-08 4 0.13795E-05 0.81332E-11 0.33741E+01 c Velocity[X] 0.59548E-30 c Velocity[Y] 0.40665E-11 c Velocity[Z] 0.40667E-11 c Pressure 0.14730E-12 26 0.12871E-07 0.11893E-05 0.85681E+01 c k 0.16188E-05 2 0.12683E-05 0.70934E-06 0.55386E+01 c omega 0.13153E+02 1 0.28415E-07 0.45151E+02 0.34981E-01 c TempK 0.94251E+02 1 0.13926E-05 0.41223E+00 0.71569E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -2.5945e-13 2.1201e-13 -2.7384e-17 -6.7889e-18 v Velocity[Y] -0.00024726 0.00024762 -3.4802e-10 -6.6609e-12 v Velocity[Z] -0.00024762 0.00024727 3.4334e-10 -1.9658e-12 v ǁVelocityǁ 6.1541e-11 0.00029921 1.5862e-05 7.6629e-06 v Pressure -0.00015474 0.0077239 0.00028886 -7.1088e-21 v k 9.2722e-08 0.0063294 0.0042215 0.0047908 v omega 53.267 1.0313e+05 2694.8 534.55 v TempK 288 340.59 291.06 289.04 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.1039e-12 0.00013503 8.6495e-05 0.00010351 v CourantNb 3.7502e-10 0.00044442 2.4542e-05 1.1591e-05 v FourierNb 0.15045 0.62814 0.2721 0.22329 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.817 4.8171 0.00027344 -2.2716e-08 v volume_forces[Z] -4.817 4.8171 -0.00027339 4.1357e-08 v ǁvolume_forcesǁ 2.2277e-09 4.8197 0.27856 0.094012 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 291.29 289.18 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.025223 8.5343e-05 4.8766e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.15045 0.62814 0.27213 0.2233 INSTANT 0.924480000E-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 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.18590E-05 0.37871E-02 Friction velocity uk : 0.35413E-05 0.37863E-02 Dimensionless distance yplus : 0.23579E-04 0.25191E-01 Friction thermal sca. tstar : -0.35595E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.16560E-04 0.17692E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.18590E-05 0.37871E-02 Friction velocity uk : 0.35413E-05 0.37863E-02 Dimensionless distance yplus : 0.23579E-04 0.25191E-01 Friction thermal sca. tstar : -0.35595E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.16560E-04 0.17692E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.55424E-08 4 0.13820E-05 0.76728E-11 0.32724E+01 c Velocity[X] 0.61649E-30 c Velocity[Y] 0.38363E-11 c Velocity[Z] 0.38365E-11 c Pressure 0.14539E-12 26 0.12630E-07 0.11737E-05 0.84846E+01 c k 0.16109E-05 2 0.12417E-05 0.69581E-06 0.55137E+01 c omega 0.13153E+02 1 0.28150E-07 0.44422E+02 0.34697E-01 c TempK 0.94252E+02 1 0.13764E-05 0.40632E+00 0.71053E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -2.5886e-13 2.1176e-13 -2.7244e-17 -6.755e-18 v Velocity[Y] -0.00024731 0.00024768 -3.5292e-10 -6.5591e-12 v Velocity[Z] -0.00024768 0.00024731 3.4837e-10 -1.9033e-12 v ǁVelocityǁ 6.0852e-11 0.00029925 1.5886e-05 7.6818e-06 v Pressure -0.00015639 0.0077652 0.00029123 -1.4193e-20 v k 9.1037e-08 0.0062883 0.0041972 0.0047662 v omega 53.044 1.0313e+05 2694.6 534.35 v TempK 288 340.6 291.08 289.04 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.0837e-12 0.00013467 8.6358e-05 0.0001034 v CourantNb 3.791e-10 0.00044461 2.4571e-05 1.1615e-05 v FourierNb 0.15041 0.62814 0.27155 0.22296 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.818 4.8181 0.00027442 -2.5307e-08 v volume_forces[Z] -4.818 4.8181 -0.00027437 4.4489e-08 v ǁvolume_forcesǁ 2.2247e-09 4.8207 0.27956 0.094493 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 291.31 289.19 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.025191 8.523e-05 4.8699e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.15041 0.62814 0.27158 0.22297 INSTANT 0.934110000E-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 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19534E-05 0.37821E-02 Friction velocity uk : 0.35749E-05 0.37814E-02 Dimensionless distance yplus : 0.23803E-04 0.25158E-01 Friction thermal sca. tstar : -0.36993E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.16718E-04 0.17669E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19534E-05 0.37821E-02 Friction velocity uk : 0.35749E-05 0.37814E-02 Dimensionless distance yplus : 0.23803E-04 0.25158E-01 Friction thermal sca. tstar : -0.36993E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.16718E-04 0.17669E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.55525E-08 4 0.13575E-05 0.72417E-11 0.31748E+01 c Velocity[X] 0.63705E-30 c Velocity[Y] 0.36208E-11 c Velocity[Z] 0.36209E-11 c Pressure 0.14333E-12 26 0.12387E-07 0.11567E-05 0.84027E+01 c k 0.16030E-05 2 0.12158E-05 0.68259E-06 0.54890E+01 c omega 0.13153E+02 1 0.27888E-07 0.43710E+02 0.34418E-01 c TempK 0.94253E+02 1 0.13604E-05 0.40056E+00 0.70546E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -2.5826e-13 2.115e-13 -2.7106e-17 -6.7214e-18 v Velocity[Y] -0.00024733 0.00024772 -3.5786e-10 -6.5068e-12 v Velocity[Z] -0.00024772 0.00024733 3.5332e-10 -1.8797e-12 v ǁVelocityǁ 6.011e-11 0.00029925 1.5908e-05 7.6999e-06 v Pressure -0.00015804 0.0078063 0.00029359 1.6203e-20 v k 8.9392e-08 0.0062476 0.0041732 0.0047418 v omega 52.823 1.0313e+05 2694.4 534.16 v TempK 288 340.61 291.09 289.05 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.064e-12 0.00013431 8.6222e-05 0.00010329 v CourantNb 3.8318e-10 0.00044476 2.4599e-05 1.1637e-05 v FourierNb 0.15037 0.62814 0.27101 0.22263 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.819 4.8191 0.00027539 -2.7875e-08 v volume_forces[Z] -4.819 4.8191 -0.00027534 4.7594e-08 v ǁvolume_forcesǁ 2.1998e-09 4.8217 0.28055 0.094972 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 291.32 289.2 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.025158 8.5115e-05 4.8631e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.15037 0.62814 0.27104 0.22264 INSTANT 0.943740000E-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 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.20357E-05 0.37771E-02 Friction velocity uk : 0.36130E-05 0.37764E-02 Dimensionless distance yplus : 0.24056E-04 0.25125E-01 Friction thermal sca. tstar : -0.38577E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.16896E-04 0.17646E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.20357E-05 0.37771E-02 Friction velocity uk : 0.36130E-05 0.37764E-02 Dimensionless distance yplus : 0.24056E-04 0.25125E-01 Friction thermal sca. tstar : -0.38577E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.16896E-04 0.17646E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.55620E-08 4 0.13471E-05 0.68386E-11 0.30813E+01 c Velocity[X] 0.65713E-30 c Velocity[Y] 0.34192E-11 c Velocity[Z] 0.34194E-11 c Pressure 0.14143E-12 26 0.12161E-07 0.11410E-05 0.83224E+01 c k 0.15952E-05 2 0.11907E-05 0.66968E-06 0.54645E+01 c omega 0.13153E+02 1 0.27629E-07 0.43012E+02 0.34142E-01 c TempK 0.94254E+02 1 0.13448E-05 0.39493E+00 0.70047E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -2.5766e-13 2.1123e-13 -2.697e-17 -6.6882e-18 v Velocity[Y] -0.00024733 0.00024773 -3.6277e-10 -6.4568e-12 v Velocity[Z] -0.00024773 0.00024733 3.5825e-10 -1.8563e-12 v ǁVelocityǁ 5.9314e-11 0.00029923 1.5928e-05 7.7171e-06 v Pressure -0.00015969 0.0078473 0.00029594 -9.9156e-21 v k 8.7787e-08 0.006209 0.0041495 0.0047177 v omega 52.604 1.0313e+05 2694.3 533.96 v TempK 288 340.62 291.1 289.05 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.0448e-12 0.00013399 8.6087e-05 0.00010318 v CourantNb 3.8726e-10 0.00044486 2.4623e-05 1.1657e-05 v FourierNb 0.15034 0.62814 0.27048 0.2223 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.82 4.8201 0.00027636 -3.0423e-08 v volume_forces[Z] -4.82 4.8201 -0.0002763 5.0675e-08 v ǁvolume_forcesǁ 2.173e-09 4.8227 0.28153 0.09545 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 291.33 289.2 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.025125 8.5e-05 4.8563e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.15034 0.62814 0.2705 0.22231 INSTANT 0.953370000E-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 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.20093E-05 0.37721E-02 Friction velocity uk : 0.35688E-05 0.37714E-02 Dimensionless distance yplus : 0.23764E-04 0.25091E-01 Friction thermal sca. tstar : -0.40388E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.16691E-04 0.17623E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.20093E-05 0.37721E-02 Friction velocity uk : 0.35688E-05 0.37714E-02 Dimensionless distance yplus : 0.23764E-04 0.25091E-01 Friction thermal sca. tstar : -0.40388E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.16691E-04 0.17623E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.55710E-08 4 0.13372E-05 0.64621E-11 0.29918E+01 c Velocity[X] 0.67672E-30 c Velocity[Y] 0.32310E-11 c Velocity[Z] 0.32311E-11 c Pressure 0.13974E-12 26 0.11947E-07 0.11271E-05 0.82435E+01 c k 0.15875E-05 2 0.11662E-05 0.65706E-06 0.54403E+01 c omega 0.13153E+02 1 0.27373E-07 0.42328E+02 0.33870E-01 c TempK 0.94255E+02 1 0.13295E-05 0.38943E+00 0.69557E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -2.5704e-13 2.1094e-13 -2.6834e-17 -6.6554e-18 v Velocity[Y] -0.00024731 0.00024773 -3.6766e-10 -6.4076e-12 v Velocity[Z] -0.00024773 0.00024731 3.6315e-10 -1.833e-12 v ǁVelocityǁ 5.8478e-11 0.00029919 1.5947e-05 7.7335e-06 v Pressure -0.00016134 0.0078881 0.00029829 3.6892e-21 v k 8.622e-08 0.0061716 0.0041259 0.0046938 v omega 52.386 1.0313e+05 2694.1 533.77 v TempK 288 340.63 291.11 289.06 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.026e-12 0.00013372 8.5954e-05 0.00010307 v CourantNb 3.9132e-10 0.00044493 2.4646e-05 1.1677e-05 v FourierNb 0.1503 0.62814 0.26995 0.22198 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.8209 4.821 0.00027731 -3.2949e-08 v volume_forces[Z] -4.8209 4.821 -0.00027726 5.3731e-08 v ǁvolume_forcesǁ 2.1442e-09 4.8236 0.2825 0.095925 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 291.34 289.21 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.025091 8.4883e-05 4.8494e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.1503 0.62814 0.26997 0.22199 INSTANT 0.963000000E-01 TIME STEP NUMBER 100 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19797E-05 0.37670E-02 Friction velocity uk : 0.35193E-05 0.37663E-02 Dimensionless distance yplus : 0.23434E-04 0.25058E-01 Friction thermal sca. tstar : -0.42486E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.16459E-04 0.17599E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19797E-05 0.37670E-02 Friction velocity uk : 0.35193E-05 0.37663E-02 Dimensionless distance yplus : 0.23434E-04 0.25058E-01 Friction thermal sca. tstar : -0.42486E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.16459E-04 0.17599E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.55793E-08 4 0.13274E-05 0.61110E-11 0.29063E+01 c Velocity[X] 0.69580E-30 c Velocity[Y] 0.30554E-11 c Velocity[Z] 0.30556E-11 c Pressure 0.13790E-12 26 0.11741E-07 0.11120E-05 0.81660E+01 c k 0.15799E-05 2 0.11425E-05 0.64473E-06 0.54162E+01 c omega 0.13153E+02 1 0.27121E-07 0.41658E+02 0.33601E-01 c TempK 0.94255E+02 1 0.13144E-05 0.38407E+00 0.69075E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -2.5643e-13 2.1064e-13 -2.67e-17 -6.6228e-18 v Velocity[Y] -0.00024727 0.0002477 -3.7283e-10 -6.6407e-12 v Velocity[Z] -0.0002477 0.00024727 3.6786e-10 -1.9675e-12 v ǁVelocityǁ 5.7738e-11 0.00029912 1.5965e-05 7.749e-06 v Pressure -0.000163 0.0079286 0.00030064 -1.2342e-20 v k 8.4691e-08 0.0061345 0.0041026 0.0046701 v omega 52.17 1.0313e+05 2694 533.58 v TempK 288 340.64 291.12 289.06 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.0077e-12 0.00013345 8.5822e-05 0.00010297 v CourantNb 3.9536e-10 0.00044496 2.4666e-05 1.1695e-05 v FourierNb 0.15026 0.62814 0.26942 0.22166 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.8218 4.8219 0.00027827 -3.5454e-08 v volume_forces[Z] -4.8218 4.8219 -0.00027821 5.6761e-08 v ǁvolume_forcesǁ 2.114e-09 4.8245 0.28347 0.096398 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 291.35 289.21 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.025058 8.4766e-05 4.8425e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.15026 0.62814 0.26945 0.22167 INSTANT 0.972630000E-01 TIME STEP NUMBER 101 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19521E-05 0.37619E-02 Friction velocity uk : 0.34716E-05 0.37612E-02 Dimensionless distance yplus : 0.23117E-04 0.25024E-01 Friction thermal sca. tstar : -0.44954E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.16236E-04 0.17575E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19521E-05 0.37619E-02 Friction velocity uk : 0.34716E-05 0.37612E-02 Dimensionless distance yplus : 0.23117E-04 0.25024E-01 Friction thermal sca. tstar : -0.44954E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.16236E-04 0.17575E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.55870E-08 4 0.13178E-05 0.57840E-11 0.28248E+01 c Velocity[X] 0.71427E-30 c Velocity[Y] 0.28919E-11 c Velocity[Z] 0.28921E-11 c Pressure 0.13630E-12 26 0.11550E-07 0.10988E-05 0.80899E+01 c k 0.15723E-05 2 0.11194E-05 0.63269E-06 0.53924E+01 c omega 0.13153E+02 1 0.26872E-07 0.41003E+02 0.33335E-01 c TempK 0.94256E+02 1 0.12996E-05 0.37882E+00 0.68600E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -2.558e-13 2.1033e-13 -2.6568e-17 -6.5906e-18 v Velocity[Y] -0.00024721 0.00024766 -3.7768e-10 -6.5945e-12 v Velocity[Z] -0.00024766 0.00024721 3.727e-10 -1.9428e-12 v ǁVelocityǁ 5.6758e-11 0.00029902 1.598e-05 7.7637e-06 v Pressure -0.00016465 0.007969 0.00030298 3.7505e-21 v k 8.3197e-08 0.0060978 0.0040796 0.0046466 v omega 51.956 1.0313e+05 2693.8 533.39 v TempK 288 340.65 291.13 289.07 v Density 1.205 1.205 1.205 1.205 v TurbVisc 9.8984e-13 0.00013319 8.5691e-05 0.00010286 v CourantNb 3.9941e-10 0.00044496 2.4683e-05 1.1712e-05 v FourierNb 0.15022 0.62814 0.26891 0.22134 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.8228 4.8229 0.00027921 -3.7945e-08 v volume_forces[Z] -4.8228 4.8229 -0.00027916 5.9778e-08 v ǁvolume_forcesǁ 2.0872e-09 4.8255 0.28443 0.096869 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 291.36 289.22 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.025024 8.4647e-05 4.8355e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.15022 0.62814 0.26893 0.22135 INSTANT 0.982260000E-01 TIME STEP NUMBER 102 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19128E-05 0.37567E-02 Friction velocity uk : 0.34164E-05 0.37560E-02 Dimensionless distance yplus : 0.22750E-04 0.24989E-01 Friction thermal sca. tstar : -0.47914E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.15978E-04 0.17551E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19128E-05 0.37567E-02 Friction velocity uk : 0.34164E-05 0.37560E-02 Dimensionless distance yplus : 0.22750E-04 0.24989E-01 Friction thermal sca. tstar : -0.47914E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.15978E-04 0.17551E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.55942E-08 4 0.13085E-05 0.54799E-11 0.27472E+01 c Velocity[X] 0.73214E-30 c Velocity[Y] 0.27399E-11 c Velocity[Z] 0.27400E-11 c Pressure 0.13460E-12 26 0.11349E-07 0.10848E-05 0.80152E+01 c k 0.15647E-05 2 0.10970E-05 0.62092E-06 0.53688E+01 c omega 0.13153E+02 1 0.26626E-07 0.40360E+02 0.33073E-01 c TempK 0.94257E+02 1 0.12851E-05 0.37370E+00 0.68134E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -2.5517e-13 2.1001e-13 -2.6437e-17 -6.5587e-18 v Velocity[Y] -0.00024713 0.00024759 -3.8238e-10 -6.4127e-12 v Velocity[Z] -0.00024759 0.00024713 3.7781e-10 -1.6433e-12 v ǁVelocityǁ 5.6014e-11 0.00029891 1.5995e-05 7.7775e-06 v Pressure -0.00016631 0.0080093 0.00030531 9.9891e-21 v k 8.1739e-08 0.0060613 0.0040568 0.0046233 v omega 51.744 1.0313e+05 2693.7 533.2 v TempK 288 340.66 291.14 289.07 v Density 1.205 1.205 1.205 1.205 v TurbVisc 9.7238e-13 0.00013292 8.5561e-05 0.00010276 v CourantNb 4.0353e-10 0.00044492 2.4699e-05 1.1728e-05 v FourierNb 0.15019 0.62814 0.26839 0.22103 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.8237 4.8238 0.00028016 -4.041e-08 v volume_forces[Z] -4.8237 4.8238 -0.0002801 6.2759e-08 v ǁvolume_forcesǁ 2.0518e-09 4.8264 0.28539 0.097338 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 291.37 289.22 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.024989 8.4528e-05 4.8285e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.15019 0.62814 0.26842 0.22104 INSTANT 0.991890000E-01 TIME STEP NUMBER 103 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.18810E-05 0.37515E-02 Friction velocity uk : 0.33670E-05 0.37509E-02 Dimensionless distance yplus : 0.22421E-04 0.24955E-01 Friction thermal sca. tstar : -0.51554E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.15747E-04 0.17527E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.18810E-05 0.37515E-02 Friction velocity uk : 0.33670E-05 0.37509E-02 Dimensionless distance yplus : 0.22421E-04 0.24955E-01 Friction thermal sca. tstar : -0.51554E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.15747E-04 0.17527E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.56009E-08 4 0.12997E-05 0.51978E-11 0.26734E+01 c Velocity[X] 0.74947E-30 c Velocity[Y] 0.25988E-11 c Velocity[Z] 0.25989E-11 c Pressure 0.13318E-12 26 0.11175E-07 0.10731E-05 0.79418E+01 c k 0.15573E-05 2 0.10752E-05 0.60942E-06 0.53453E+01 c omega 0.13153E+02 1 0.26383E-07 0.39730E+02 0.32814E-01 c TempK 0.94258E+02 1 0.12709E-05 0.36869E+00 0.67674E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -2.5453e-13 2.0968e-13 -2.6307e-17 -6.5272e-18 v Velocity[Y] -0.00024703 0.00024751 -3.8721e-10 -6.3666e-12 v Velocity[Z] -0.00024751 0.00024703 3.8258e-10 -1.6235e-12 v ǁVelocityǁ 5.4923e-11 0.00029877 1.6007e-05 7.7906e-06 v Pressure -0.00016797 0.0080493 0.00030764 -3.3693e-20 v k 8.0314e-08 0.0060252 0.0040342 0.0046003 v omega 51.533 1.0313e+05 2693.5 533.01 v TempK 288 340.67 291.15 289.08 v Density 1.205 1.205 1.205 1.205 v TurbVisc 9.5533e-13 0.00013265 8.5432e-05 0.00010265 v CourantNb 4.0764e-10 0.00044485 2.4712e-05 1.1742e-05 v FourierNb 0.15015 0.62814 0.26789 0.22072 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.8246 4.8247 0.00028109 -4.2845e-08 v volume_forces[Z] -4.8246 4.8247 -0.00028103 6.5712e-08 v ǁvolume_forcesǁ 2.0249e-09 4.8273 0.28634 0.097805 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 291.38 289.23 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.024955 8.4408e-05 4.8215e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.15015 0.62814 0.26791 0.22073 INSTANT 0.100152000E+00 TIME STEP NUMBER 104 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.18316E-05 0.37463E-02 Friction velocity uk : 0.33059E-05 0.37456E-02 Dimensionless distance yplus : 0.22014E-04 0.24920E-01 Friction thermal sca. tstar : -0.56178E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.15461E-04 0.17502E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.18316E-05 0.37463E-02 Friction velocity uk : 0.33059E-05 0.37456E-02 Dimensionless distance yplus : 0.22014E-04 0.24920E-01 Friction thermal sca. tstar : -0.56178E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.15461E-04 0.17502E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.56069E-08 4 0.12907E-05 0.49363E-11 0.26035E+01 c Velocity[X] 0.76618E-30 c Velocity[Y] 0.24681E-11 c Velocity[Z] 0.24682E-11 c Pressure 0.13156E-12 26 0.10991E-07 0.10598E-05 0.78697E+01 c k 0.15499E-05 2 0.10540E-05 0.59817E-06 0.53221E+01 c omega 0.13153E+02 1 0.26143E-07 0.39113E+02 0.32558E-01 c TempK 0.94259E+02 1 0.12569E-05 0.36380E+00 0.67222E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -2.5389e-13 2.0934e-13 -2.6178e-17 -6.4959e-18 v Velocity[Y] -0.00024692 0.00024741 -3.9201e-10 -6.3216e-12 v Velocity[Z] -0.00024741 0.00024692 3.8733e-10 -1.6036e-12 v ǁVelocityǁ 5.39e-11 0.00029861 1.6019e-05 7.8029e-06 v Pressure -0.00016963 0.0080892 0.00030996 -7.3662e-21 v k 7.8923e-08 0.0059894 0.0040118 0.0045774 v omega 51.325 1.0313e+05 2693.4 532.82 v TempK 288 340.68 291.16 289.08 v Density 1.205 1.205 1.205 1.205 v TurbVisc 9.3867e-13 0.00013239 8.5304e-05 0.00010255 v CourantNb 4.1172e-10 0.00044474 2.4723e-05 1.1756e-05 v FourierNb 0.15011 0.62814 0.26739 0.22041 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.8255 4.8256 0.00028202 -4.5271e-08 v volume_forces[Z] -4.8255 4.8256 -0.00028196 6.8646e-08 v ǁvolume_forcesǁ 1.9855e-09 4.8282 0.28728 0.09827 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 291.39 289.23 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.02492 8.4287e-05 4.8144e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.15011 0.62814 0.26741 0.22042 INSTANT 0.101115000E+00 TIME STEP NUMBER 105 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.17815E-05 0.37410E-02 Friction velocity uk : 0.32449E-05 0.37404E-02 Dimensionless distance yplus : 0.21607E-04 0.24885E-01 Friction thermal sca. tstar : -0.62325E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.15176E-04 0.17478E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.17815E-05 0.37410E-02 Friction velocity uk : 0.32449E-05 0.37404E-02 Dimensionless distance yplus : 0.21607E-04 0.24885E-01 Friction thermal sca. tstar : -0.62325E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.15176E-04 0.17478E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.56125E-08 4 0.12826E-05 0.46945E-11 0.25375E+01 c Velocity[X] 0.78236E-30 c Velocity[Y] 0.23472E-11 c Velocity[Z] 0.23473E-11 c Pressure 0.13017E-12 26 0.10827E-07 0.10483E-05 0.77988E+01 c k 0.15426E-05 2 0.10334E-05 0.58718E-06 0.52990E+01 c omega 0.13153E+02 1 0.25906E-07 0.38508E+02 0.32305E-01 c TempK 0.94260E+02 1 0.12432E-05 0.35901E+00 0.66778E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -2.5324e-13 2.0898e-13 -2.6051e-17 -6.465e-18 v Velocity[Y] -0.00024679 0.00024729 -3.9679e-10 -6.2773e-12 v Velocity[Z] -0.00024729 0.00024679 3.9206e-10 -1.5841e-12 v ǁVelocityǁ 5.2911e-11 0.00029842 1.6029e-05 7.8144e-06 v Pressure -0.00017129 0.0081289 0.00031227 1.3384e-20 v k 7.7563e-08 0.0059539 0.0039897 0.0045548 v omega 51.117 1.0313e+05 2693.2 532.64 v TempK 288 340.69 291.17 289.09 v Density 1.205 1.205 1.205 1.205 v TurbVisc 9.2241e-13 0.00013212 8.5177e-05 0.00010245 v CourantNb 4.158e-10 0.0004446 2.4732e-05 1.1768e-05 v FourierNb 0.15008 0.62813 0.2669 0.2201 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.8264 4.8265 0.00028294 -4.7677e-08 v volume_forces[Z] -4.8264 4.8265 -0.00028288 7.1557e-08 v ǁvolume_forcesǁ 1.9485e-09 4.8291 0.28822 0.098733 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 291.4 289.24 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.024885 8.4166e-05 4.8072e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.15008 0.62813 0.26692 0.22011 INSTANT 0.102078000E+00 TIME STEP NUMBER 106 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.17291E-05 0.37357E-02 Friction velocity uk : 0.31829E-05 0.37351E-02 Dimensionless distance yplus : 0.21194E-04 0.24850E-01 Friction thermal sca. tstar : -0.71064E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.14886E-04 0.17453E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.17291E-05 0.37357E-02 Friction velocity uk : 0.31829E-05 0.37351E-02 Dimensionless distance yplus : 0.21194E-04 0.24850E-01 Friction thermal sca. tstar : -0.71064E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.14886E-04 0.17453E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.56175E-08 4 0.12740E-05 0.44715E-11 0.24752E+01 c Velocity[X] 0.79784E-30 c Velocity[Y] 0.22357E-11 c Velocity[Z] 0.22358E-11 c Pressure 0.12883E-12 26 0.10666E-07 0.10373E-05 0.77292E+01 c k 0.15353E-05 2 0.10133E-05 0.57644E-06 0.52762E+01 c omega 0.13153E+02 1 0.25671E-07 0.37915E+02 0.32056E-01 c TempK 0.94260E+02 1 0.12297E-05 0.35433E+00 0.66340E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -2.5259e-13 2.0862e-13 -2.5925e-17 -6.4344e-18 v Velocity[Y] -0.00024664 0.00024716 -4.0156e-10 -6.2342e-12 v Velocity[Z] -0.00024716 0.00024664 3.9675e-10 -1.5645e-12 v ǁVelocityǁ 5.1948e-11 0.00029822 1.6038e-05 7.8252e-06 v Pressure -0.00017295 0.0081684 0.00031458 -8.1016e-21 v k 7.6235e-08 0.0059187 0.0039678 0.0045323 v omega 50.912 1.0313e+05 2693.1 532.46 v TempK 288 340.7 291.18 289.1 v Density 1.205 1.205 1.205 1.205 v TurbVisc 9.0652e-13 0.00013185 8.5051e-05 0.00010235 v CourantNb 4.1988e-10 0.00044443 2.4739e-05 1.1779e-05 v FourierNb 0.15004 0.62813 0.26641 0.2198 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.8273 4.8274 0.00028386 -5.0065e-08 v volume_forces[Z] -4.8273 4.8274 -0.0002838 7.4444e-08 v ǁvolume_forcesǁ 1.9127e-09 4.8299 0.28915 0.099194 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 291.41 289.24 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.02485 8.4043e-05 4.8e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.15004 0.62813 0.26643 0.21981 INSTANT 0.103041000E+00 TIME STEP NUMBER 107 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.16735E-05 0.37304E-02 Friction velocity uk : 0.31192E-05 0.37297E-02 Dimensionless distance yplus : 0.20771E-04 0.24814E-01 Friction thermal sca. tstar : -0.84944E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.14588E-04 0.17428E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.16735E-05 0.37304E-02 Friction velocity uk : 0.31192E-05 0.37297E-02 Dimensionless distance yplus : 0.20771E-04 0.24814E-01 Friction thermal sca. tstar : -0.84944E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.14588E-04 0.17428E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.56220E-08 4 0.12659E-05 0.42663E-11 0.24167E+01 c Velocity[X] 0.81271E-30 c Velocity[Y] 0.21331E-11 c Velocity[Z] 0.21332E-11 c Pressure 0.12758E-12 26 0.10516E-07 0.10270E-05 0.76607E+01 c k 0.15281E-05 2 0.99378E-06 0.56593E-06 0.52536E+01 c omega 0.13153E+02 1 0.25440E-07 0.37334E+02 0.31809E-01 c TempK 0.94261E+02 1 0.12164E-05 0.34976E+00 0.65908E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -2.5193e-13 2.0825e-13 -2.58e-17 -6.4041e-18 v Velocity[Y] -0.00024648 0.00024701 -4.063e-10 -6.1905e-12 v Velocity[Z] -0.00024701 0.00024648 4.0142e-10 -1.5451e-12 v ǁVelocityǁ 5.1011e-11 0.000298 1.6045e-05 7.8353e-06 v Pressure -0.00017461 0.0082077 0.00031689 -1.7968e-20 v k 7.4937e-08 0.0058838 0.0039461 0.0045101 v omega 50.708 1.0313e+05 2692.9 532.27 v TempK 288 340.71 291.19 289.1 v Density 1.205 1.205 1.205 1.205 v TurbVisc 8.9099e-13 0.00013159 8.4927e-05 0.00010224 v CourantNb 4.2396e-10 0.00044423 2.4744e-05 1.1789e-05 v FourierNb 0.15 0.62813 0.26592 0.2195 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.8281 4.8282 0.00028477 -5.2434e-08 v volume_forces[Z] -4.8281 4.8282 -0.00028471 7.7308e-08 v ǁvolume_forcesǁ 1.8779e-09 4.8308 0.29007 0.099653 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 291.42 289.25 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.024814 8.392e-05 4.7928e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.15 0.62813 0.26595 0.21951 INSTANT 0.104004000E+00 TIME STEP NUMBER 108 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.16143E-05 0.37250E-02 Friction velocity uk : 0.30537E-05 0.37244E-02 Dimensionless distance yplus : 0.20335E-04 0.24779E-01 Friction thermal sca. tstar : -0.11237E+05 0.00000E+00 Dim-less thermal sca. tplus : 0.14282E-04 0.17403E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.16143E-05 0.37250E-02 Friction velocity uk : 0.30537E-05 0.37244E-02 Dimensionless distance yplus : 0.20335E-04 0.24779E-01 Friction thermal sca. tstar : -0.11237E+05 0.00000E+00 Dim-less thermal sca. tplus : 0.14282E-04 0.17403E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.56260E-08 4 0.12579E-05 0.40779E-11 0.23619E+01 c Velocity[X] 0.82698E-30 c Velocity[Y] 0.20389E-11 c Velocity[Z] 0.20390E-11 c Pressure 0.12619E-12 26 0.10359E-07 0.10155E-05 0.75934E+01 c k 0.15210E-05 2 0.97478E-06 0.55566E-06 0.52311E+01 c omega 0.13153E+02 1 0.25211E-07 0.36764E+02 0.31565E-01 c TempK 0.94262E+02 1 0.12034E-05 0.34528E+00 0.65484E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -2.5127e-13 2.0787e-13 -2.5676e-17 -6.3741e-18 v Velocity[Y] -0.0002463 0.00024684 -4.1103e-10 -6.1485e-12 v Velocity[Z] -0.00024684 0.0002463 4.0605e-10 -1.5263e-12 v ǁVelocityǁ 5.0103e-11 0.00029775 1.6051e-05 7.8446e-06 v Pressure -0.00017628 0.0082469 0.00031919 -3.1144e-20 v k 7.3669e-08 0.0058493 0.0039246 0.0044881 v omega 50.506 1.0313e+05 2692.8 532.09 v TempK 288 340.72 291.2 289.11 v Density 1.205 1.205 1.205 1.205 v TurbVisc 8.7582e-13 0.00013132 8.4803e-05 0.00010214 v CourantNb 4.2805e-10 0.00044421 2.4747e-05 1.1798e-05 v FourierNb 0.14997 0.62813 0.26545 0.2192 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.829 4.8291 0.00028567 -5.4784e-08 v volume_forces[Z] -4.829 4.8291 -0.00028561 8.015e-08 v ǁvolume_forcesǁ 1.844e-09 4.8316 0.29099 0.10011 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 291.43 289.25 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.024779 8.3797e-05 4.7855e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14997 0.62813 0.26547 0.21921 INSTANT 0.104967000E+00 TIME STEP NUMBER 109 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15509E-05 0.37196E-02 Friction velocity uk : 0.29860E-05 0.37190E-02 Dimensionless distance yplus : 0.19883E-04 0.24743E-01 Friction thermal sca. tstar : -0.22450E+05 0.00000E+00 Dim-less thermal sca. tplus : 0.13965E-04 0.17378E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15509E-05 0.37196E-02 Friction velocity uk : 0.29860E-05 0.37190E-02 Dimensionless distance yplus : 0.19883E-04 0.24743E-01 Friction thermal sca. tstar : -0.22450E+05 0.00000E+00 Dim-less thermal sca. tplus : 0.13965E-04 0.17378E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.56295E-08 4 0.12503E-05 0.39055E-11 0.23108E+01 c Velocity[X] 0.84065E-30 c Velocity[Y] 0.19527E-11 c Velocity[Z] 0.19528E-11 c Pressure 0.12512E-12 26 0.10227E-07 0.10067E-05 0.75273E+01 c k 0.15139E-05 2 0.95629E-06 0.54562E-06 0.52088E+01 c omega 0.13153E+02 1 0.24985E-07 0.36204E+02 0.31324E-01 c TempK 0.94263E+02 1 0.11906E-05 0.34089E+00 0.65066E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -2.5061e-13 2.0747e-13 -2.5554e-17 -6.3444e-18 v Velocity[Y] -0.00024611 0.00024666 -4.1574e-10 -6.1111e-12 v Velocity[Z] -0.00024666 0.00024611 4.1067e-10 -1.4961e-12 v ǁVelocityǁ 4.9241e-11 0.00029749 1.6056e-05 7.8532e-06 v Pressure -0.00017794 0.008286 0.00032148 2.629e-20 v k 7.243e-08 0.005815 0.0039033 0.0044662 v omega 50.305 1.0313e+05 2692.7 531.91 v TempK 288 340.73 291.21 289.11 v Density 1.205 1.205 1.205 1.205 v TurbVisc 8.6099e-13 0.00013105 8.468e-05 0.00010204 v CourantNb 4.3213e-10 0.00044429 2.4748e-05 1.1807e-05 v FourierNb 0.14993 0.62813 0.26497 0.21891 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.8298 4.8299 0.00028657 -5.7117e-08 v volume_forces[Z] -4.8298 4.8299 -0.00028651 8.297e-08 v ǁvolume_forcesǁ 1.8112e-09 4.8325 0.2919 0.10057 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 291.44 289.26 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.024743 8.3672e-05 4.7782e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14993 0.62813 0.265 0.21892 INSTANT 0.105930000E+00 TIME STEP NUMBER 110 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.14835E-05 0.37142E-02 Friction velocity uk : 0.29162E-05 0.37136E-02 Dimensionless distance yplus : 0.19419E-04 0.24707E-01 Friction thermal sca. tstar : -0.17111E+05 0.00000E+00 Dim-less thermal sca. tplus : 0.13639E-04 0.17352E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.14835E-05 0.37142E-02 Friction velocity uk : 0.29162E-05 0.37136E-02 Dimensionless distance yplus : 0.19419E-04 0.24707E-01 Friction thermal sca. tstar : -0.17111E+05 0.00000E+00 Dim-less thermal sca. tplus : 0.13639E-04 0.17352E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.56325E-08 4 0.12426E-05 0.37483E-11 0.22634E+01 c Velocity[X] 0.85367E-30 c Velocity[Y] 0.18741E-11 c Velocity[Z] 0.18742E-11 c Pressure 0.12376E-12 26 0.10082E-07 0.99556E-06 0.74622E+01 c k 0.15069E-05 2 0.93829E-06 0.53580E-06 0.51867E+01 c omega 0.13153E+02 1 0.24762E-07 0.35656E+02 0.31086E-01 c TempK 0.94264E+02 1 0.11780E-05 0.33660E+00 0.64654E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -2.4994e-13 2.0707e-13 -2.5433e-17 -6.315e-18 v Velocity[Y] -0.0002459 0.00024646 -4.2042e-10 -6.0703e-12 v Velocity[Z] -0.00024647 0.0002459 4.1524e-10 -1.4781e-12 v ǁVelocityǁ 4.8413e-11 0.00029721 1.6059e-05 7.8611e-06 v Pressure -0.00017961 0.0083248 0.00032377 -1.5664e-20 v k 7.1218e-08 0.005781 0.0038822 0.0044446 v omega 50.106 1.0313e+05 2692.5 531.73 v TempK 288 340.73 291.22 289.12 v Density 1.205 1.205 1.205 1.205 v TurbVisc 8.465e-13 0.00013079 8.4558e-05 0.00010194 v CourantNb 4.3622e-10 0.00044433 2.4748e-05 1.1814e-05 v FourierNb 0.1499 0.62813 0.26451 0.21862 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.8306 4.8307 0.00028747 -5.9431e-08 v volume_forces[Z] -4.8306 4.8307 -0.00028741 8.5767e-08 v ǁvolume_forcesǁ 1.78e-09 4.8333 0.29281 0.10102 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 291.45 289.26 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.024707 8.3548e-05 4.7709e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.1499 0.62813 0.26453 0.21863 INSTANT 0.106893000E+00 TIME STEP NUMBER 111 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.14103E-05 0.37088E-02 Friction velocity uk : 0.28433E-05 0.37081E-02 Dimensionless distance yplus : 0.18933E-04 0.24671E-01 Friction thermal sca. tstar : -0.10374E+05 0.00000E+00 Dim-less thermal sca. tplus : 0.13298E-04 0.17327E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.14103E-05 0.37088E-02 Friction velocity uk : 0.28433E-05 0.37081E-02 Dimensionless distance yplus : 0.18933E-04 0.24671E-01 Friction thermal sca. tstar : -0.10374E+05 0.00000E+00 Dim-less thermal sca. tplus : 0.13298E-04 0.17327E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.56351E-08 4 0.12351E-05 0.36054E-11 0.22196E+01 c Velocity[X] 0.86608E-30 c Velocity[Y] 0.18026E-11 c Velocity[Z] 0.18027E-11 c Pressure 0.12263E-12 26 0.99483E-08 0.98623E-06 0.73982E+01 c k 0.14999E-05 2 0.92076E-06 0.52619E-06 0.51648E+01 c omega 0.13153E+02 1 0.24541E-07 0.35118E+02 0.30850E-01 c TempK 0.94265E+02 1 0.11657E-05 0.33240E+00 0.64248E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -2.4926e-13 2.0666e-13 -2.5313e-17 -6.2859e-18 v Velocity[Y] -0.00024568 0.00024625 -4.2507e-10 -6.0294e-12 v Velocity[Z] -0.00024625 0.00024568 4.1979e-10 -1.4599e-12 v ǁVelocityǁ 4.7643e-11 0.00029691 1.6061e-05 7.8684e-06 v Pressure -0.00018127 0.0083635 0.00032605 2.4881e-21 v k 7.0033e-08 0.0057472 0.0038614 0.0044231 v omega 49.909 1.0313e+05 2692.4 531.56 v TempK 288 340.74 291.23 289.12 v Density 1.205 1.205 1.205 1.205 v TurbVisc 8.3233e-13 0.00013052 8.4437e-05 0.00010184 v CourantNb 4.4031e-10 0.00044434 2.4745e-05 1.182e-05 v FourierNb 0.14986 0.62813 0.26404 0.21833 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.8315 4.8316 0.00028836 -6.1728e-08 v volume_forces[Z] -4.8315 4.8316 -0.00028829 8.8543e-08 v ǁvolume_forcesǁ 1.7501e-09 4.8341 0.29371 0.10147 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 291.46 289.27 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.024671 8.3426e-05 4.7637e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14986 0.62813 0.26407 0.21834 INSTANT 0.107856000E+00 TIME STEP NUMBER 112 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.13318E-05 0.37033E-02 Friction velocity uk : 0.27677E-05 0.37027E-02 Dimensionless distance yplus : 0.18430E-04 0.24634E-01 Friction thermal sca. tstar : -0.81220E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.12944E-04 0.17301E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.13318E-05 0.37033E-02 Friction velocity uk : 0.27677E-05 0.37027E-02 Dimensionless distance yplus : 0.18430E-04 0.24634E-01 Friction thermal sca. tstar : -0.81220E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.12944E-04 0.17301E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.56372E-08 4 0.12276E-05 0.34760E-11 0.21793E+01 c Velocity[X] 0.87788E-30 c Velocity[Y] 0.17380E-11 c Velocity[Z] 0.17380E-11 c Pressure 0.12142E-12 26 0.98098E-08 0.97628E-06 0.73353E+01 c k 0.14930E-05 2 0.90369E-06 0.51680E-06 0.51431E+01 c omega 0.13153E+02 1 0.24323E-07 0.34590E+02 0.30618E-01 c TempK 0.94265E+02 1 0.11536E-05 0.32829E+00 0.63848E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -2.4859e-13 2.0625e-13 -2.5195e-17 -6.2571e-18 v Velocity[Y] -0.00024544 0.00024603 -4.2971e-10 -5.9896e-12 v Velocity[Z] -0.00024603 0.00024544 4.243e-10 -1.442e-12 v ǁVelocityǁ 4.6941e-11 0.0002966 1.6063e-05 7.875e-06 v Pressure -0.00018294 0.0084021 0.00032833 3.0642e-22 v k 6.8875e-08 0.0057138 0.0038407 0.0044018 v omega 49.713 1.0313e+05 2692.2 531.38 v TempK 288 340.75 291.24 289.13 v Density 1.205 1.205 1.205 1.205 v TurbVisc 8.1848e-13 0.00013025 8.4318e-05 0.00010175 v CourantNb 4.4441e-10 0.00044432 2.4741e-05 1.1825e-05 v FourierNb 0.14983 0.62813 0.26359 0.21804 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.8323 4.8324 0.00028924 -6.4008e-08 v volume_forces[Z] -4.8323 4.8324 -0.00028918 9.1297e-08 v ǁvolume_forcesǁ 1.7223e-09 4.8349 0.29461 0.10192 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 291.47 289.27 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.024634 8.3302e-05 4.7564e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14983 0.62813 0.26361 0.21805 INSTANT 0.108819000E+00 TIME STEP NUMBER 113 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12473E-05 0.36978E-02 Friction velocity uk : 0.26889E-05 0.36972E-02 Dimensionless distance yplus : 0.17905E-04 0.24598E-01 Friction thermal sca. tstar : -0.68981E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.12575E-04 0.17276E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12473E-05 0.36978E-02 Friction velocity uk : 0.26889E-05 0.36972E-02 Dimensionless distance yplus : 0.17905E-04 0.24598E-01 Friction thermal sca. tstar : -0.68981E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.12575E-04 0.17276E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.56388E-08 4 0.12206E-05 0.33595E-11 0.21425E+01 c Velocity[X] 0.88909E-30 c Velocity[Y] 0.16797E-11 c Velocity[Z] 0.16798E-11 c Pressure 0.12040E-12 26 0.96891E-08 0.96785E-06 0.72734E+01 c k 0.14862E-05 2 0.88707E-06 0.50761E-06 0.51216E+01 c omega 0.13153E+02 1 0.24107E-07 0.34072E+02 0.30388E-01 c TempK 0.94266E+02 1 0.11416E-05 0.32426E+00 0.63454E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -2.4791e-13 2.0582e-13 -2.5077e-17 -6.2285e-18 v Velocity[Y] -0.00024519 0.00024579 -4.3434e-10 -5.9505e-12 v Velocity[Z] -0.00024579 0.0002452 4.2879e-10 -1.4245e-12 v ǁVelocityǁ 4.6317e-11 0.00029627 1.6063e-05 7.881e-06 v Pressure -0.00018461 0.0084404 0.0003306 -2.4391e-21 v k 6.7742e-08 0.0056807 0.0038202 0.0043807 v omega 49.518 1.0313e+05 2692.1 531.21 v TempK 288 340.76 291.25 289.13 v Density 1.205 1.205 1.205 1.205 v TurbVisc 8.0494e-13 0.00012999 8.4199e-05 0.00010165 v CourantNb 4.485e-10 0.00044427 2.4735e-05 1.1829e-05 v FourierNb 0.14979 0.62813 0.26313 0.21776 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.8331 4.8332 0.00029012 -6.6271e-08 v volume_forces[Z] -4.8331 4.8332 -0.00029005 9.403e-08 v ǁvolume_forcesǁ 1.6969e-09 4.8357 0.2955 0.10237 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 291.48 289.28 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.024598 8.3178e-05 4.7491e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14979 0.62813 0.26316 0.21777 INSTANT 0.109782000E+00 TIME STEP NUMBER 114 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11561E-05 0.36923E-02 Friction velocity uk : 0.26068E-05 0.36917E-02 Dimensionless distance yplus : 0.17358E-04 0.24561E-01 Friction thermal sca. tstar : -0.61016E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.12191E-04 0.17250E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11561E-05 0.36923E-02 Friction velocity uk : 0.26068E-05 0.36917E-02 Dimensionless distance yplus : 0.17358E-04 0.24561E-01 Friction thermal sca. tstar : -0.61016E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.12191E-04 0.17250E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.56400E-08 4 0.12132E-05 0.32551E-11 0.21092E+01 c Velocity[X] 0.89966E-30 c Velocity[Y] 0.16275E-11 c Velocity[Z] 0.16276E-11 c Pressure 0.11931E-12 26 0.95616E-08 0.95889E-06 0.72125E+01 c k 0.14794E-05 2 0.87088E-06 0.49862E-06 0.51002E+01 c omega 0.13153E+02 1 0.23894E-07 0.33564E+02 0.30160E-01 c TempK 0.94267E+02 1 0.11299E-05 0.32032E+00 0.63066E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -2.4722e-13 2.0539e-13 -2.4961e-17 -6.2003e-18 v Velocity[Y] -0.00024493 0.00024554 -4.3894e-10 -5.9114e-12 v Velocity[Z] -0.00024554 0.00024494 4.3326e-10 -1.4067e-12 v ǁVelocityǁ 4.5783e-11 0.00029592 1.6061e-05 7.8863e-06 v Pressure -0.00018628 0.0084787 0.00033286 -1.1938e-20 v k 6.6634e-08 0.0056478 0.0038 0.0043598 v omega 49.326 1.0313e+05 2691.9 531.03 v TempK 288 340.77 291.26 289.14 v Density 1.205 1.205 1.205 1.205 v TurbVisc 7.917e-13 0.00012972 8.4081e-05 0.00010155 v CourantNb 4.526e-10 0.00044419 2.4727e-05 1.1832e-05 v FourierNb 0.14976 0.62813 0.26269 0.21747 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.8339 4.834 0.00029099 -6.8517e-08 v volume_forces[Z] -4.8339 4.834 -0.00029093 9.6742e-08 v ǁvolume_forcesǁ 1.6744e-09 4.8365 0.29639 0.10282 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 291.49 289.28 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.024561 8.3053e-05 4.7418e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14976 0.62813 0.26271 0.21749 INSTANT 0.110745000E+00 TIME STEP NUMBER 115 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10573E-05 0.36868E-02 Friction velocity uk : 0.25210E-05 0.36862E-02 Dimensionless distance yplus : 0.16787E-04 0.24524E-01 Friction thermal sca. tstar : -0.55307E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.11790E-04 0.17224E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10573E-05 0.36868E-02 Friction velocity uk : 0.25210E-05 0.36862E-02 Dimensionless distance yplus : 0.16787E-04 0.24524E-01 Friction thermal sca. tstar : -0.55307E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.11790E-04 0.17224E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.56408E-08 4 0.12063E-05 0.31621E-11 0.20792E+01 c Velocity[X] 0.90966E-30 c Velocity[Y] 0.15810E-11 c Velocity[Z] 0.15811E-11 c Pressure 0.11829E-12 26 0.94410E-08 0.95047E-06 0.71525E+01 c k 0.14727E-05 2 0.85510E-06 0.48983E-06 0.50790E+01 c omega 0.13153E+02 1 0.23683E-07 0.33065E+02 0.29935E-01 c TempK 0.94268E+02 1 0.11184E-05 0.31645E+00 0.62683E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -2.4654e-13 2.0495e-13 -2.4846e-17 -6.1723e-18 v Velocity[Y] -0.00024466 0.00024527 -4.4352e-10 -5.8729e-12 v Velocity[Z] -0.00024528 0.00024466 4.377e-10 -1.3893e-12 v ǁVelocityǁ 4.535e-11 0.00029556 1.6059e-05 7.891e-06 v Pressure -0.00018795 0.0085167 0.00033512 2.2062e-22 v k 6.555e-08 0.0056152 0.0037799 0.0043391 v omega 49.134 1.0313e+05 2691.8 530.86 v TempK 288 340.78 291.27 289.14 v Density 1.205 1.205 1.205 1.205 v TurbVisc 7.7874e-13 0.00012946 8.3963e-05 0.00010145 v CourantNb 4.567e-10 0.00044407 2.4717e-05 1.1834e-05 v FourierNb 0.14972 0.62813 0.26224 0.21719 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.8346 4.8347 0.00029186 -7.0746e-08 v volume_forces[Z] -4.8346 4.8347 -0.00029179 9.9433e-08 v ǁvolume_forcesǁ 1.6551e-09 4.8373 0.29727 0.10326 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 291.5 289.29 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.024524 8.2927e-05 4.7344e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14972 0.62813 0.26227 0.21721 INSTANT 0.111708000E+00 TIME STEP NUMBER 116 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.94976E-06 0.36812E-02 Friction velocity uk : 0.24310E-05 0.36806E-02 Dimensionless distance yplus : 0.16188E-04 0.24487E-01 Friction thermal sca. tstar : -0.50960E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.11369E-04 0.17198E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.94976E-06 0.36812E-02 Friction velocity uk : 0.24310E-05 0.36806E-02 Dimensionless distance yplus : 0.16188E-04 0.24487E-01 Friction thermal sca. tstar : -0.50960E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.11369E-04 0.17198E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.56411E-08 4 0.11995E-05 0.30799E-11 0.20525E+01 c Velocity[X] 0.91908E-30 c Velocity[Y] 0.15399E-11 c Velocity[Z] 0.15400E-11 c Pressure 0.11741E-12 26 0.93269E-08 0.94322E-06 0.70936E+01 c k 0.14660E-05 2 0.83973E-06 0.48122E-06 0.50580E+01 c omega 0.13153E+02 1 0.23474E-07 0.32575E+02 0.29713E-01 c TempK 0.94269E+02 1 0.11070E-05 0.31267E+00 0.62306E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -2.4585e-13 2.0451e-13 -2.4732e-17 -6.1446e-18 v Velocity[Y] -0.00024438 0.000245 -4.4809e-10 -5.8354e-12 v Velocity[Z] -0.000245 0.00024438 4.4211e-10 -1.3721e-12 v ǁVelocityǁ 4.5029e-11 0.00029518 1.6056e-05 7.8951e-06 v Pressure -0.00018963 0.0085547 0.00033738 2.9171e-21 v k 6.449e-08 0.0055829 0.00376 0.0043185 v omega 48.944 1.0313e+05 2691.7 530.69 v TempK 288 340.79 291.28 289.14 v Density 1.205 1.205 1.205 1.205 v TurbVisc 7.6607e-13 0.00012919 8.3847e-05 0.00010136 v CourantNb 4.608e-10 0.00044393 2.4706e-05 1.1836e-05 v FourierNb 0.14969 0.62813 0.26181 0.21692 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.8354 4.8355 0.00029272 -7.2959e-08 v volume_forces[Z] -4.8354 4.8355 -0.00029266 1.021e-07 v ǁvolume_forcesǁ 1.6394e-09 4.838 0.29814 0.1037 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 291.51 289.29 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.024487 8.2802e-05 4.7271e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14969 0.62813 0.26183 0.21693 INSTANT 0.112671000E+00 TIME STEP NUMBER 117 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.83220E-06 0.36756E-02 Friction velocity uk : 0.23364E-05 0.36751E-02 Dimensionless distance yplus : 0.15558E-04 0.24450E-01 Friction thermal sca. tstar : -0.47508E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.10927E-04 0.17172E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.83220E-06 0.36756E-02 Friction velocity uk : 0.23364E-05 0.36751E-02 Dimensionless distance yplus : 0.15558E-04 0.24450E-01 Friction thermal sca. tstar : -0.47508E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.10927E-04 0.17172E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.56410E-08 4 0.11926E-05 0.30079E-11 0.20290E+01 c Velocity[X] 0.92790E-30 c Velocity[Y] 0.15039E-11 c Velocity[Z] 0.15040E-11 c Pressure 0.11638E-12 26 0.92097E-08 0.93471E-06 0.70355E+01 c k 0.14594E-05 2 0.82475E-06 0.47280E-06 0.50372E+01 c omega 0.13153E+02 1 0.23269E-07 0.32095E+02 0.29493E-01 c TempK 0.94270E+02 1 0.10959E-05 0.30896E+00 0.61934E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -2.4516e-13 2.0405e-13 -2.4619e-17 -6.1172e-18 v Velocity[Y] -0.00024408 0.00024471 -4.5264e-10 -5.7979e-12 v Velocity[Z] -0.00024471 0.00024408 4.465e-10 -1.3554e-12 v ǁVelocityǁ 4.4832e-11 0.00029478 1.6051e-05 7.8986e-06 v Pressure -0.0001913 0.0085925 0.00033963 -2.3042e-21 v k 6.3453e-08 0.0055508 0.0037403 0.0042982 v omega 48.756 1.0313e+05 2691.5 530.52 v TempK 288 340.79 291.29 289.15 v Density 1.205 1.205 1.205 1.205 v TurbVisc 7.5368e-13 0.00012893 8.3732e-05 0.00010126 v CourantNb 4.6491e-10 0.00044376 2.4694e-05 1.1836e-05 v FourierNb 0.14965 0.62813 0.26137 0.21664 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.8362 4.8363 0.00029358 -7.5155e-08 v volume_forces[Z] -4.8362 4.8363 -0.00029351 1.0475e-07 v ǁvolume_forcesǁ 1.6278e-09 4.8388 0.29901 0.10415 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 291.52 289.3 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.02445 8.2676e-05 4.7197e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14965 0.62813 0.2614 0.21665 INSTANT 0.113634000E+00 TIME STEP NUMBER 118 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.70264E-06 0.36701E-02 Friction velocity uk : 0.22365E-05 0.36695E-02 Dimensionless distance yplus : 0.14893E-04 0.24413E-01 Friction thermal sca. tstar : -0.44682E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.10460E-04 0.17146E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.70264E-06 0.36701E-02 Friction velocity uk : 0.22365E-05 0.36695E-02 Dimensionless distance yplus : 0.14893E-04 0.24413E-01 Friction thermal sca. tstar : -0.44682E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.10460E-04 0.17146E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.56406E-08 4 0.11859E-05 0.29455E-11 0.20086E+01 c Velocity[X] 0.93615E-30 c Velocity[Y] 0.14727E-11 c Velocity[Z] 0.14728E-11 c Pressure 0.11543E-12 26 0.90933E-08 0.92691E-06 0.69784E+01 c k 0.14528E-05 2 0.81015E-06 0.46456E-06 0.50165E+01 c omega 0.13153E+02 1 0.23065E-07 0.31623E+02 0.29275E-01 c TempK 0.94270E+02 1 0.10849E-05 0.30532E+00 0.61568E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -2.4447e-13 2.036e-13 -2.4507e-17 -6.0901e-18 v Velocity[Y] -0.00024377 0.00024441 -4.5717e-10 -5.761e-12 v Velocity[Z] -0.00024441 0.00024378 4.5086e-10 -1.3387e-12 v ǁVelocityǁ 4.477e-11 0.00029438 1.6046e-05 7.9015e-06 v Pressure -0.00019297 0.0086301 0.00034187 2.205e-20 v k 6.2438e-08 0.0055191 0.0037208 0.004278 v omega 48.569 1.0313e+05 2691.4 530.35 v TempK 288 340.8 291.3 289.15 v Density 1.205 1.205 1.205 1.205 v TurbVisc 7.4156e-13 0.00012866 8.3617e-05 0.00010117 v CourantNb 4.6901e-10 0.00044356 2.4679e-05 1.1836e-05 v FourierNb 0.14962 0.62813 0.26094 0.21637 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.8369 4.837 0.00029443 -7.7336e-08 v volume_forces[Z] -4.8369 4.837 -0.00029436 1.0738e-07 v ǁvolume_forcesǁ 1.6207e-09 4.8395 0.29988 0.10459 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 291.53 289.3 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.024413 8.2549e-05 4.7122e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14962 0.62813 0.26097 0.21638 INSTANT 0.114597000E+00 TIME STEP NUMBER 119 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.55888E-06 0.36645E-02 Friction velocity uk : 0.21307E-05 0.36639E-02 Dimensionless distance yplus : 0.14188E-04 0.24376E-01 Friction thermal sca. tstar : -0.42313E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.99650E-05 0.17120E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.55888E-06 0.36645E-02 Friction velocity uk : 0.21307E-05 0.36639E-02 Dimensionless distance yplus : 0.14188E-04 0.24376E-01 Friction thermal sca. tstar : -0.42313E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.99650E-05 0.17120E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.56397E-08 4 0.11793E-05 0.28921E-11 0.19912E+01 c Velocity[X] 0.94384E-30 c Velocity[Y] 0.14460E-11 c Velocity[Z] 0.14461E-11 c Pressure 0.11454E-12 26 0.89825E-08 0.91961E-06 0.69221E+01 c k 0.14463E-05 2 0.79591E-06 0.45649E-06 0.49960E+01 c omega 0.13153E+02 1 0.22864E-07 0.31160E+02 0.29060E-01 c TempK 0.94271E+02 1 0.10742E-05 0.30176E+00 0.61206E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -2.4377e-13 2.0313e-13 -2.4396e-17 -6.0632e-18 v Velocity[Y] -0.00024346 0.0002441 -4.6168e-10 -5.7249e-12 v Velocity[Z] -0.0002441 0.00024346 4.552e-10 -1.3225e-12 v ǁVelocityǁ 4.4853e-11 0.00029396 1.604e-05 7.9038e-06 v Pressure -0.00019465 0.0086676 0.00034411 -1.2159e-20 v k 6.1445e-08 0.0054876 0.0037015 0.0042579 v omega 48.383 1.0313e+05 2691.3 530.19 v TempK 288 340.81 291.31 289.16 v Density 1.205 1.205 1.205 1.205 v TurbVisc 7.2969e-13 0.0001284 8.3504e-05 0.00010107 v CourantNb 4.7312e-10 0.00044333 2.4664e-05 1.1835e-05 v FourierNb 0.14959 0.62813 0.26052 0.2161 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.8377 4.8378 0.00029528 -7.95e-08 v volume_forces[Z] -4.8377 4.8378 -0.00029521 1.1e-07 v ǁvolume_forcesǁ 1.6184e-09 4.8403 0.30074 0.10502 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 291.54 289.31 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.024376 8.2423e-05 4.7048e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14959 0.62813 0.26054 0.21611 INSTANT 0.115560000E+00 TIME STEP NUMBER 120 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.39763E-06 0.36589E-02 Friction velocity uk : 0.20181E-05 0.36583E-02 Dimensionless distance yplus : 0.13438E-04 0.24339E-01 Friction thermal sca. tstar : -0.40291E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.94381E-05 0.17094E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.39763E-06 0.36589E-02 Friction velocity uk : 0.20181E-05 0.36583E-02 Dimensionless distance yplus : 0.13438E-04 0.24339E-01 Friction thermal sca. tstar : -0.40291E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.94381E-05 0.17094E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.56384E-08 4 0.11728E-05 0.28471E-11 0.19766E+01 c Velocity[X] 0.95098E-30 c Velocity[Y] 0.14235E-11 c Velocity[Z] 0.14236E-11 c Pressure 0.11367E-12 26 0.88723E-08 0.91242E-06 0.68667E+01 c k 0.14399E-05 2 0.78203E-06 0.44860E-06 0.49756E+01 c omega 0.13153E+02 1 0.22665E-07 0.30705E+02 0.28847E-01 c TempK 0.94272E+02 1 0.10636E-05 0.29826E+00 0.60849E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -2.4308e-13 2.0266e-13 -2.4287e-17 -6.0366e-18 v Velocity[Y] -0.00024313 0.00024378 -4.6618e-10 -5.689e-12 v Velocity[Z] -0.00024378 0.00024313 4.5952e-10 -1.3064e-12 v ǁVelocityǁ 4.5088e-11 0.00029352 1.6032e-05 7.9056e-06 v Pressure -0.00019633 0.0087049 0.00034635 -2.0346e-21 v k 6.0473e-08 0.0054564 0.0036823 0.0042381 v omega 48.199 1.0313e+05 2691.1 530.02 v TempK 288 340.82 291.32 289.16 v Density 1.205 1.205 1.205 1.205 v TurbVisc 7.1808e-13 0.00012814 8.3391e-05 0.00010098 v CourantNb 4.7723e-10 0.00044308 2.4647e-05 1.1833e-05 v FourierNb 0.14955 0.62813 0.2601 0.21583 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.8384 4.8385 0.00029612 -8.165e-08 v volume_forces[Z] -4.8384 4.8385 -0.00029605 1.1259e-07 v ǁvolume_forcesǁ 1.6214e-09 4.841 0.30159 0.10546 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 291.55 289.31 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.024339 8.2296e-05 4.6974e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14955 0.62813 0.26012 0.21584 INSTANT 0.116523000E+00 TIME STEP NUMBER 121 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.21425E-06 0.36532E-02 Friction velocity uk : 0.18974E-05 0.36527E-02 Dimensionless distance yplus : 0.12634E-04 0.24302E-01 Friction thermal sca. tstar : -0.38540E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.88735E-05 0.17068E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.21425E-06 0.36532E-02 Friction velocity uk : 0.18974E-05 0.36527E-02 Dimensionless distance yplus : 0.12634E-04 0.24302E-01 Friction thermal sca. tstar : -0.38540E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.88735E-05 0.17068E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.56368E-08 4 0.11664E-05 0.28100E-11 0.19648E+01 c Velocity[X] 0.95757E-30 c Velocity[Y] 0.14050E-11 c Velocity[Z] 0.14050E-11 c Pressure 0.11287E-12 26 0.87664E-08 0.90581E-06 0.68122E+01 c k 0.14335E-05 2 0.76849E-06 0.44087E-06 0.49555E+01 c omega 0.13153E+02 1 0.22468E-07 0.30259E+02 0.28637E-01 c TempK 0.94273E+02 1 0.10531E-05 0.29483E+00 0.60498E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -2.4238e-13 2.0218e-13 -2.4178e-17 -6.0103e-18 v Velocity[Y] -0.00024279 0.00024345 -4.7066e-10 -5.6535e-12 v Velocity[Z] -0.00024345 0.00024279 4.6381e-10 -1.2903e-12 v ǁVelocityǁ 4.5482e-11 0.00029308 1.6024e-05 7.9069e-06 v Pressure -0.000198 0.0087421 0.00034858 -8.0648e-21 v k 5.9522e-08 0.0054255 0.0036634 0.0042184 v omega 48.016 1.0313e+05 2691 529.86 v TempK 288 340.83 291.33 289.17 v Density 1.205 1.205 1.205 1.205 v TurbVisc 7.0672e-13 0.00012787 8.3279e-05 0.00010088 v CourantNb 4.8134e-10 0.0004428 2.4628e-05 1.183e-05 v FourierNb 0.14952 0.62813 0.25968 0.21557 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.8392 4.8393 0.00029696 -8.3784e-08 v volume_forces[Z] -4.8392 4.8393 -0.00029689 1.1516e-07 v ǁvolume_forcesǁ 1.6299e-09 4.8417 0.30244 0.1059 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 291.56 289.32 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.024302 8.2169e-05 4.6899e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14952 0.62813 0.2597 0.21558 INSTANT 0.117486000E+00 TIME STEP NUMBER 122 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.83059E-07 0.36476E-02 Friction velocity uk : 0.18081E-05 0.36471E-02 Dimensionless distance yplus : 0.12040E-04 0.24264E-01 Friction thermal sca. tstar : -0.37004E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.84559E-05 0.17042E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.83059E-07 0.36476E-02 Friction velocity uk : 0.18081E-05 0.36471E-02 Dimensionless distance yplus : 0.12040E-04 0.24264E-01 Friction thermal sca. tstar : -0.37004E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.84559E-05 0.17042E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.56347E-08 4 0.11600E-05 0.27804E-11 0.19556E+01 c Velocity[X] 0.96363E-30 c Velocity[Y] 0.13902E-11 c Velocity[Z] 0.13902E-11 c Pressure 0.11202E-12 26 0.86574E-08 0.89882E-06 0.67585E+01 c k 0.14271E-05 2 0.75529E-06 0.43331E-06 0.49355E+01 c omega 0.13153E+02 1 0.22273E-07 0.29820E+02 0.28428E-01 c TempK 0.94274E+02 1 0.10429E-05 0.29147E+00 0.60151E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -2.4168e-13 2.017e-13 -2.4071e-17 -5.9842e-18 v Velocity[Y] -0.00024244 0.00024311 -4.7512e-10 -5.6183e-12 v Velocity[Z] -0.00024311 0.00024245 4.6808e-10 -1.275e-12 v ǁVelocityǁ 4.6041e-11 0.00029262 1.6015e-05 7.9076e-06 v Pressure -0.00019968 0.0087791 0.0003508 1.651e-20 v k 5.859e-08 0.0053948 0.0036446 0.0041989 v omega 47.835 1.0313e+05 2690.9 529.69 v TempK 288 340.83 291.34 289.17 v Density 1.205 1.205 1.205 1.205 v TurbVisc 6.956e-13 0.00012761 8.3168e-05 0.00010079 v CourantNb 4.8546e-10 0.0004425 2.4608e-05 1.1827e-05 v FourierNb 0.14949 0.62813 0.25927 0.2153 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.8399 4.84 0.0002978 -8.5902e-08 v volume_forces[Z] -4.8399 4.84 -0.00029772 1.1771e-07 v ǁvolume_forcesǁ 1.6442e-09 4.8425 0.30329 0.10633 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 291.56 289.32 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.024264 8.2042e-05 4.6824e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14949 0.62813 0.25929 0.21531 INSTANT 0.118449000E+00 TIME STEP NUMBER 123 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.21985E-06 0.36420E-02 Friction velocity uk : 0.18588E-05 0.36414E-02 Dimensionless distance yplus : 0.12377E-04 0.24227E-01 Friction thermal sca. tstar : -0.35642E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.86931E-05 0.17015E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.21985E-06 0.36420E-02 Friction velocity uk : 0.18588E-05 0.36414E-02 Dimensionless distance yplus : 0.12377E-04 0.24227E-01 Friction thermal sca. tstar : -0.35642E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.86931E-05 0.17015E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.56324E-08 4 0.12064E-05 0.27577E-11 0.19489E+01 c Velocity[X] 0.96914E-30 c Velocity[Y] 0.13788E-11 c Velocity[Z] 0.13788E-11 c Pressure 0.11121E-12 26 0.85554E-08 0.89214E-06 0.67056E+01 c k 0.14208E-05 2 0.74242E-06 0.42591E-06 0.49156E+01 c omega 0.13153E+02 1 0.22081E-07 0.29390E+02 0.28222E-01 c TempK 0.94274E+02 1 0.10328E-05 0.28817E+00 0.59808E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -2.4098e-13 2.0121e-13 -2.3964e-17 -5.9584e-18 v Velocity[Y] -0.00024209 0.00024276 -4.7957e-10 -5.5836e-12 v Velocity[Z] -0.00024276 0.00024209 4.7232e-10 -1.2592e-12 v ǁVelocityǁ 4.6766e-11 0.00029215 1.6004e-05 7.9078e-06 v Pressure -0.00020136 0.008816 0.00035302 2.8141e-20 v k 5.7678e-08 0.0053644 0.003626 0.0041795 v omega 47.655 1.0313e+05 2690.7 529.53 v TempK 288 340.84 291.34 289.18 v Density 1.205 1.205 1.205 1.205 v TurbVisc 6.8471e-13 0.00012735 8.3057e-05 0.0001007 v CourantNb 4.8957e-10 0.00044218 2.4587e-05 1.1822e-05 v FourierNb 0.14945 0.62813 0.25886 0.21504 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.8406 4.8407 0.00029862 -8.8006e-08 v volume_forces[Z] -4.8406 4.8407 -0.00029855 1.2025e-07 v ǁvolume_forcesǁ 1.6644e-09 4.8432 0.30413 0.10676 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 291.57 289.33 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.024227 8.1914e-05 4.6749e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14945 0.62813 0.25888 0.21505 INSTANT 0.119412000E+00 TIME STEP NUMBER 124 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.42430E-06 0.36363E-02 Friction velocity uk : 0.19502E-05 0.36358E-02 Dimensionless distance yplus : 0.12987E-04 0.24189E-01 Friction thermal sca. tstar : -0.34426E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.91209E-05 0.16989E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.42430E-06 0.36363E-02 Friction velocity uk : 0.19502E-05 0.36358E-02 Dimensionless distance yplus : 0.12987E-04 0.24189E-01 Friction thermal sca. tstar : -0.34426E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.91209E-05 0.16989E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.56296E-08 4 0.11476E-05 0.27415E-11 0.19446E+01 c Velocity[X] 0.97417E-30 c Velocity[Y] 0.13707E-11 c Velocity[Z] 0.13707E-11 c Pressure 0.11042E-12 26 0.84488E-08 0.88566E-06 0.66535E+01 c k 0.14146E-05 2 0.72985E-06 0.41866E-06 0.48959E+01 c omega 0.13153E+02 1 0.21891E-07 0.28967E+02 0.28019E-01 c TempK 0.94275E+02 1 0.10228E-05 0.28494E+00 0.59470E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -2.4028e-13 2.0072e-13 -2.3859e-17 -5.9328e-18 v Velocity[Y] -0.00024172 0.0002424 -4.8399e-10 -5.5491e-12 v Velocity[Z] -0.0002424 0.00024173 4.7654e-10 -1.2442e-12 v ǁVelocityǁ 4.766e-11 0.00029168 1.5993e-05 7.9075e-06 v Pressure -0.00020304 0.0088528 0.00035523 1.3544e-20 v k 5.6786e-08 0.0053343 0.0036075 0.0041603 v omega 47.476 1.0313e+05 2690.6 529.37 v TempK 288 340.85 291.35 289.18 v Density 1.205 1.205 1.205 1.205 v TurbVisc 6.7405e-13 0.00012709 8.2948e-05 0.00010061 v CourantNb 4.9369e-10 0.00044183 2.4565e-05 1.1817e-05 v FourierNb 0.14942 0.62813 0.25845 0.21478 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.8413 4.8414 0.00029945 -9.0095e-08 v volume_forces[Z] -4.8413 4.8414 -0.00029938 1.2276e-07 v ǁvolume_forcesǁ 1.6906e-09 4.8439 0.30497 0.10719 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 291.58 289.33 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.024189 8.1786e-05 4.6674e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14942 0.62813 0.25848 0.21479 INSTANT 0.120375000E+00 TIME STEP NUMBER 125 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.61461E-06 0.36306E-02 Friction velocity uk : 0.20399E-05 0.36301E-02 Dimensionless distance yplus : 0.13584E-04 0.24151E-01 Friction thermal sca. tstar : -0.33330E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.95403E-05 0.16962E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.61461E-06 0.36306E-02 Friction velocity uk : 0.20399E-05 0.36301E-02 Dimensionless distance yplus : 0.13584E-04 0.24151E-01 Friction thermal sca. tstar : -0.33330E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.95403E-05 0.16962E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.56266E-08 4 0.11413E-05 0.27313E-11 0.19425E+01 c Velocity[X] 0.97867E-30 c Velocity[Y] 0.13657E-11 c Velocity[Z] 0.13657E-11 c Pressure 0.10967E-12 26 0.83407E-08 0.87944E-06 0.66021E+01 c k 0.14084E-05 2 0.71760E-06 0.41156E-06 0.48764E+01 c omega 0.13153E+02 1 0.21703E-07 0.28551E+02 0.27817E-01 c TempK 0.94276E+02 1 0.10131E-05 0.28176E+00 0.59137E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -2.3957e-13 2.0023e-13 -2.3755e-17 -5.9075e-18 v Velocity[Y] -0.00024135 0.00024203 -4.884e-10 -5.5154e-12 v Velocity[Z] -0.00024203 0.00024135 4.8074e-10 -1.2294e-12 v ǁVelocityǁ 4.8721e-11 0.0002912 1.5981e-05 7.9067e-06 v Pressure -0.00020472 0.0088894 0.00035744 -1.8385e-20 v k 5.5911e-08 0.0053044 0.0035892 0.0041413 v omega 47.299 1.0313e+05 2690.5 529.21 v TempK 288 340.86 291.36 289.19 v Density 1.205 1.205 1.205 1.205 v TurbVisc 6.6361e-13 0.00012683 8.2839e-05 0.00010051 v CourantNb 4.9781e-10 0.00044145 2.4541e-05 1.1812e-05 v FourierNb 0.14939 0.62813 0.25805 0.21452 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.842 4.8421 0.00030027 -9.2169e-08 v volume_forces[Z] -4.842 4.8421 -0.0003002 1.2526e-07 v ǁvolume_forcesǁ 1.7229e-09 4.8446 0.3058 0.10762 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 291.59 289.33 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.024151 8.1659e-05 4.66e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14939 0.62813 0.25808 0.21454 INSTANT 0.121338000E+00 TIME STEP NUMBER 126 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.79292E-06 0.36250E-02 Friction velocity uk : 0.21280E-05 0.36244E-02 Dimensionless distance yplus : 0.14170E-04 0.24114E-01 Friction thermal sca. tstar : -0.32336E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.99521E-05 0.16936E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.79292E-06 0.36250E-02 Friction velocity uk : 0.21280E-05 0.36244E-02 Dimensionless distance yplus : 0.14170E-04 0.24114E-01 Friction thermal sca. tstar : -0.32336E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.99521E-05 0.16936E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.56231E-08 4 0.11352E-05 0.27268E-11 0.19426E+01 c Velocity[X] 0.98270E-30 c Velocity[Y] 0.13634E-11 c Velocity[Z] 0.13634E-11 c Pressure 0.10892E-12 26 0.82385E-08 0.87326E-06 0.65515E+01 c k 0.14022E-05 2 0.70563E-06 0.40461E-06 0.48570E+01 c omega 0.13153E+02 1 0.21517E-07 0.28143E+02 0.27618E-01 c TempK 0.94277E+02 1 0.10034E-05 0.27864E+00 0.58808E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -2.3887e-13 1.9972e-13 -2.3652e-17 -5.8825e-18 v Velocity[Y] -0.00024097 0.00024165 -4.9279e-10 -5.4817e-12 v Velocity[Z] -0.00024166 0.00024097 4.8491e-10 -1.2149e-12 v ǁVelocityǁ 4.9947e-11 0.0002907 1.5969e-05 7.9055e-06 v Pressure -0.0002064 0.0089259 0.00035965 -3.677e-21 v k 5.5055e-08 0.0052748 0.0035711 0.0041224 v omega 47.123 1.0313e+05 2690.3 529.05 v TempK 288 340.86 291.37 289.19 v Density 1.205 1.205 1.205 1.205 v TurbVisc 6.5339e-13 0.00012657 8.2731e-05 0.00010042 v CourantNb 5.0193e-10 0.00044106 2.4516e-05 1.1805e-05 v FourierNb 0.14935 0.62812 0.25766 0.21427 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.8427 4.8428 0.00030108 -9.4229e-08 v volume_forces[Z] -4.8427 4.8428 -0.00030101 1.2774e-07 v ǁvolume_forcesǁ 1.7613e-09 4.8453 0.30662 0.10805 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 291.6 289.34 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.024114 8.1531e-05 4.6524e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14935 0.62812 0.25768 0.21428 INSTANT 0.122301000E+00 TIME STEP NUMBER 127 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.96094E-06 0.36193E-02 Friction velocity uk : 0.22146E-05 0.36188E-02 Dimensionless distance yplus : 0.14747E-04 0.24076E-01 Friction thermal sca. tstar : -0.31431E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.10357E-04 0.16909E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.96094E-06 0.36193E-02 Friction velocity uk : 0.22146E-05 0.36188E-02 Dimensionless distance yplus : 0.14747E-04 0.24076E-01 Friction thermal sca. tstar : -0.31431E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.10357E-04 0.16909E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.56194E-08 4 0.11292E-05 0.27276E-11 0.19446E+01 c Velocity[X] 0.98625E-30 c Velocity[Y] 0.13638E-11 c Velocity[Z] 0.13638E-11 c Pressure 0.10822E-12 26 0.81364E-08 0.86748E-06 0.65017E+01 c k 0.13962E-05 2 0.69396E-06 0.39780E-06 0.48378E+01 c omega 0.13153E+02 1 0.21333E-07 0.27742E+02 0.27420E-01 c TempK 0.94278E+02 1 0.99397E-06 0.27559E+00 0.58484E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -2.3816e-13 1.9922e-13 -2.355e-17 -5.8577e-18 v Velocity[Y] -0.00024058 0.00024127 -4.9717e-10 -5.4533e-12 v Velocity[Z] -0.00024127 0.00024058 4.8905e-10 -1.1994e-12 v ǁVelocityǁ 5.1336e-11 0.0002902 1.5955e-05 7.9037e-06 v Pressure -0.00020808 0.0089623 0.00036184 4.6575e-22 v k 5.4216e-08 0.0052454 0.0035532 0.0041037 v omega 46.948 1.0313e+05 2690.2 528.89 v TempK 288 340.87 291.38 289.2 v Density 1.205 1.205 1.205 1.205 v TurbVisc 6.4338e-13 0.00012631 8.2624e-05 0.00010033 v CourantNb 5.0605e-10 0.00044064 2.449e-05 1.1798e-05 v FourierNb 0.14932 0.62812 0.25727 0.21402 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.8434 4.8435 0.0003019 -9.6274e-08 v volume_forces[Z] -4.8434 4.8435 -0.00030182 1.302e-07 v ǁvolume_forcesǁ 1.8056e-09 4.8459 0.30745 0.10847 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 291.61 289.34 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.024076 8.1403e-05 4.6449e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14932 0.62812 0.25729 0.21403 INSTANT 0.123264000E+00 TIME STEP NUMBER 128 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11203E-05 0.36136E-02 Friction velocity uk : 0.23000E-05 0.36131E-02 Dimensionless distance yplus : 0.15316E-04 0.24038E-01 Friction thermal sca. tstar : -0.30601E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.10757E-04 0.16883E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11203E-05 0.36136E-02 Friction velocity uk : 0.23000E-05 0.36131E-02 Dimensionless distance yplus : 0.15316E-04 0.24038E-01 Friction thermal sca. tstar : -0.30601E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.10757E-04 0.16883E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.56153E-08 4 0.11232E-05 0.27332E-11 0.19484E+01 c Velocity[X] 0.98932E-30 c Velocity[Y] 0.13666E-11 c Velocity[Z] 0.13666E-11 c Pressure 0.10758E-12 26 0.80413E-08 0.86218E-06 0.64526E+01 c k 0.13901E-05 2 0.68256E-06 0.39113E-06 0.48187E+01 c omega 0.13153E+02 1 0.21152E-07 0.27348E+02 0.27225E-01 c TempK 0.94278E+02 1 0.98465E-06 0.27258E+00 0.58163E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -2.3746e-13 1.9871e-13 -2.3448e-17 -5.8331e-18 v Velocity[Y] -0.00024018 0.00024088 -5.0152e-10 -5.4204e-12 v Velocity[Z] -0.00024088 0.00024019 4.9317e-10 -1.1849e-12 v ǁVelocityǁ 5.2882e-11 0.00028969 1.5941e-05 7.9015e-06 v Pressure -0.00020976 0.0089985 0.00036404 3.4931e-21 v k 5.3395e-08 0.0052163 0.0035354 0.0040851 v omega 46.775 1.0313e+05 2690.1 528.74 v TempK 288 340.88 291.39 289.2 v Density 1.205 1.205 1.205 1.205 v TurbVisc 6.3357e-13 0.00012606 8.2517e-05 0.00010024 v CourantNb 5.1017e-10 0.00044021 2.4462e-05 1.179e-05 v FourierNb 0.14929 0.62812 0.25688 0.21376 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.8441 4.8441 0.0003027 -9.8306e-08 v volume_forces[Z] -4.8441 4.8441 -0.00030263 1.3264e-07 v ǁvolume_forcesǁ 1.8558e-09 4.8466 0.30826 0.1089 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 291.62 289.35 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.024038 8.1275e-05 4.6374e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14929 0.62812 0.2569 0.21378 INSTANT 0.124227000E+00 TIME STEP NUMBER 129 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12717E-05 0.36079E-02 Friction velocity uk : 0.23842E-05 0.36074E-02 Dimensionless distance yplus : 0.15876E-04 0.24000E-01 Friction thermal sca. tstar : -0.29836E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.11150E-04 0.16856E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12717E-05 0.36079E-02 Friction velocity uk : 0.23842E-05 0.36074E-02 Dimensionless distance yplus : 0.15876E-04 0.24000E-01 Friction thermal sca. tstar : -0.29836E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.11150E-04 0.16856E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.56110E-08 4 0.11174E-05 0.27433E-11 0.19540E+01 c Velocity[X] 0.99196E-30 c Velocity[Y] 0.13717E-11 c Velocity[Z] 0.13717E-11 c Pressure 0.10682E-12 26 0.79345E-08 0.85596E-06 0.64042E+01 c k 0.13841E-05 2 0.67144E-06 0.38460E-06 0.47998E+01 c omega 0.13153E+02 1 0.20972E-07 0.26962E+02 0.27032E-01 c TempK 0.94279E+02 1 0.97547E-06 0.26964E+00 0.57847E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -2.3675e-13 1.982e-13 -2.3348e-17 -5.8088e-18 v Velocity[Y] -0.00023978 0.00024048 -5.0586e-10 -5.3896e-12 v Velocity[Z] -0.00024048 0.00023978 4.9727e-10 -1.1702e-12 v ǁVelocityǁ 5.4577e-11 0.00028916 1.5926e-05 7.8989e-06 v Pressure -0.00021144 0.0090346 0.00036623 -2.5592e-20 v k 5.259e-08 0.0051874 0.0035178 0.0040667 v omega 46.602 1.0313e+05 2690 528.58 v TempK 288 340.89 291.4 289.21 v Density 1.205 1.205 1.205 1.205 v TurbVisc 6.2397e-13 0.0001258 8.2412e-05 0.00010015 v CourantNb 5.143e-10 0.00043975 2.4434e-05 1.1782e-05 v FourierNb 0.14926 0.62812 0.25649 0.21352 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.8447 4.8448 0.0003035 -1.0032e-07 v volume_forces[Z] -4.8447 4.8448 -0.00030343 1.3507e-07 v ǁvolume_forcesǁ 1.9117e-09 4.8473 0.30908 0.10932 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 291.63 289.35 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.024 8.1147e-05 4.6299e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14926 0.62812 0.25652 0.21353 INSTANT 0.125190000E+00 TIME STEP NUMBER 130 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.14162E-05 0.36022E-02 Friction velocity uk : 0.24672E-05 0.36017E-02 Dimensionless distance yplus : 0.16429E-04 0.23963E-01 Friction thermal sca. tstar : -0.29130E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.11538E-04 0.16830E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.14162E-05 0.36022E-02 Friction velocity uk : 0.24672E-05 0.36017E-02 Dimensionless distance yplus : 0.16429E-04 0.23963E-01 Friction thermal sca. tstar : -0.29130E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.11538E-04 0.16830E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.56063E-08 4 0.11115E-05 0.27576E-11 0.19611E+01 c Velocity[X] 0.99415E-30 c Velocity[Y] 0.13788E-11 c Velocity[Z] 0.13788E-11 c Pressure 0.10612E-12 26 0.78355E-08 0.85014E-06 0.63565E+01 c k 0.13782E-05 2 0.66057E-06 0.37821E-06 0.47810E+01 c omega 0.13153E+02 1 0.20794E-07 0.26581E+02 0.26840E-01 c TempK 0.94280E+02 1 0.96644E-06 0.26674E+00 0.57535E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -2.3605e-13 1.9768e-13 -2.3249e-17 -5.7847e-18 v Velocity[Y] -0.00023937 0.00024007 -5.1017e-10 -5.3568e-12 v Velocity[Z] -0.00024007 0.00023937 5.0134e-10 -1.1564e-12 v ǁVelocityǁ 5.6418e-11 0.00028863 1.591e-05 7.8958e-06 v Pressure -0.00021313 0.0090706 0.00036841 7.1211e-21 v k 5.1801e-08 0.0051587 0.0035003 0.0040484 v omega 46.431 1.0313e+05 2689.8 528.42 v TempK 288 340.89 291.41 289.21 v Density 1.205 1.205 1.205 1.205 v TurbVisc 6.1456e-13 0.00012554 8.2306e-05 0.00010006 v CourantNb 5.1843e-10 0.00043927 2.4404e-05 1.1773e-05 v FourierNb 0.14922 0.62812 0.25611 0.21327 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.8454 4.8455 0.0003043 -1.0233e-07 v volume_forces[Z] -4.8454 4.8455 -0.00030423 1.3747e-07 v ǁvolume_forcesǁ 1.973e-09 4.8479 0.30989 0.10974 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 291.64 289.36 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.023963 8.1019e-05 4.6224e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14923 0.62812 0.25613 0.21328 INSTANT 0.126153000E+00 TIME STEP NUMBER 131 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15547E-05 0.35965E-02 Friction velocity uk : 0.25492E-05 0.35960E-02 Dimensionless distance yplus : 0.16975E-04 0.23925E-01 Friction thermal sca. tstar : -0.28475E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.11922E-04 0.16803E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15547E-05 0.35965E-02 Friction velocity uk : 0.25492E-05 0.35960E-02 Dimensionless distance yplus : 0.16975E-04 0.23925E-01 Friction thermal sca. tstar : -0.28475E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.11922E-04 0.16803E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.56013E-08 4 0.11301E-05 0.27756E-11 0.19696E+01 c Velocity[X] 0.99590E-30 c Velocity[Y] 0.13878E-11 c Velocity[Z] 0.13878E-11 c Pressure 0.10545E-12 26 0.77378E-08 0.84465E-06 0.63095E+01 c k 0.13722E-05 2 0.64996E-06 0.37194E-06 0.47624E+01 c omega 0.13153E+02 1 0.20619E-07 0.26208E+02 0.26651E-01 c TempK 0.94281E+02 1 0.95754E-06 0.26390E+00 0.57226E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -2.3534e-13 1.9716e-13 -2.3151e-17 -5.7609e-18 v Velocity[Y] -0.00023895 0.00023965 -5.1447e-10 -5.3241e-12 v Velocity[Z] -0.00023965 0.00023895 5.0538e-10 -1.1432e-12 v ǁVelocityǁ 5.8397e-11 0.00028809 1.5894e-05 7.8923e-06 v Pressure -0.00021481 0.0091064 0.00037059 2.3386e-20 v k 5.1028e-08 0.0051302 0.003483 0.0040303 v omega 46.262 1.0313e+05 2689.7 528.27 v TempK 288 340.9 291.42 289.22 v Density 1.205 1.205 1.205 1.205 v TurbVisc 6.0534e-13 0.00012528 8.2202e-05 9.9975e-05 v CourantNb 5.2256e-10 0.00043878 2.4374e-05 1.1763e-05 v FourierNb 0.14919 0.62812 0.25573 0.21302 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.846 4.8461 0.0003051 -1.0432e-07 v volume_forces[Z] -4.846 4.8461 -0.00030502 1.3987e-07 v ǁvolume_forcesǁ 2.0395e-09 4.8486 0.31069 0.11016 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 291.65 289.36 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.023925 8.089e-05 4.6149e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14919 0.62812 0.25576 0.21303 INSTANT 0.127116000E+00 TIME STEP NUMBER 132 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.16878E-05 0.35908E-02 Friction velocity uk : 0.26302E-05 0.35903E-02 Dimensionless distance yplus : 0.17514E-04 0.23887E-01 Friction thermal sca. tstar : -0.27865E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.12301E-04 0.16777E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.16878E-05 0.35908E-02 Friction velocity uk : 0.26302E-05 0.35903E-02 Dimensionless distance yplus : 0.17514E-04 0.23887E-01 Friction thermal sca. tstar : -0.27865E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.12301E-04 0.16777E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.55960E-08 4 0.10999E-05 0.27972E-11 0.19795E+01 c Velocity[X] 0.99724E-30 c Velocity[Y] 0.13986E-11 c Velocity[Z] 0.13986E-11 c Pressure 0.10483E-12 26 0.76416E-08 0.83953E-06 0.62631E+01 c k 0.13664E-05 2 0.63960E-06 0.36580E-06 0.47439E+01 c omega 0.13153E+02 1 0.20445E-07 0.25841E+02 0.26464E-01 c TempK 0.94282E+02 1 0.94878E-06 0.26111E+00 0.56922E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -2.3464e-13 1.9664e-13 -2.3053e-17 -5.7373e-18 v Velocity[Y] -0.00023853 0.00023923 -5.1875e-10 -5.2925e-12 v Velocity[Z] -0.00023923 0.00023853 5.0941e-10 -1.1304e-12 v ǁVelocityǁ 6.0507e-11 0.00028754 1.5876e-05 7.8884e-06 v Pressure -0.00021649 0.0091421 0.00037276 -2.3312e-20 v k 5.0271e-08 0.005102 0.0034659 0.0040123 v omega 46.093 1.0313e+05 2689.6 528.12 v TempK 288 340.91 291.43 289.22 v Density 1.205 1.205 1.205 1.205 v TurbVisc 5.9631e-13 0.00012503 8.2099e-05 9.9887e-05 v CourantNb 5.2669e-10 0.00043826 2.4342e-05 1.1753e-05 v FourierNb 0.14916 0.62812 0.25536 0.21278 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.8467 4.8468 0.00030589 -1.0629e-07 v volume_forces[Z] -4.8467 4.8468 -0.00030581 1.4224e-07 v ǁvolume_forcesǁ 2.111e-09 4.8492 0.31149 0.11058 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 291.65 289.37 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.023887 8.0762e-05 4.6074e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14916 0.62812 0.25538 0.21279 INSTANT 0.128079000E+00 TIME STEP NUMBER 133 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.18160E-05 0.35852E-02 Friction velocity uk : 0.27104E-05 0.35847E-02 Dimensionless distance yplus : 0.18048E-04 0.23849E-01 Friction thermal sca. tstar : -0.27295E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.12676E-04 0.16750E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.18160E-05 0.35852E-02 Friction velocity uk : 0.27104E-05 0.35847E-02 Dimensionless distance yplus : 0.18048E-04 0.23849E-01 Friction thermal sca. tstar : -0.27295E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.12676E-04 0.16750E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.55905E-08 4 0.10942E-05 0.28220E-11 0.19906E+01 c Velocity[X] 0.99816E-30 c Velocity[Y] 0.14110E-11 c Velocity[Z] 0.14110E-11 c Pressure 0.10423E-12 26 0.75527E-08 0.83463E-06 0.62174E+01 c k 0.13606E-05 2 0.62948E-06 0.35979E-06 0.47255E+01 c omega 0.13153E+02 1 0.20273E-07 0.25480E+02 0.26278E-01 c TempK 0.94283E+02 1 0.94015E-06 0.25836E+00 0.56621E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -2.3393e-13 1.9611e-13 -2.2957e-17 -5.714e-18 v Velocity[Y] -0.0002381 0.0002388 -5.2301e-10 -5.261e-12 v Velocity[Z] -0.0002388 0.0002381 5.1341e-10 -1.1174e-12 v ǁVelocityǁ 6.2743e-11 0.00028698 1.5858e-05 7.8841e-06 v Pressure -0.00021818 0.0091777 0.00037493 -2.6585e-20 v k 4.9529e-08 0.0050741 0.0034489 0.0039945 v omega 45.926 1.0313e+05 2689.5 527.97 v TempK 288 340.91 291.43 289.23 v Density 1.205 1.205 1.205 1.205 v TurbVisc 5.8745e-13 0.00012484 8.1996e-05 9.9799e-05 v CourantNb 5.3082e-10 0.00043773 2.4309e-05 1.1742e-05 v FourierNb 0.14913 0.62812 0.25499 0.21254 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.8473 4.8474 0.00030667 -1.0826e-07 v volume_forces[Z] -4.8473 4.8474 -0.00030659 1.446e-07 v ǁvolume_forcesǁ 2.1873e-09 4.8499 0.31229 0.11099 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 291.66 289.37 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.023849 8.0634e-05 4.5999e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14913 0.62812 0.25501 0.21255 INSTANT 0.129042000E+00 TIME STEP NUMBER 134 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19398E-05 0.35795E-02 Friction velocity uk : 0.27897E-05 0.35790E-02 Dimensionless distance yplus : 0.18576E-04 0.23811E-01 Friction thermal sca. tstar : -0.26762E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.13047E-04 0.16723E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19398E-05 0.35795E-02 Friction velocity uk : 0.27897E-05 0.35790E-02 Dimensionless distance yplus : 0.18576E-04 0.23811E-01 Friction thermal sca. tstar : -0.26762E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.13047E-04 0.16723E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.55846E-08 4 0.10886E-05 0.28497E-11 0.20028E+01 c Velocity[X] 0.99868E-30 c Velocity[Y] 0.14248E-11 c Velocity[Z] 0.14248E-11 c Pressure 0.10356E-12 26 0.74596E-08 0.82910E-06 0.61723E+01 c k 0.13548E-05 2 0.61960E-06 0.35389E-06 0.47073E+01 c omega 0.13153E+02 1 0.20103E-07 0.25125E+02 0.26095E-01 c TempK 0.94283E+02 1 0.93165E-06 0.25567E+00 0.56324E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -2.3323e-13 1.9558e-13 -2.2862e-17 -5.6908e-18 v Velocity[Y] -0.00023766 0.00023837 -5.2728e-10 -5.2557e-12 v Velocity[Z] -0.00023837 0.00023766 5.1737e-10 -1.1155e-12 v ǁVelocityǁ 6.5128e-11 0.00028641 1.584e-05 7.8794e-06 v Pressure -0.00021987 0.0092132 0.0003771 -3.6917e-20 v k 4.8801e-08 0.0050466 0.003432 0.0039768 v omega 45.76 1.0313e+05 2689.3 527.82 v TempK 288 340.92 291.44 289.23 v Density 1.205 1.205 1.205 1.205 v TurbVisc 5.7877e-13 0.00012465 8.1893e-05 9.9712e-05 v CourantNb 5.3494e-10 0.00043718 2.4275e-05 1.1731e-05 v FourierNb 0.1491 0.62812 0.25462 0.2123 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.848 4.8481 0.00030745 -1.1021e-07 v volume_forces[Z] -4.848 4.8481 -0.00030738 1.4694e-07 v ǁvolume_forcesǁ 2.2682e-09 4.8505 0.31308 0.11141 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 291.67 289.38 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.023811 8.0506e-05 4.5924e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.1491 0.62812 0.25464 0.21231 INSTANT 0.130005000E+00 TIME STEP NUMBER 135 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.20611E-05 0.35738E-02 Friction velocity uk : 0.28694E-05 0.35733E-02 Dimensionless distance yplus : 0.19107E-04 0.23773E-01 Friction thermal sca. tstar : -0.26261E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.13419E-04 0.16697E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.20611E-05 0.35738E-02 Friction velocity uk : 0.28694E-05 0.35733E-02 Dimensionless distance yplus : 0.19107E-04 0.23773E-01 Friction thermal sca. tstar : -0.26261E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.13419E-04 0.16697E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.55785E-08 4 0.10830E-05 0.28800E-11 0.20160E+01 c Velocity[X] 0.99883E-30 c Velocity[Y] 0.14400E-11 c Velocity[Z] 0.14400E-11 c Pressure 0.10292E-12 26 0.73682E-08 0.82385E-06 0.61279E+01 c k 0.13491E-05 2 0.60994E-06 0.34812E-06 0.46893E+01 c omega 0.13153E+02 1 0.19935E-07 0.24776E+02 0.25913E-01 c TempK 0.94284E+02 1 0.92328E-06 0.25302E+00 0.56031E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -2.3252e-13 1.9505e-13 -2.2767e-17 -5.6679e-18 v Velocity[Y] -0.00023722 0.00023792 -5.3148e-10 -5.1937e-12 v Velocity[Z] -0.00023793 0.00023722 5.214e-10 -1.0354e-12 v ǁVelocityǁ 6.7574e-11 0.00028583 1.5821e-05 7.8743e-06 v Pressure -0.00022155 0.0092485 0.00037926 5.5155e-21 v k 4.8088e-08 0.0050208 0.0034153 0.0039592 v omega 45.595 1.0313e+05 2689.2 527.67 v TempK 288 340.93 291.45 289.23 v Density 1.205 1.205 1.205 1.205 v TurbVisc 5.7027e-13 0.00012446 8.1792e-05 9.9625e-05 v CourantNb 5.3909e-10 0.00043661 2.4241e-05 1.1719e-05 v FourierNb 0.14907 0.62812 0.25425 0.21206 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.8486 4.8487 0.00030823 -1.1214e-07 v volume_forces[Z] -4.8486 4.8487 -0.00030815 1.4926e-07 v ǁvolume_forcesǁ 2.3544e-09 4.8511 0.31387 0.11182 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 291.68 289.38 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.023773 8.0378e-05 4.5848e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14907 0.62812 0.25428 0.21207 INSTANT 0.130968000E+00 TIME STEP NUMBER 136 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.21761E-05 0.35681E-02 Friction velocity uk : 0.29462E-05 0.35676E-02 Dimensionless distance yplus : 0.19618E-04 0.23735E-01 Friction thermal sca. tstar : -0.25790E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.13779E-04 0.16670E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.21761E-05 0.35681E-02 Friction velocity uk : 0.29462E-05 0.35676E-02 Dimensionless distance yplus : 0.19618E-04 0.23735E-01 Friction thermal sca. tstar : -0.25790E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.13779E-04 0.16670E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.55722E-08 4 0.10774E-05 0.29127E-11 0.20301E+01 c Velocity[X] 0.99781E-30 c Velocity[Y] 0.14564E-11 c Velocity[Z] 0.14564E-11 c Pressure 0.10229E-12 25 0.11301E-07 0.81863E-06 0.60840E+01 c k 0.13434E-05 2 0.60050E-06 0.34246E-06 0.46713E+01 c omega 0.13153E+02 1 0.19769E-07 0.24434E+02 0.25733E-01 c TempK 0.94285E+02 1 0.91504E-06 0.25042E+00 0.55741E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -2.3182e-13 1.9451e-13 -2.2674e-17 -5.6454e-18 v Velocity[Y] -0.00023677 0.00023748 -5.3569e-10 -5.1675e-12 v Velocity[Z] -0.00023748 0.00023678 5.2533e-10 -1.0207e-12 v ǁVelocityǁ 7.0197e-11 0.00028525 1.5801e-05 7.8688e-06 v Pressure -0.00022324 0.0092837 0.00038141 2.1449e-20 v k 4.7389e-08 0.0049952 0.0033987 0.0039418 v omega 45.432 1.0313e+05 2689.1 527.52 v TempK 288 340.93 291.46 289.24 v Density 1.205 1.205 1.205 1.205 v TurbVisc 5.6193e-13 0.00012427 8.1691e-05 9.9539e-05 v CourantNb 5.4327e-10 0.00043602 2.4205e-05 1.1707e-05 v FourierNb 0.14904 0.62812 0.25389 0.21182 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.8492 4.8493 0.000309 -1.1407e-07 v volume_forces[Z] -4.8492 4.8493 -0.00030893 1.5157e-07 v ǁvolume_forcesǁ 2.4428e-09 4.8517 0.31465 0.11224 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 291.69 289.39 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.023735 8.025e-05 4.5773e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14904 0.62812 0.25392 0.21183 INSTANT 0.131931000E+00 TIME STEP NUMBER 137 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.22909E-05 0.35624E-02 Friction velocity uk : 0.30248E-05 0.35619E-02 Dimensionless distance yplus : 0.20142E-04 0.23697E-01 Friction thermal sca. tstar : -0.25346E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.14146E-04 0.16644E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.22909E-05 0.35624E-02 Friction velocity uk : 0.30248E-05 0.35619E-02 Dimensionless distance yplus : 0.20142E-04 0.23697E-01 Friction thermal sca. tstar : -0.25346E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.14146E-04 0.16644E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.55655E-08 4 0.10764E-05 0.29476E-11 0.20450E+01 c Velocity[X] 0.99794E-30 c Velocity[Y] 0.14738E-11 c Velocity[Z] 0.14738E-11 c Pressure 0.10181E-12 25 0.11206E-07 0.81466E-06 0.60408E+01 c k 0.13378E-05 2 0.59127E-06 0.33691E-06 0.46535E+01 c omega 0.13153E+02 1 0.19605E-07 0.24097E+02 0.25555E-01 c TempK 0.94286E+02 1 0.90691E-06 0.24786E+00 0.55455E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -2.3112e-13 1.9398e-13 -2.2582e-17 -5.6229e-18 v Velocity[Y] -0.00023632 0.00023703 -5.3987e-10 -5.137e-12 v Velocity[Z] -0.00023703 0.00023632 5.2924e-10 -1.0092e-12 v ǁVelocityǁ 7.2895e-11 0.00028466 1.578e-05 7.863e-06 v Pressure -0.00022493 0.0093188 0.00038356 -1.7527e-20 v k 4.6703e-08 0.0049699 0.0033823 0.0039246 v omega 45.269 1.0313e+05 2689 527.37 v TempK 288 340.94 291.47 289.24 v Density 1.205 1.205 1.205 1.205 v TurbVisc 5.5376e-13 0.00012407 8.1591e-05 9.9453e-05 v CourantNb 5.4741e-10 0.00043542 2.4169e-05 1.1694e-05 v FourierNb 0.149 0.62812 0.25353 0.21159 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.8498 4.8499 0.00030977 -1.1598e-07 v volume_forces[Z] -4.8498 4.8499 -0.00030969 1.5386e-07 v ǁvolume_forcesǁ 2.5376e-09 4.8523 0.31543 0.11265 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 291.7 289.39 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.023697 8.0122e-05 4.5698e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14901 0.62812 0.25356 0.2116 INSTANT 0.132894000E+00 TIME STEP NUMBER 138 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.24016E-05 0.35567E-02 Friction velocity uk : 0.31018E-05 0.35562E-02 Dimensionless distance yplus : 0.20655E-04 0.23660E-01 Friction thermal sca. tstar : -0.24926E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.14507E-04 0.16617E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.24016E-05 0.35567E-02 Friction velocity uk : 0.31018E-05 0.35562E-02 Dimensionless distance yplus : 0.20655E-04 0.23660E-01 Friction thermal sca. tstar : -0.24926E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.14507E-04 0.16617E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.55587E-08 4 0.10672E-05 0.29844E-11 0.20606E+01 c Velocity[X] 0.99707E-30 c Velocity[Y] 0.14922E-11 c Velocity[Z] 0.14922E-11 c Pressure 0.10127E-12 25 0.11122E-07 0.81020E-06 0.59981E+01 c k 0.13322E-05 2 0.58226E-06 0.33147E-06 0.46359E+01 c omega 0.13153E+02 1 0.19443E-07 0.23766E+02 0.25379E-01 c TempK 0.94287E+02 1 0.89891E-06 0.24535E+00 0.55172E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -2.3041e-13 1.9344e-13 -2.249e-17 -5.6007e-18 v Velocity[Y] -0.00023586 0.00023657 -5.4405e-10 -5.1067e-12 v Velocity[Z] -0.00023657 0.00023587 5.3313e-10 -9.9793e-13 v ǁVelocityǁ 7.5681e-11 0.00028406 1.5759e-05 7.8568e-06 v Pressure -0.00022662 0.0093538 0.00038571 6.7779e-21 v k 4.6031e-08 0.0049446 0.0033661 0.0039075 v omega 45.108 1.0313e+05 2688.8 527.22 v TempK 288 340.95 291.48 289.25 v Density 1.205 1.205 1.205 1.205 v TurbVisc 5.4574e-13 0.00012388 8.1491e-05 9.9367e-05 v CourantNb 5.5155e-10 0.0004348 2.4131e-05 1.168e-05 v FourierNb 0.14897 0.62812 0.25318 0.21135 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.8504 4.8505 0.00031054 -1.1788e-07 v volume_forces[Z] -4.8504 4.8505 -0.00031046 1.5614e-07 v ǁvolume_forcesǁ 2.6352e-09 4.8529 0.31621 0.11306 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 291.71 289.39 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.02366 7.9995e-05 4.5624e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14897 0.62812 0.2532 0.21136 INSTANT 0.133857000E+00 TIME STEP NUMBER 139 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.25092E-05 0.35510E-02 Friction velocity uk : 0.31780E-05 0.35505E-02 Dimensionless distance yplus : 0.21162E-04 0.23622E-01 Friction thermal sca. tstar : -0.24529E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.14863E-04 0.16590E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.25092E-05 0.35510E-02 Friction velocity uk : 0.31780E-05 0.35505E-02 Dimensionless distance yplus : 0.21162E-04 0.23622E-01 Friction thermal sca. tstar : -0.24529E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.14863E-04 0.16590E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.55516E-08 4 0.10616E-05 0.30228E-11 0.20768E+01 c Velocity[X] 0.99579E-30 c Velocity[Y] 0.15114E-11 c Velocity[Z] 0.15114E-11 c Pressure 0.10059E-12 25 0.11047E-07 0.80461E-06 0.59561E+01 c k 0.13266E-05 2 0.57344E-06 0.32615E-06 0.46184E+01 c omega 0.13153E+02 1 0.19282E-07 0.23440E+02 0.25205E-01 c TempK 0.94287E+02 1 0.89102E-06 0.24288E+00 0.54892E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -2.2971e-13 1.9289e-13 -2.2399e-17 -5.5787e-18 v Velocity[Y] -0.0002354 0.00023611 -5.482e-10 -5.0765e-12 v Velocity[Z] -0.00023611 0.00023541 5.3699e-10 -9.873e-13 v ǁVelocityǁ 7.8555e-11 0.00028346 1.5738e-05 7.8503e-06 v Pressure -0.00022831 0.0093886 0.00038785 7.8442e-22 v k 4.5372e-08 0.0049196 0.0033499 0.0038905 v omega 44.948 1.0313e+05 2688.7 527.08 v TempK 288 340.95 291.49 289.25 v Density 1.205 1.205 1.205 1.205 v TurbVisc 5.3788e-13 0.00012369 8.1392e-05 9.9282e-05 v CourantNb 5.5569e-10 0.00043417 2.4093e-05 1.1666e-05 v FourierNb 0.14894 0.62812 0.25283 0.21112 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.851 4.8511 0.0003113 -1.1976e-07 v volume_forces[Z] -4.851 4.8511 -0.00031122 1.584e-07 v ǁvolume_forcesǁ 2.7359e-09 4.8535 0.31698 0.11347 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 291.71 289.4 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.023622 7.9867e-05 4.5549e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14894 0.62812 0.25285 0.21113 INSTANT 0.134820000E+00 TIME STEP NUMBER 140 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.26140E-05 0.35453E-02 Friction velocity uk : 0.32534E-05 0.35448E-02 Dimensionless distance yplus : 0.21664E-04 0.23584E-01 Friction thermal sca. tstar : -0.25400E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.15215E-04 0.16564E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.26140E-05 0.35453E-02 Friction velocity uk : 0.32534E-05 0.35448E-02 Dimensionless distance yplus : 0.21664E-04 0.23584E-01 Friction thermal sca. tstar : -0.25400E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.15215E-04 0.16564E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.55442E-08 4 0.10562E-05 0.30627E-11 0.20936E+01 c Velocity[X] 0.99416E-30 c Velocity[Y] 0.15314E-11 c Velocity[Z] 0.15313E-11 c Pressure 0.10001E-12 25 0.10982E-07 0.79982E-06 0.59145E+01 c k 0.13211E-05 2 0.56482E-06 0.32092E-06 0.46010E+01 c omega 0.13153E+02 1 0.19123E-07 0.23120E+02 0.25032E-01 c TempK 0.94288E+02 1 0.88325E-06 0.24045E+00 0.54616E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -2.2901e-13 1.9235e-13 -2.2309e-17 -5.5569e-18 v Velocity[Y] -0.00023494 0.00023564 -5.5233e-10 -5.0466e-12 v Velocity[Z] -0.00023564 0.00023494 5.4084e-10 -9.7659e-13 v ǁVelocityǁ 8.1513e-11 0.00028285 1.5715e-05 7.8434e-06 v Pressure -0.00023 0.0094233 0.00038998 -2.2993e-20 v k 4.4725e-08 0.0048948 0.003334 0.0038736 v omega 44.789 1.0313e+05 2688.6 526.93 v TempK 288 340.96 291.49 289.26 v Density 1.205 1.205 1.205 1.205 v TurbVisc 5.3018e-13 0.0001235 8.1294e-05 9.9197e-05 v CourantNb 5.5983e-10 0.00043353 2.4054e-05 1.1652e-05 v FourierNb 0.14891 0.62812 0.25248 0.21089 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.8516 4.8517 0.00031206 -1.2164e-07 v volume_forces[Z] -4.8516 4.8517 -0.00031198 1.6065e-07 v ǁvolume_forcesǁ 2.8397e-09 4.8541 0.31775 0.11387 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 291.72 289.4 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.023584 7.9739e-05 4.5474e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14891 0.62812 0.2525 0.2109 INSTANT 0.135783000E+00 TIME STEP NUMBER 141 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.27164E-05 0.35396E-02 Friction velocity uk : 0.33281E-05 0.35391E-02 Dimensionless distance yplus : 0.22162E-04 0.23546E-01 Friction thermal sca. tstar : -0.26934E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.15565E-04 0.16537E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.27164E-05 0.35396E-02 Friction velocity uk : 0.33281E-05 0.35391E-02 Dimensionless distance yplus : 0.22162E-04 0.23546E-01 Friction thermal sca. tstar : -0.26934E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.15565E-04 0.16537E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.55366E-08 4 0.10508E-05 0.31039E-11 0.21108E+01 c Velocity[X] 0.99221E-30 c Velocity[Y] 0.15520E-11 c Velocity[Z] 0.15519E-11 c Pressure 0.99431E-13 25 0.10926E-07 0.79509E-06 0.58736E+01 c k 0.13157E-05 2 0.55640E-06 0.31580E-06 0.45837E+01 c omega 0.13153E+02 1 0.18966E-07 0.22806E+02 0.24861E-01 c TempK 0.94289E+02 1 0.87559E-06 0.23806E+00 0.54343E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -2.2831e-13 1.918e-13 -2.222e-17 -5.5353e-18 v Velocity[Y] -0.00023446 0.00023517 -5.5645e-10 -5.0172e-12 v Velocity[Z] -0.00023517 0.00023447 5.4465e-10 -9.6644e-13 v ǁVelocityǁ 8.4553e-11 0.00028224 1.5693e-05 7.8362e-06 v Pressure -0.00023169 0.009458 0.00039211 -3.2321e-20 v k 4.4091e-08 0.0048702 0.0033181 0.0038569 v omega 44.631 1.0313e+05 2688.5 526.79 v TempK 288 340.97 291.5 289.26 v Density 1.205 1.205 1.205 1.205 v TurbVisc 5.2262e-13 0.00012331 8.1197e-05 9.9113e-05 v CourantNb 5.6397e-10 0.00043286 2.4014e-05 1.1637e-05 v FourierNb 0.14888 0.62812 0.25214 0.21066 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.8522 4.8523 0.00031282 -1.235e-07 v volume_forces[Z] -4.8522 4.8523 -0.00031273 1.6288e-07 v ǁvolume_forcesǁ 2.9467e-09 4.8547 0.31851 0.11428 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 291.73 289.41 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.023546 7.9612e-05 4.5399e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14888 0.62812 0.25216 0.21068 INSTANT 0.136746000E+00 TIME STEP NUMBER 142 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.28165E-05 0.35339E-02 Friction velocity uk : 0.34023E-05 0.35335E-02 Dimensionless distance yplus : 0.22656E-04 0.23508E-01 Friction thermal sca. tstar : -0.28800E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.15912E-04 0.16511E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.28165E-05 0.35339E-02 Friction velocity uk : 0.34023E-05 0.35335E-02 Dimensionless distance yplus : 0.22656E-04 0.23508E-01 Friction thermal sca. tstar : -0.28800E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.15912E-04 0.16511E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.55288E-08 4 0.10454E-05 0.31462E-11 0.21284E+01 c Velocity[X] 0.99000E-30 c Velocity[Y] 0.15731E-11 c Velocity[Z] 0.15731E-11 c Pressure 0.98903E-13 24 0.10910E-07 0.79074E-06 0.58332E+01 c k 0.13102E-05 2 0.54816E-06 0.31078E-06 0.45666E+01 c omega 0.13153E+02 1 0.18810E-07 0.22496E+02 0.24692E-01 c TempK 0.94290E+02 1 0.86804E-06 0.23571E+00 0.54074E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -2.2761e-13 1.9126e-13 -2.2132e-17 -5.5139e-18 v Velocity[Y] -0.00023399 0.00023469 -5.6079e-10 -5.2163e-12 v Velocity[Z] -0.00023469 0.00023399 5.4838e-10 -1.0267e-12 v ǁVelocityǁ 8.7254e-11 0.00028161 1.5669e-05 7.8287e-06 v Pressure -0.00023338 0.0094925 0.00039424 1.9463e-20 v k 4.3468e-08 0.0048457 0.0033024 0.0038403 v omega 44.474 1.0313e+05 2688.4 526.65 v TempK 288 340.97 291.51 289.27 v Density 1.205 1.205 1.205 1.205 v TurbVisc 5.152e-13 0.00012312 8.11e-05 9.9029e-05 v CourantNb 5.6809e-10 0.00043219 2.3974e-05 1.1622e-05 v FourierNb 0.14885 0.62812 0.25179 0.21044 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.8528 4.8529 0.00031357 -1.2535e-07 v volume_forces[Z] -4.8528 4.8529 -0.00031348 1.6509e-07 v ǁvolume_forcesǁ 3.0566e-09 4.8553 0.31927 0.11468 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 291.74 289.41 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.023508 7.9484e-05 4.5325e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14885 0.62812 0.25182 0.21045 INSTANT 0.137709000E+00 TIME STEP NUMBER 143 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.29017E-05 0.35282E-02 Friction velocity uk : 0.34648E-05 0.35278E-02 Dimensionless distance yplus : 0.23072E-04 0.23471E-01 Friction thermal sca. tstar : -0.31137E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.16204E-04 0.16484E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.29017E-05 0.35282E-02 Friction velocity uk : 0.34648E-05 0.35278E-02 Dimensionless distance yplus : 0.23072E-04 0.23471E-01 Friction thermal sca. tstar : -0.31137E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.16204E-04 0.16484E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.55208E-08 4 0.10402E-05 0.31894E-11 0.21464E+01 c Velocity[X] 0.98743E-30 c Velocity[Y] 0.15947E-11 c Velocity[Z] 0.15947E-11 c Pressure 0.98360E-13 24 0.10873E-07 0.78627E-06 0.57933E+01 c k 0.13049E-05 2 0.54010E-06 0.30586E-06 0.45496E+01 c omega 0.13153E+02 1 0.18657E-07 0.22192E+02 0.24524E-01 c TempK 0.94291E+02 1 0.86060E-06 0.23340E+00 0.53807E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -2.2691e-13 1.9071e-13 -2.2045e-17 -5.4928e-18 v Velocity[Y] -0.00023351 0.00023421 -5.6487e-10 -5.1887e-12 v Velocity[Z] -0.00023421 0.00023352 5.5216e-10 -1.0161e-12 v ǁVelocityǁ 9.0707e-11 0.00028099 1.5646e-05 7.8209e-06 v Pressure -0.00023507 0.0095268 0.00039636 -1.1006e-20 v k 4.2858e-08 0.0048214 0.0032868 0.0038238 v omega 44.318 1.0313e+05 2688.3 526.51 v TempK 288 340.98 291.52 289.27 v Density 1.205 1.205 1.205 1.205 v TurbVisc 5.0793e-13 0.00012293 8.1003e-05 9.8946e-05 v CourantNb 5.7222e-10 0.0004315 2.3933e-05 1.1606e-05 v FourierNb 0.14882 0.62812 0.25145 0.21021 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.8534 4.8535 0.00031431 -1.2719e-07 v volume_forces[Z] -4.8534 4.8535 -0.00031423 1.673e-07 v ǁvolume_forcesǁ 3.1542e-09 4.8559 0.32003 0.11509 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 291.75 289.42 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.023471 7.9357e-05 4.525e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14882 0.62812 0.25148 0.21022 INSTANT 0.138672000E+00 TIME STEP NUMBER 144 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.30066E-05 0.35226E-02 Friction velocity uk : 0.35455E-05 0.35221E-02 Dimensionless distance yplus : 0.23609E-04 0.23433E-01 Friction thermal sca. tstar : -0.34178E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.16581E-04 0.16458E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.30066E-05 0.35226E-02 Friction velocity uk : 0.35455E-05 0.35221E-02 Dimensionless distance yplus : 0.23609E-04 0.23433E-01 Friction thermal sca. tstar : -0.34178E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.16581E-04 0.16458E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.55126E-08 4 0.10349E-05 0.32333E-11 0.21646E+01 c Velocity[X] 0.98460E-30 c Velocity[Y] 0.16167E-11 c Velocity[Z] 0.16166E-11 c Pressure 0.97791E-13 24 0.10841E-07 0.78160E-06 0.57539E+01 c k 0.12995E-05 2 0.53222E-06 0.30103E-06 0.45327E+01 c omega 0.13153E+02 1 0.18505E-07 0.21893E+02 0.24358E-01 c TempK 0.94291E+02 1 0.85327E-06 0.23112E+00 0.53544E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -2.2621e-13 1.9016e-13 -2.1959e-17 -5.4718e-18 v Velocity[Y] -0.00023303 0.00023372 -5.6893e-10 -5.1584e-12 v Velocity[Z] -0.00023373 0.00023303 5.5591e-10 -1.0069e-12 v ǁVelocityǁ 9.4115e-11 0.00028036 1.5622e-05 7.8128e-06 v Pressure -0.00023676 0.0095611 0.00039848 2.1106e-20 v k 4.2259e-08 0.0047973 0.0032714 0.0038075 v omega 44.164 1.0313e+05 2688.1 526.37 v TempK 288 340.99 291.53 289.28 v Density 1.205 1.205 1.205 1.205 v TurbVisc 5.0079e-13 0.00012274 8.0907e-05 9.8863e-05 v CourantNb 5.7637e-10 0.0004308 2.3891e-05 1.159e-05 v FourierNb 0.14879 0.62812 0.25112 0.20999 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.854 4.8541 0.00031506 -1.2902e-07 v volume_forces[Z] -4.854 4.8541 -0.00031497 1.6948e-07 v ǁvolume_forcesǁ 3.2791e-09 4.8564 0.32078 0.11549 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 291.76 289.42 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.023433 7.923e-05 4.5175e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14879 0.62812 0.25114 0.21 INSTANT 0.139635000E+00 TIME STEP NUMBER 145 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.31054E-05 0.35169E-02 Friction velocity uk : 0.36219E-05 0.35165E-02 Dimensionless distance yplus : 0.24118E-04 0.23395E-01 Friction thermal sca. tstar : -0.38362E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.16939E-04 0.16431E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.31054E-05 0.35169E-02 Friction velocity uk : 0.36219E-05 0.35165E-02 Dimensionless distance yplus : 0.24118E-04 0.23395E-01 Friction thermal sca. tstar : -0.38362E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.16939E-04 0.16431E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.55042E-08 4 0.10297E-05 0.32778E-11 0.21831E+01 c Velocity[X] 0.98148E-30 c Velocity[Y] 0.16389E-11 c Velocity[Z] 0.16389E-11 c Pressure 0.97248E-13 24 0.10818E-07 0.77713E-06 0.57151E+01 c k 0.12942E-05 2 0.52451E-06 0.29629E-06 0.45160E+01 c omega 0.13153E+02 1 0.18354E-07 0.21598E+02 0.24194E-01 c TempK 0.94292E+02 1 0.84603E-06 0.22889E+00 0.53283E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -2.2552e-13 1.8961e-13 -2.1873e-17 -5.4511e-18 v Velocity[Y] -0.00023254 0.00023323 -5.7297e-10 -5.1295e-12 v Velocity[Z] -0.00023324 0.00023255 5.5964e-10 -9.9761e-13 v ǁVelocityǁ 9.7538e-11 0.00027972 1.5597e-05 7.8044e-06 v Pressure -0.00023846 0.0095953 0.00040059 -3.5814e-20 v k 4.1671e-08 0.0047734 0.003256 0.0037913 v omega 44.01 1.0313e+05 2688 526.23 v TempK 288 340.99 291.54 289.28 v Density 1.205 1.205 1.205 1.205 v TurbVisc 4.9379e-13 0.00012255 8.0812e-05 9.878e-05 v CourantNb 5.8052e-10 0.00043009 2.3848e-05 1.1573e-05 v FourierNb 0.14876 0.62812 0.25078 0.20977 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.8546 4.8546 0.0003158 -1.3083e-07 v volume_forces[Z] -4.8546 4.8546 -0.00031571 1.7165e-07 v ǁvolume_forcesǁ 3.4022e-09 4.857 0.32153 0.11589 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 291.76 289.43 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.023395 7.9103e-05 4.5101e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14876 0.62812 0.25081 0.20978 INSTANT 0.140598000E+00 TIME STEP NUMBER 146 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.32005E-05 0.35113E-02 Friction velocity uk : 0.36962E-05 0.35108E-02 Dimensionless distance yplus : 0.24612E-04 0.23358E-01 Friction thermal sca. tstar : -0.44643E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.17286E-04 0.16405E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.32005E-05 0.35113E-02 Friction velocity uk : 0.36962E-05 0.35108E-02 Dimensionless distance yplus : 0.24612E-04 0.23358E-01 Friction thermal sca. tstar : -0.44643E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.17286E-04 0.16405E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.54956E-08 4 0.10245E-05 0.33228E-11 0.22017E+01 c Velocity[X] 0.97811E-30 c Velocity[Y] 0.16614E-11 c Velocity[Z] 0.16613E-11 c Pressure 0.96717E-13 24 0.10800E-07 0.77277E-06 0.56767E+01 c k 0.12890E-05 2 0.51697E-06 0.29165E-06 0.44994E+01 c omega 0.13153E+02 1 0.18206E-07 0.21309E+02 0.24031E-01 c TempK 0.94293E+02 1 0.83890E-06 0.22669E+00 0.53026E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -2.2482e-13 1.8906e-13 -2.1788e-17 -5.4305e-18 v Velocity[Y] -0.00023206 0.00023274 -5.77e-10 -5.101e-12 v Velocity[Z] -0.00023275 0.00023206 5.6335e-10 -9.8876e-13 v ǁVelocityǁ 1.01e-10 0.00027908 1.5572e-05 7.7957e-06 v Pressure -0.00024015 0.0096293 0.0004027 1.3066e-20 v k 4.1095e-08 0.0047497 0.0032409 0.0037752 v omega 43.858 1.0313e+05 2687.9 526.09 v TempK 288 341 291.54 289.28 v Density 1.205 1.205 1.205 1.205 v TurbVisc 4.8692e-13 0.00012236 8.0718e-05 9.8698e-05 v CourantNb 5.8467e-10 0.00042936 2.3805e-05 1.1556e-05 v FourierNb 0.14873 0.62812 0.25045 0.20955 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.8551 4.8552 0.00031653 -1.3264e-07 v volume_forces[Z] -4.8551 4.8552 -0.00031645 1.7381e-07 v ǁvolume_forcesǁ 3.526e-09 4.8576 0.32228 0.11629 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 291.77 289.43 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.023358 7.8976e-05 4.5027e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14873 0.62812 0.25048 0.20956 INSTANT 0.141561000E+00 TIME STEP NUMBER 147 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.32931E-05 0.35056E-02 Friction velocity uk : 0.37692E-05 0.35052E-02 Dimensionless distance yplus : 0.25098E-04 0.23320E-01 Friction thermal sca. tstar : -0.55651E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.17628E-04 0.16379E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.32931E-05 0.35056E-02 Friction velocity uk : 0.37692E-05 0.35052E-02 Dimensionless distance yplus : 0.25098E-04 0.23320E-01 Friction thermal sca. tstar : -0.55651E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.17628E-04 0.16379E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.54868E-08 4 0.10759E-05 0.33680E-11 0.22204E+01 c Velocity[X] 0.97451E-30 c Velocity[Y] 0.16840E-11 c Velocity[Z] 0.16840E-11 c Pressure 0.96199E-13 24 0.10789E-07 0.76851E-06 0.56389E+01 c k 0.12837E-05 2 0.50959E-06 0.28710E-06 0.44829E+01 c omega 0.13153E+02 1 0.18059E-07 0.21024E+02 0.23870E-01 c TempK 0.94294E+02 1 0.83187E-06 0.22452E+00 0.52771E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -2.2413e-13 1.885e-13 -2.1704e-17 -5.4102e-18 v Velocity[Y] -0.00023156 0.00023225 -5.8101e-10 -5.0725e-12 v Velocity[Z] -0.00023225 0.00023157 5.6704e-10 -9.7972e-13 v ǁVelocityǁ 1.0451e-10 0.00027843 1.5546e-05 7.7868e-06 v Pressure -0.00024184 0.0096632 0.0004048 -1.1399e-20 v k 4.0529e-08 0.0047261 0.0032258 0.0037592 v omega 43.706 1.0313e+05 2687.8 525.95 v TempK 288 341 291.55 289.29 v Density 1.205 1.205 1.205 1.205 v TurbVisc 4.8018e-13 0.00012217 8.0624e-05 9.8616e-05 v CourantNb 5.8882e-10 0.00042862 2.3761e-05 1.1539e-05 v FourierNb 0.1487 0.62812 0.25013 0.20933 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.8557 4.8558 0.00031727 -1.3443e-07 v volume_forces[Z] -4.8557 4.8558 -0.00031718 1.7595e-07 v ǁvolume_forcesǁ 3.6512e-09 4.8581 0.32302 0.11669 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 291.78 289.43 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.02332 7.8849e-05 4.4952e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.1487 0.62812 0.25015 0.20934 INSTANT 0.142524000E+00 TIME STEP NUMBER 148 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.33837E-05 0.35000E-02 Friction velocity uk : 0.38413E-05 0.34995E-02 Dimensionless distance yplus : 0.25579E-04 0.23283E-01 Friction thermal sca. tstar : -0.83657E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.17965E-04 0.16352E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.33837E-05 0.35000E-02 Friction velocity uk : 0.38413E-05 0.34995E-02 Dimensionless distance yplus : 0.25579E-04 0.23283E-01 Friction thermal sca. tstar : -0.83657E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.17965E-04 0.16352E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.54778E-08 4 0.10143E-05 0.34134E-11 0.22393E+01 c Velocity[X] 0.97064E-30 c Velocity[Y] 0.17067E-11 c Velocity[Z] 0.17067E-11 c Pressure 0.95638E-13 24 0.10779E-07 0.76392E-06 0.56015E+01 c k 0.12785E-05 2 0.50237E-06 0.28263E-06 0.44665E+01 c omega 0.13153E+02 1 0.17913E-07 0.20744E+02 0.23711E-01 c TempK 0.94294E+02 1 0.82494E-06 0.22239E+00 0.52519E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -2.2344e-13 1.8795e-13 -2.1621e-17 -5.3901e-18 v Velocity[Y] -0.00023107 0.00023175 -5.85e-10 -5.0444e-12 v Velocity[Z] -0.00023175 0.00023107 5.707e-10 -9.7137e-13 v ǁVelocityǁ 1.0808e-10 0.00027778 1.552e-05 7.7776e-06 v Pressure -0.00024354 0.009697 0.0004069 3.7027e-20 v k 3.9973e-08 0.0047027 0.0032109 0.0037434 v omega 43.556 1.0313e+05 2687.7 525.81 v TempK 288 341.01 291.56 289.29 v Density 1.205 1.205 1.205 1.205 v TurbVisc 4.7356e-13 0.00012198 8.053e-05 9.8534e-05 v CourantNb 5.9297e-10 0.00042788 2.3716e-05 1.1521e-05 v FourierNb 0.14867 0.62812 0.2498 0.20911 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.8562 4.8563 0.000318 -1.3621e-07 v volume_forces[Z] -4.8562 4.8563 -0.00031791 1.7808e-07 v ǁvolume_forcesǁ 3.7781e-09 4.8587 0.32376 0.11708 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 291.79 289.44 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.023283 7.8722e-05 4.4877e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14867 0.62812 0.24982 0.20912 INSTANT 0.143487000E+00 TIME STEP NUMBER 149 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.34727E-05 0.34943E-02 Friction velocity uk : 0.39127E-05 0.34939E-02 Dimensionless distance yplus : 0.26054E-04 0.23245E-01 Friction thermal sca. tstar : -0.32895E+05 0.00000E+00 Dim-less thermal sca. tplus : 0.18299E-04 0.16326E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.34727E-05 0.34943E-02 Friction velocity uk : 0.39127E-05 0.34939E-02 Dimensionless distance yplus : 0.26054E-04 0.23245E-01 Friction thermal sca. tstar : -0.32895E+05 0.00000E+00 Dim-less thermal sca. tplus : 0.18299E-04 0.16326E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.54686E-08 4 0.10091E-05 0.34588E-11 0.22581E+01 c Velocity[X] 0.96652E-30 c Velocity[Y] 0.17294E-11 c Velocity[Z] 0.17293E-11 c Pressure 0.95095E-13 24 0.10773E-07 0.75947E-06 0.55646E+01 c k 0.12734E-05 2 0.49530E-06 0.27825E-06 0.44503E+01 c omega 0.13153E+02 1 0.17769E-07 0.20468E+02 0.23553E-01 c TempK 0.94295E+02 1 0.81811E-06 0.22030E+00 0.52270E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -2.2275e-13 1.8739e-13 -2.1539e-17 -5.3701e-18 v Velocity[Y] -0.00023057 0.00023125 -5.8898e-10 -5.0164e-12 v Velocity[Z] -0.00023125 0.00023058 5.7434e-10 -9.6303e-13 v ǁVelocityǁ 1.1169e-10 0.00027712 1.5494e-05 7.7681e-06 v Pressure -0.00024523 0.0097308 0.000409 -2.7553e-20 v k 3.9428e-08 0.0046795 0.0031961 0.0037277 v omega 43.407 1.0313e+05 2687.6 525.68 v TempK 288 341.02 291.57 289.3 v Density 1.205 1.205 1.205 1.205 v TurbVisc 4.6707e-13 0.00012179 8.0437e-05 9.8453e-05 v CourantNb 5.9712e-10 0.00042712 2.3671e-05 1.1503e-05 v FourierNb 0.14864 0.62812 0.24948 0.20889 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.8568 4.8569 0.00031872 -1.3798e-07 v volume_forces[Z] -4.8568 4.8569 -0.00031863 1.8019e-07 v ǁvolume_forcesǁ 3.9069e-09 4.8592 0.32449 0.11748 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 291.8 289.44 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.023245 7.8594e-05 4.4803e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14864 0.62812 0.2495 0.20891 INSTANT 0.144450000E+00 TIME STEP NUMBER 150 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.35601E-05 0.34887E-02 Friction velocity uk : 0.39835E-05 0.34883E-02 Dimensionless distance yplus : 0.26526E-04 0.23208E-01 Friction thermal sca. tstar : -0.72348E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.18630E-04 0.16300E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.35601E-05 0.34887E-02 Friction velocity uk : 0.39835E-05 0.34883E-02 Dimensionless distance yplus : 0.26526E-04 0.23208E-01 Friction thermal sca. tstar : -0.72348E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.18630E-04 0.16300E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.54592E-08 4 0.10040E-05 0.35041E-11 0.22770E+01 c Velocity[X] 0.96219E-30 c Velocity[Y] 0.17521E-11 c Velocity[Z] 0.17520E-11 c Pressure 0.94625E-13 24 0.10773E-07 0.75560E-06 0.55282E+01 c k 0.12683E-05 2 0.48838E-06 0.27395E-06 0.44341E+01 c omega 0.13153E+02 1 0.17627E-07 0.20197E+02 0.23396E-01 c TempK 0.94296E+02 1 0.81136E-06 0.21823E+00 0.52024E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -2.2206e-13 1.8684e-13 -2.1458e-17 -5.3504e-18 v Velocity[Y] -0.00023007 0.00023074 -5.9293e-10 -4.9887e-12 v Velocity[Z] -0.00023075 0.00023008 5.7796e-10 -9.5479e-13 v ǁVelocityǁ 1.1537e-10 0.00027646 1.5467e-05 7.7584e-06 v Pressure -0.00024693 0.0097644 0.00041109 2.5481e-20 v k 3.8893e-08 0.0046564 0.0031814 0.0037121 v omega 43.258 1.0313e+05 2687.5 525.54 v TempK 288 341.02 291.58 289.3 v Density 1.205 1.205 1.205 1.205 v TurbVisc 4.607e-13 0.0001216 8.0345e-05 9.8373e-05 v CourantNb 6.0127e-10 0.00042635 2.3625e-05 1.1484e-05 v FourierNb 0.14861 0.62812 0.24916 0.20868 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.8573 4.8574 0.00031944 -1.3974e-07 v volume_forces[Z] -4.8573 4.8574 -0.00031936 1.8229e-07 v ǁvolume_forcesǁ 4.0377e-09 4.8598 0.32522 0.11787 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 291.8 289.45 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.023208 7.8472e-05 4.4731e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14861 0.62812 0.24918 0.20869 INSTANT 0.145413000E+00 TIME STEP NUMBER 151 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.36463E-05 0.34831E-02 Friction velocity uk : 0.40539E-05 0.34827E-02 Dimensionless distance yplus : 0.26994E-04 0.23171E-01 Friction thermal sca. tstar : -0.51715E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.18959E-04 0.16274E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.36463E-05 0.34831E-02 Friction velocity uk : 0.40539E-05 0.34827E-02 Dimensionless distance yplus : 0.26994E-04 0.23171E-01 Friction thermal sca. tstar : -0.51715E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.18959E-04 0.16274E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.54497E-08 4 0.99898E-06 0.35491E-11 0.22958E+01 c Velocity[X] 0.95765E-30 c Velocity[Y] 0.17746E-11 c Velocity[Z] 0.17745E-11 c Pressure 0.94069E-13 24 0.10772E-07 0.75105E-06 0.54922E+01 c k 0.12632E-05 2 0.48161E-06 0.26974E-06 0.44181E+01 c omega 0.13153E+02 1 0.17486E-07 0.19931E+02 0.23241E-01 c TempK 0.94297E+02 1 0.80471E-06 0.21620E+00 0.51780E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -2.2137e-13 1.8628e-13 -2.1377e-17 -5.3309e-18 v Velocity[Y] -0.00022957 0.00023023 -5.9687e-10 -4.9611e-12 v Velocity[Z] -0.00023024 0.00022957 5.8157e-10 -9.4708e-13 v ǁVelocityǁ 1.1909e-10 0.0002758 1.544e-05 7.7485e-06 v Pressure -0.00024863 0.0097979 0.00041318 -1.9611e-20 v k 3.8367e-08 0.0046335 0.0031668 0.0036966 v omega 43.111 1.0313e+05 2687.3 525.41 v TempK 288 341.03 291.58 289.31 v Density 1.205 1.205 1.205 1.205 v TurbVisc 4.5444e-13 0.00012141 8.0253e-05 9.8292e-05 v CourantNb 6.0543e-10 0.00042557 2.3579e-05 1.1465e-05 v FourierNb 0.14858 0.62812 0.24884 0.20847 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.8579 4.8579 0.00032016 -1.4149e-07 v volume_forces[Z] -4.8579 4.8579 -0.00032008 1.8438e-07 v ǁvolume_forcesǁ 4.1705e-09 4.8603 0.32595 0.11827 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 291.81 289.45 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.023171 7.835e-05 4.4659e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14858 0.62812 0.24886 0.20848 INSTANT 0.146376000E+00 TIME STEP NUMBER 152 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.37311E-05 0.34775E-02 Friction velocity uk : 0.41238E-05 0.34771E-02 Dimensionless distance yplus : 0.27460E-04 0.23133E-01 Friction thermal sca. tstar : -0.42340E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.19286E-04 0.16247E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.37311E-05 0.34775E-02 Friction velocity uk : 0.41238E-05 0.34771E-02 Dimensionless distance yplus : 0.27460E-04 0.23133E-01 Friction thermal sca. tstar : -0.42340E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.19286E-04 0.16247E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.54400E-08 4 0.10516E-05 0.35939E-11 0.23146E+01 c Velocity[X] 0.95290E-30 c Velocity[Y] 0.17970E-11 c Velocity[Z] 0.17969E-11 c Pressure 0.93556E-13 25 0.10782E-07 0.74684E-06 0.54567E+01 c k 0.12582E-05 2 0.47498E-06 0.26560E-06 0.44022E+01 c omega 0.13153E+02 1 0.17347E-07 0.19669E+02 0.23088E-01 c TempK 0.94298E+02 1 0.79815E-06 0.21420E+00 0.51540E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -2.2069e-13 1.8573e-13 -2.1297e-17 -5.3115e-18 v Velocity[Y] -0.00022907 0.00022972 -6.008e-10 -4.9423e-12 v Velocity[Z] -0.00022973 0.00022907 5.8512e-10 -9.6368e-13 v ǁVelocityǁ 1.2294e-10 0.00027513 1.5412e-05 7.7383e-06 v Pressure -0.00025032 0.0098313 0.00041526 9.217e-21 v k 3.7851e-08 0.0046108 0.0031524 0.0036812 v omega 42.965 1.0313e+05 2687.2 525.27 v TempK 288 341.03 291.59 289.31 v Density 1.205 1.205 1.205 1.205 v TurbVisc 4.483e-13 0.00012122 8.0162e-05 9.8212e-05 v CourantNb 6.0955e-10 0.00042478 2.3532e-05 1.1446e-05 v FourierNb 0.14855 0.62812 0.24853 0.20826 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.8584 4.8585 0.00032088 -1.4323e-07 v volume_forces[Z] -4.8584 4.8585 -0.00032079 1.8645e-07 v ǁvolume_forcesǁ 4.3052e-09 4.8608 0.32668 0.11866 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 291.82 289.46 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.023133 7.8227e-05 4.4587e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14855 0.62812 0.24855 0.20827 INSTANT 0.147339000E+00 TIME STEP NUMBER 153 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.38162E-05 0.34719E-02 Friction velocity uk : 0.41945E-05 0.34715E-02 Dimensionless distance yplus : 0.27931E-04 0.23096E-01 Friction thermal sca. tstar : -0.36692E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.19617E-04 0.16221E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.38162E-05 0.34719E-02 Friction velocity uk : 0.41945E-05 0.34715E-02 Dimensionless distance yplus : 0.27931E-04 0.23096E-01 Friction thermal sca. tstar : -0.36692E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.19617E-04 0.16221E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.54302E-08 4 0.98899E-06 0.36383E-11 0.23333E+01 c Velocity[X] 0.94794E-30 c Velocity[Y] 0.18192E-11 c Velocity[Z] 0.18191E-11 c Pressure 0.93020E-13 25 0.10787E-07 0.74246E-06 0.54216E+01 c k 0.12532E-05 2 0.46849E-06 0.26154E-06 0.43864E+01 c omega 0.13153E+02 1 0.17209E-07 0.19410E+02 0.22936E-01 c TempK 0.94298E+02 1 0.79168E-06 0.21223E+00 0.51301E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -2.2001e-13 1.8517e-13 -2.1218e-17 -5.2923e-18 v Velocity[Y] -0.00022856 0.00022921 -6.0471e-10 -4.9153e-12 v Velocity[Z] -0.00022922 0.00022856 5.8868e-10 -9.5629e-13 v ǁVelocityǁ 1.268e-10 0.00027446 1.5384e-05 7.7279e-06 v Pressure -0.00025202 0.0098645 0.00041734 7.8197e-21 v k 3.7344e-08 0.0045883 0.003138 0.003666 v omega 42.819 1.0313e+05 2687.1 525.14 v TempK 288 341.04 291.6 289.31 v Density 1.205 1.205 1.205 1.205 v TurbVisc 4.4226e-13 0.00012103 8.0072e-05 9.8133e-05 v CourantNb 6.1367e-10 0.00042398 2.3485e-05 1.1427e-05 v FourierNb 0.14852 0.62812 0.24822 0.20805 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.8589 4.859 0.00032159 -1.4495e-07 v volume_forces[Z] -4.8589 4.859 -0.0003215 1.8851e-07 v ǁvolume_forcesǁ 4.4441e-09 4.8613 0.3274 0.11905 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 291.83 289.46 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.023096 7.8104e-05 4.4515e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14852 0.62812 0.24824 0.20806 INSTANT 0.148302000E+00 TIME STEP NUMBER 154 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.38993E-05 0.34663E-02 Friction velocity uk : 0.42641E-05 0.34659E-02 Dimensionless distance yplus : 0.28394E-04 0.23059E-01 Friction thermal sca. tstar : -0.40965E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.19942E-04 0.16195E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.38993E-05 0.34663E-02 Friction velocity uk : 0.42641E-05 0.34659E-02 Dimensionless distance yplus : 0.28394E-04 0.23059E-01 Friction thermal sca. tstar : -0.40965E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.19942E-04 0.16195E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.54202E-08 4 0.98405E-06 0.36822E-11 0.23518E+01 c Velocity[X] 0.94280E-30 c Velocity[Y] 0.18411E-11 c Velocity[Z] 0.18411E-11 c Pressure 0.92512E-13 25 0.10793E-07 0.73830E-06 0.53869E+01 c k 0.12482E-05 2 0.46213E-06 0.25756E-06 0.43707E+01 c omega 0.13153E+02 1 0.17073E-07 0.19157E+02 0.22785E-01 c TempK 0.94299E+02 1 0.78530E-06 0.21029E+00 0.51066E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -2.1933e-13 1.8461e-13 -2.114e-17 -5.2734e-18 v Velocity[Y] -0.00022805 0.0002287 -6.0859e-10 -4.8877e-12 v Velocity[Z] -0.0002287 0.00022806 5.9222e-10 -9.4892e-13 v ǁVelocityǁ 1.3069e-10 0.00027379 1.5356e-05 7.7173e-06 v Pressure -0.00025372 0.0098977 0.00041941 -2.8803e-21 v k 3.6846e-08 0.0045659 0.0031238 0.0036509 v omega 42.675 1.0313e+05 2687 525.01 v TempK 288 341.05 291.61 289.32 v Density 1.205 1.205 1.205 1.205 v TurbVisc 4.3634e-13 0.00012084 7.9982e-05 9.8053e-05 v CourantNb 6.1782e-10 0.00042317 2.3437e-05 1.1407e-05 v FourierNb 0.14849 0.62812 0.24791 0.20784 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.8594 4.8595 0.0003223 -1.4667e-07 v volume_forces[Z] -4.8594 4.8595 -0.00032221 1.9056e-07 v ǁvolume_forcesǁ 4.5836e-09 4.8619 0.32812 0.11944 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 291.84 289.47 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.023059 7.7981e-05 4.4443e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14849 0.62812 0.24793 0.20785 INSTANT 0.149265000E+00 TIME STEP NUMBER 155 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.39812E-05 0.34608E-02 Friction velocity uk : 0.43330E-05 0.34604E-02 Dimensionless distance yplus : 0.28853E-04 0.23022E-01 Friction thermal sca. tstar : -0.49714E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.20265E-04 0.16169E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.39812E-05 0.34608E-02 Friction velocity uk : 0.43330E-05 0.34604E-02 Dimensionless distance yplus : 0.28853E-04 0.23022E-01 Friction thermal sca. tstar : -0.49714E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.20265E-04 0.16169E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.54100E-08 4 0.97911E-06 0.37255E-11 0.23702E+01 c Velocity[X] 0.93748E-30 c Velocity[Y] 0.18628E-11 c Velocity[Z] 0.18627E-11 c Pressure 0.92003E-13 25 0.10803E-07 0.73413E-06 0.53527E+01 c k 0.12433E-05 2 0.45591E-06 0.25365E-06 0.43552E+01 c omega 0.13153E+02 1 0.16938E-07 0.18907E+02 0.22636E-01 c TempK 0.94300E+02 1 0.77900E-06 0.20838E+00 0.50833E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -2.1865e-13 1.8406e-13 -2.1062e-17 -5.2546e-18 v Velocity[Y] -0.00022754 0.00022818 -6.1246e-10 -4.8607e-12 v Velocity[Z] -0.00022818 0.00022755 5.9574e-10 -9.415e-13 v ǁVelocityǁ 1.3464e-10 0.00027312 1.5328e-05 7.7064e-06 v Pressure -0.00025541 0.0099308 0.00042148 3.2603e-21 v k 3.6358e-08 0.0045437 0.0031097 0.0036358 v omega 42.532 1.0313e+05 2686.9 524.88 v TempK 288 341.05 291.62 289.32 v Density 1.205 1.205 1.205 1.205 v TurbVisc 4.3052e-13 0.00012066 7.9892e-05 9.7975e-05 v CourantNb 6.2196e-10 0.00042235 2.3389e-05 1.1387e-05 v FourierNb 0.14846 0.62812 0.2476 0.20763 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.86 4.86 0.00032301 -1.4837e-07 v volume_forces[Z] -4.86 4.86 -0.00032292 1.9259e-07 v ǁvolume_forcesǁ 4.7246e-09 4.8624 0.32883 0.11983 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 291.84 289.47 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.023022 7.7858e-05 4.4371e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14847 0.62812 0.24762 0.20764 INSTANT 0.150228000E+00 TIME STEP NUMBER 156 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.40620E-05 0.34552E-02 Friction velocity uk : 0.44015E-05 0.34548E-02 Dimensionless distance yplus : 0.29309E-04 0.22985E-01 Friction thermal sca. tstar : -0.68655E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.20585E-04 0.16143E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.40620E-05 0.34552E-02 Friction velocity uk : 0.44015E-05 0.34548E-02 Dimensionless distance yplus : 0.29309E-04 0.22985E-01 Friction thermal sca. tstar : -0.68655E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.20585E-04 0.16143E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.53998E-08 4 0.99797E-06 0.37681E-11 0.23885E+01 c Velocity[X] 0.93198E-30 c Velocity[Y] 0.18841E-11 c Velocity[Z] 0.18840E-11 c Pressure 0.91488E-13 25 0.10814E-07 0.72992E-06 0.53189E+01 c k 0.12384E-05 2 0.44981E-06 0.24982E-06 0.43397E+01 c omega 0.13153E+02 1 0.16805E-07 0.18661E+02 0.22489E-01 c TempK 0.94301E+02 1 0.77279E-06 0.20650E+00 0.50602E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -2.1797e-13 1.835e-13 -2.0985e-17 -5.236e-18 v Velocity[Y] -0.00022703 0.00022766 -6.1632e-10 -4.8387e-12 v Velocity[Z] -0.00022767 0.00022703 5.9924e-10 -9.3201e-13 v ǁVelocityǁ 1.3863e-10 0.00027244 1.5299e-05 7.6954e-06 v Pressure -0.00025711 0.0099638 0.00042354 9.9524e-21 v k 3.5877e-08 0.0045216 0.0030958 0.0036209 v omega 42.389 1.0313e+05 2686.8 524.75 v TempK 288 341.06 291.62 289.33 v Density 1.205 1.205 1.205 1.205 v TurbVisc 4.2481e-13 0.00012047 7.9803e-05 9.7896e-05 v CourantNb 6.2612e-10 0.00042153 2.334e-05 1.1366e-05 v FourierNb 0.14843 0.62812 0.24729 0.20742 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.8605 4.8606 0.00032371 -1.5007e-07 v volume_forces[Z] -4.8605 4.8606 -0.00032362 1.9461e-07 v ǁvolume_forcesǁ 4.8672e-09 4.8629 0.32954 0.12022 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 291.85 289.47 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.022985 7.7735e-05 4.4299e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14844 0.62812 0.24732 0.20744 INSTANT 0.151191000E+00 TIME STEP NUMBER 157 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.41419E-05 0.34497E-02 Friction velocity uk : 0.44697E-05 0.34493E-02 Dimensionless distance yplus : 0.29763E-04 0.22948E-01 Friction thermal sca. tstar : -0.23219E+05 0.00000E+00 Dim-less thermal sca. tplus : 0.20904E-04 0.16117E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.41419E-05 0.34497E-02 Friction velocity uk : 0.44697E-05 0.34493E-02 Dimensionless distance yplus : 0.29763E-04 0.22948E-01 Friction thermal sca. tstar : -0.23219E+05 0.00000E+00 Dim-less thermal sca. tplus : 0.20904E-04 0.16117E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.53893E-08 4 0.96938E-06 0.38100E-11 0.24066E+01 c Velocity[X] 0.92632E-30 c Velocity[Y] 0.19051E-11 c Velocity[Z] 0.19050E-11 c Pressure 0.91116E-13 25 0.10824E-07 0.72685E-06 0.52855E+01 c k 0.12336E-05 2 0.44384E-06 0.24605E-06 0.43244E+01 c omega 0.13153E+02 1 0.16673E-07 0.18419E+02 0.22342E-01 c TempK 0.94302E+02 1 0.76666E-06 0.20465E+00 0.50374E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -2.173e-13 1.8294e-13 -2.0909e-17 -5.2175e-18 v Velocity[Y] -0.00022652 0.00022714 -6.2015e-10 -4.8124e-12 v Velocity[Z] -0.00022715 0.00022652 6.0272e-10 -9.2477e-13 v ǁVelocityǁ 1.4267e-10 0.00027176 1.527e-05 7.6842e-06 v Pressure -0.00025881 0.0099966 0.0004256 3.5544e-20 v k 3.5406e-08 0.0044998 0.0030819 0.0036061 v omega 42.248 1.0313e+05 2686.7 524.62 v TempK 288 341.06 291.63 289.33 v Density 1.205 1.205 1.205 1.205 v TurbVisc 4.192e-13 0.00012028 7.9715e-05 9.7818e-05 v CourantNb 6.3028e-10 0.00042069 2.3291e-05 1.1346e-05 v FourierNb 0.14841 0.62812 0.24699 0.20722 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.861 4.8611 0.00032441 -1.5176e-07 v volume_forces[Z] -4.861 4.8611 -0.00032432 1.9662e-07 v ǁvolume_forcesǁ 5.0116e-09 4.8634 0.33025 0.1206 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 291.86 289.48 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.022948 7.7611e-05 4.4226e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14841 0.62812 0.24702 0.20723 INSTANT 0.152154000E+00 TIME STEP NUMBER 158 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.42209E-05 0.34441E-02 Friction velocity uk : 0.45374E-05 0.34437E-02 Dimensionless distance yplus : 0.30214E-04 0.22911E-01 Friction thermal sca. tstar : -0.81383E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.21220E-04 0.16092E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.42209E-05 0.34441E-02 Friction velocity uk : 0.45374E-05 0.34437E-02 Dimensionless distance yplus : 0.30214E-04 0.22911E-01 Friction thermal sca. tstar : -0.81383E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.21220E-04 0.16092E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.53788E-08 4 0.96453E-06 0.38511E-11 0.24244E+01 c Velocity[X] 0.92051E-30 c Velocity[Y] 0.19256E-11 c Velocity[Z] 0.19255E-11 c Pressure 0.90488E-13 25 0.10828E-07 0.72173E-06 0.52525E+01 c k 0.12288E-05 2 0.43799E-06 0.24236E-06 0.43092E+01 c omega 0.13153E+02 1 0.16542E-07 0.18181E+02 0.22198E-01 c TempK 0.94302E+02 1 0.76061E-06 0.20283E+00 0.50148E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -2.1662e-13 1.8238e-13 -2.0834e-17 -5.1993e-18 v Velocity[Y] -0.000226 0.00022662 -6.2394e-10 -4.7626e-12 v Velocity[Z] -0.00022662 0.00022601 6.0624e-10 -8.5761e-13 v ǁVelocityǁ 1.4672e-10 0.00027107 1.524e-05 7.6728e-06 v Pressure -0.00026051 0.010029 0.00042766 5.6e-20 v k 3.4942e-08 0.0044781 0.0030681 0.0035915 v omega 42.107 1.0313e+05 2686.6 524.49 v TempK 288 341.07 291.64 289.34 v Density 1.205 1.205 1.205 1.205 v TurbVisc 4.1369e-13 0.00012009 7.9627e-05 9.774e-05 v CourantNb 6.3445e-10 0.00041985 2.3242e-05 1.1325e-05 v FourierNb 0.14838 0.62812 0.24669 0.20702 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.8615 4.8616 0.00032511 -1.5343e-07 v volume_forces[Z] -4.8615 4.8616 -0.00032502 1.9861e-07 v ǁvolume_forcesǁ 5.1576e-09 4.8639 0.33096 0.12099 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 291.87 289.48 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.022911 7.7493e-05 4.4157e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14838 0.62812 0.24672 0.20703 INSTANT 0.153117000E+00 TIME STEP NUMBER 159 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.42982E-05 0.34386E-02 Friction velocity uk : 0.46040E-05 0.34382E-02 Dimensionless distance yplus : 0.30658E-04 0.22875E-01 Friction thermal sca. tstar : -0.53716E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.21532E-04 0.16066E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.42982E-05 0.34386E-02 Friction velocity uk : 0.46040E-05 0.34382E-02 Dimensionless distance yplus : 0.30658E-04 0.22875E-01 Friction thermal sca. tstar : -0.53716E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.21532E-04 0.16066E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.53681E-08 4 0.96690E-06 0.38914E-11 0.24420E+01 c Velocity[X] 0.91455E-30 c Velocity[Y] 0.19457E-11 c Velocity[Z] 0.19456E-11 c Pressure 0.89965E-13 25 0.10837E-07 0.71747E-06 0.52198E+01 c k 0.12240E-05 2 0.43225E-06 0.23873E-06 0.42940E+01 c omega 0.13153E+02 1 0.16413E-07 0.17946E+02 0.22054E-01 c TempK 0.94303E+02 1 0.75464E-06 0.20103E+00 0.49924E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -2.1595e-13 1.8183e-13 -2.0759e-17 -5.1812e-18 v Velocity[Y] -0.00022549 0.0002261 -6.2774e-10 -4.7361e-12 v Velocity[Z] -0.0002261 0.00022549 6.0967e-10 -8.5126e-13 v ǁVelocityǁ 1.5087e-10 0.00027039 1.5211e-05 7.6612e-06 v Pressure -0.00026221 0.010062 0.00042971 -4.9468e-20 v k 3.4487e-08 0.0044566 0.0030545 0.0035769 v omega 41.968 1.0313e+05 2686.5 524.37 v TempK 288 341.07 291.65 289.34 v Density 1.205 1.205 1.205 1.205 v TurbVisc 4.0828e-13 0.00011991 7.9539e-05 9.7663e-05 v CourantNb 6.3861e-10 0.000419 2.3192e-05 1.1304e-05 v FourierNb 0.14835 0.62812 0.2464 0.20681 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.862 4.8621 0.0003258 -1.5509e-07 v volume_forces[Z] -4.862 4.8621 -0.00032571 2.0059e-07 v ǁvolume_forcesǁ 5.3038e-09 4.8644 0.33166 0.12137 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 291.88 289.49 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.022875 7.7374e-05 4.4088e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14835 0.62812 0.24642 0.20683 INSTANT 0.154080000E+00 TIME STEP NUMBER 160 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.43760E-05 0.34331E-02 Friction velocity uk : 0.46715E-05 0.34327E-02 Dimensionless distance yplus : 0.31107E-04 0.22838E-01 Friction thermal sca. tstar : -0.42903E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.21848E-04 0.16040E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.43760E-05 0.34331E-02 Friction velocity uk : 0.46715E-05 0.34327E-02 Dimensionless distance yplus : 0.31107E-04 0.22838E-01 Friction thermal sca. tstar : -0.42903E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.21848E-04 0.16040E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.53573E-08 4 0.95492E-06 0.39307E-11 0.24594E+01 c Velocity[X] 0.90845E-30 c Velocity[Y] 0.19654E-11 c Velocity[Z] 0.19653E-11 c Pressure 0.89489E-13 25 0.10847E-07 0.71357E-06 0.51876E+01 c k 0.12192E-05 2 0.42664E-06 0.23517E-06 0.42790E+01 c omega 0.13153E+02 1 0.16285E-07 0.17716E+02 0.21912E-01 c TempK 0.94304E+02 1 0.74874E-06 0.19926E+00 0.49703E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -2.1529e-13 1.8127e-13 -2.0685e-17 -5.1633e-18 v Velocity[Y] -0.00022497 0.00022557 -6.3152e-10 -4.7105e-12 v Velocity[Z] -0.00022558 0.00022498 6.1309e-10 -8.4494e-13 v ǁVelocityǁ 1.5506e-10 0.0002697 1.5181e-05 7.6494e-06 v Pressure -0.00026391 0.010095 0.00043176 2.7259e-20 v k 3.404e-08 0.0044352 0.003041 0.0035624 v omega 41.829 1.0313e+05 2686.4 524.24 v TempK 288 341.08 291.65 289.34 v Density 1.205 1.205 1.205 1.205 v TurbVisc 4.0296e-13 0.00011972 7.9452e-05 9.7586e-05 v CourantNb 6.4278e-10 0.00041815 2.3141e-05 1.1282e-05 v FourierNb 0.14832 0.62812 0.2461 0.20661 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.8625 4.8626 0.00032649 -1.5675e-07 v volume_forces[Z] -4.8625 4.8626 -0.0003264 2.0256e-07 v ǁvolume_forcesǁ 5.4541e-09 4.8649 0.33236 0.12176 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 291.88 289.49 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.022838 7.7256e-05 4.4018e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14832 0.62812 0.24612 0.20662 INSTANT 0.155043000E+00 TIME STEP NUMBER 161 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.44527E-05 0.34276E-02 Friction velocity uk : 0.47385E-05 0.34272E-02 Dimensionless distance yplus : 0.31553E-04 0.22802E-01 Friction thermal sca. tstar : -0.36734E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.22161E-04 0.16014E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.44527E-05 0.34276E-02 Friction velocity uk : 0.47385E-05 0.34272E-02 Dimensionless distance yplus : 0.31553E-04 0.22802E-01 Friction thermal sca. tstar : -0.36734E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.22161E-04 0.16014E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.53464E-08 4 0.95016E-06 0.39690E-11 0.24766E+01 c Velocity[X] 0.90221E-30 c Velocity[Y] 0.19845E-11 c Velocity[Z] 0.19845E-11 c Pressure 0.89049E-13 25 0.10858E-07 0.70997E-06 0.51558E+01 c k 0.12145E-05 2 0.42113E-06 0.23168E-06 0.42641E+01 c omega 0.13153E+02 1 0.16159E-07 0.17489E+02 0.21771E-01 c TempK 0.94305E+02 1 0.74293E-06 0.19751E+00 0.49484E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -2.1462e-13 1.8072e-13 -2.0612e-17 -5.1456e-18 v Velocity[Y] -0.00022445 0.00022505 -6.3528e-10 -4.6848e-12 v Velocity[Z] -0.00022505 0.00022446 6.1648e-10 -8.3921e-13 v ǁVelocityǁ 1.5929e-10 0.00026901 1.5151e-05 7.6375e-06 v Pressure -0.00026561 0.010127 0.0004338 7.9178e-21 v k 3.3601e-08 0.004414 0.0030276 0.003548 v omega 41.691 1.0313e+05 2686.3 524.11 v TempK 288 341.08 291.66 289.35 v Density 1.205 1.205 1.205 1.205 v TurbVisc 3.9773e-13 0.00011954 7.9366e-05 9.7509e-05 v CourantNb 6.4587e-10 0.00041728 2.3091e-05 1.126e-05 v FourierNb 0.14829 0.62812 0.24581 0.20641 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.863 4.8631 0.00032718 -1.5839e-07 v volume_forces[Z] -4.863 4.8631 -0.00032709 2.0452e-07 v ǁvolume_forcesǁ 5.6055e-09 4.8654 0.33305 0.12214 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 291.89 289.49 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.022802 7.7137e-05 4.3949e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14829 0.62812 0.24583 0.20643 INSTANT 0.156006000E+00 TIME STEP NUMBER 162 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.45286E-05 0.34221E-02 Friction velocity uk : 0.48050E-05 0.34217E-02 Dimensionless distance yplus : 0.31996E-04 0.22765E-01 Friction thermal sca. tstar : -0.32617E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.22472E-04 0.15989E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.45286E-05 0.34221E-02 Friction velocity uk : 0.48050E-05 0.34217E-02 Dimensionless distance yplus : 0.31996E-04 0.22765E-01 Friction thermal sca. tstar : -0.32617E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.22472E-04 0.15989E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.53354E-08 4 0.94541E-06 0.40063E-11 0.24935E+01 c Velocity[X] 0.89585E-30 c Velocity[Y] 0.20032E-11 c Velocity[Z] 0.20031E-11 c Pressure 0.88485E-13 25 0.10866E-07 0.70538E-06 0.51243E+01 c k 0.12098E-05 2 0.41574E-06 0.22825E-06 0.42493E+01 c omega 0.13153E+02 1 0.16034E-07 0.17265E+02 0.21632E-01 c TempK 0.94306E+02 1 0.73718E-06 0.19579E+00 0.49268E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -2.1396e-13 1.8016e-13 -2.0539e-17 -5.128e-18 v Velocity[Y] -0.00022394 0.00022452 -6.3902e-10 -4.6596e-12 v Velocity[Z] -0.00022452 0.00022394 6.1985e-10 -8.3306e-13 v ǁVelocityǁ 1.6356e-10 0.00026832 1.512e-05 7.6254e-06 v Pressure -0.00026731 0.01016 0.00043584 -8.8248e-21 v k 3.3169e-08 0.0043929 0.0030142 0.0035338 v omega 41.554 1.0313e+05 2686.2 523.99 v TempK 288 341.09 291.67 289.35 v Density 1.205 1.205 1.205 1.205 v TurbVisc 3.926e-13 0.00011935 7.928e-05 9.7433e-05 v CourantNb 6.4736e-10 0.00041641 2.304e-05 1.1239e-05 v FourierNb 0.14826 0.62812 0.24552 0.20622 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.8635 4.8636 0.00032786 -1.6003e-07 v volume_forces[Z] -4.8635 4.8636 -0.00032777 2.0646e-07 v ǁvolume_forcesǁ 5.7583e-09 4.8658 0.33374 0.12252 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 291.9 289.5 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.022765 7.7019e-05 4.388e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14826 0.62812 0.24554 0.20623 INSTANT 0.156969000E+00 TIME STEP NUMBER 163 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.46037E-05 0.34167E-02 Friction velocity uk : 0.48711E-05 0.34163E-02 Dimensionless distance yplus : 0.32436E-04 0.22729E-01 Friction thermal sca. tstar : -0.29619E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.22781E-04 0.15963E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.46037E-05 0.34167E-02 Friction velocity uk : 0.48711E-05 0.34163E-02 Dimensionless distance yplus : 0.32436E-04 0.22729E-01 Friction thermal sca. tstar : -0.29619E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.22781E-04 0.15963E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.53242E-08 4 0.94668E-06 0.40425E-11 0.25101E+01 c Velocity[X] 0.88996E-30 c Velocity[Y] 0.20213E-11 c Velocity[Z] 0.20212E-11 c Pressure 0.88057E-13 26 0.58354E-08 0.70187E-06 0.50932E+01 c k 0.12052E-05 2 0.41045E-06 0.22488E-06 0.42346E+01 c omega 0.13153E+02 1 0.15910E-07 0.17045E+02 0.21493E-01 c TempK 0.94306E+02 1 0.73152E-06 0.19410E+00 0.49053E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -2.133e-13 1.7961e-13 -2.0467e-17 -5.1106e-18 v Velocity[Y] -0.00022342 0.00022399 -6.4279e-10 -4.6806e-12 v Velocity[Z] -0.00022399 0.00022342 6.2326e-10 -7.7906e-13 v ǁVelocityǁ 1.6769e-10 0.00026763 1.5089e-05 7.6132e-06 v Pressure -0.00026901 0.010192 0.00043787 -2.5935e-20 v k 3.2744e-08 0.004372 0.003001 0.0035196 v omega 41.418 1.0313e+05 2686.1 523.86 v TempK 288 341.09 291.68 289.36 v Density 1.205 1.205 1.205 1.205 v TurbVisc 3.8755e-13 0.00011916 7.9194e-05 9.7356e-05 v CourantNb 6.4908e-10 0.00041554 2.2988e-05 1.1217e-05 v FourierNb 0.14823 0.62812 0.24523 0.20602 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.864 4.864 0.00032855 -1.6165e-07 v volume_forces[Z] -4.864 4.864 -0.00032845 2.084e-07 v ǁvolume_forcesǁ 5.9126e-09 4.8663 0.33443 0.1229 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 291.91 289.5 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.022729 7.6901e-05 4.381e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14824 0.62812 0.24525 0.20603 INSTANT 0.157932000E+00 TIME STEP NUMBER 164 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.46753E-05 0.34112E-02 Friction velocity uk : 0.49342E-05 0.34108E-02 Dimensionless distance yplus : 0.32857E-04 0.22693E-01 Friction thermal sca. tstar : -0.27320E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.23076E-04 0.15938E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.46753E-05 0.34112E-02 Friction velocity uk : 0.49342E-05 0.34108E-02 Dimensionless distance yplus : 0.32857E-04 0.22693E-01 Friction thermal sca. tstar : -0.27320E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.23076E-04 0.15938E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.53130E-08 4 0.93495E-06 0.40776E-11 0.25264E+01 c Velocity[X] 0.88280E-30 c Velocity[Y] 0.20389E-11 c Velocity[Z] 0.20388E-11 c Pressure 0.87398E-13 26 0.57979E-08 0.69652E-06 0.50625E+01 c k 0.12006E-05 2 0.40527E-06 0.22157E-06 0.42200E+01 c omega 0.13153E+02 1 0.15788E-07 0.16829E+02 0.21356E-01 c TempK 0.94307E+02 1 0.72592E-06 0.19243E+00 0.48841E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -2.1264e-13 1.7905e-13 -2.0396e-17 -5.0934e-18 v Velocity[Y] -0.0002229 0.00022346 -6.465e-10 -4.6548e-12 v Velocity[Z] -0.00022347 0.0002229 6.2659e-10 -7.7329e-13 v ǁVelocityǁ 1.7207e-10 0.00026693 1.5059e-05 7.6008e-06 v Pressure -0.00027071 0.010224 0.00043991 -4.3879e-21 v k 3.2327e-08 0.0043512 0.0029879 0.0035056 v omega 41.283 1.0313e+05 2686 523.74 v TempK 288 341.1 291.69 289.36 v Density 1.205 1.205 1.205 1.205 v TurbVisc 3.8259e-13 0.00011898 7.9109e-05 9.7281e-05 v CourantNb 6.5057e-10 0.00041466 2.2937e-05 1.1194e-05 v FourierNb 0.14821 0.62811 0.24494 0.20582 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.8644 4.8645 0.00032922 -1.6327e-07 v volume_forces[Z] -4.8644 4.8645 -0.00032913 2.1032e-07 v ǁvolume_forcesǁ 6.062e-09 4.8668 0.33512 0.12328 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 291.91 289.51 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.022693 7.6784e-05 4.3741e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14821 0.62811 0.24497 0.20583 INSTANT 0.158895000E+00 TIME STEP NUMBER 165 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.47497E-05 0.34058E-02 Friction velocity uk : 0.50003E-05 0.34054E-02 Dimensionless distance yplus : 0.33297E-04 0.22656E-01 Friction thermal sca. tstar : -0.25472E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.23385E-04 0.15912E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.47497E-05 0.34058E-02 Friction velocity uk : 0.50003E-05 0.34054E-02 Dimensionless distance yplus : 0.33297E-04 0.22656E-01 Friction thermal sca. tstar : -0.25472E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.23385E-04 0.15912E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.53016E-08 4 0.93063E-06 0.41116E-11 0.25424E+01 c Velocity[X] 0.87604E-30 c Velocity[Y] 0.20558E-11 c Velocity[Z] 0.20558E-11 c Pressure 0.86920E-13 26 0.57661E-08 0.69262E-06 0.50321E+01 c k 0.11960E-05 2 0.40019E-06 0.21832E-06 0.42055E+01 c omega 0.13153E+02 1 0.15667E-07 0.16616E+02 0.21221E-01 c TempK 0.94308E+02 1 0.72040E-06 0.19078E+00 0.48631E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -2.1198e-13 1.785e-13 -2.0326e-17 -5.0763e-18 v Velocity[Y] -0.00022238 0.00022293 -6.5019e-10 -4.6297e-12 v Velocity[Z] -0.00022294 0.00022238 6.299e-10 -7.6839e-13 v ǁVelocityǁ 1.7647e-10 0.00026624 1.5027e-05 7.5883e-06 v Pressure -0.00027241 0.010256 0.00044193 -3.4466e-20 v k 3.1917e-08 0.0043306 0.0029749 0.0034916 v omega 41.149 1.0313e+05 2685.9 523.62 v TempK 288 341.1 291.69 289.37 v Density 1.205 1.205 1.205 1.205 v TurbVisc 3.7772e-13 0.00011879 7.9025e-05 9.7205e-05 v CourantNb 6.5202e-10 0.00041377 2.2885e-05 1.1172e-05 v FourierNb 0.14818 0.62811 0.24466 0.20563 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.8649 4.865 0.0003299 -1.6488e-07 v volume_forces[Z] -4.8649 4.865 -0.00032981 2.1223e-07 v ǁvolume_forcesǁ 6.2203e-09 4.8673 0.3358 0.12365 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 291.92 289.51 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.022656 7.6666e-05 4.3673e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14818 0.62811 0.24468 0.20564 INSTANT 0.159858000E+00 TIME STEP NUMBER 166 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.48231E-05 0.34004E-02 Friction velocity uk : 0.50658E-05 0.34000E-02 Dimensionless distance yplus : 0.33733E-04 0.22620E-01 Friction thermal sca. tstar : -0.23946E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.23692E-04 0.15887E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.48231E-05 0.34004E-02 Friction velocity uk : 0.50658E-05 0.34000E-02 Dimensionless distance yplus : 0.33733E-04 0.22620E-01 Friction thermal sca. tstar : -0.23946E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.23692E-04 0.15887E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.52902E-08 4 0.92707E-06 0.41444E-11 0.25582E+01 c Velocity[X] 0.86924E-30 c Velocity[Y] 0.20722E-11 c Velocity[Z] 0.20721E-11 c Pressure 0.86431E-13 26 0.57360E-08 0.68863E-06 0.50020E+01 c k 0.11914E-05 2 0.39521E-06 0.21513E-06 0.41911E+01 c omega 0.13153E+02 1 0.15547E-07 0.16406E+02 0.21086E-01 c TempK 0.94309E+02 1 0.71494E-06 0.18916E+00 0.48423E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -2.1133e-13 1.7795e-13 -2.0256e-17 -5.0595e-18 v Velocity[Y] -0.00022186 0.0002224 -6.5386e-10 -4.6048e-12 v Velocity[Z] -0.00022241 0.00022186 6.3319e-10 -7.635e-13 v ǁVelocityǁ 1.8091e-10 0.00026554 1.4996e-05 7.5756e-06 v Pressure -0.00027411 0.010288 0.00044396 -4.128e-20 v k 3.1514e-08 0.0043101 0.002962 0.0034778 v omega 41.016 1.0313e+05 2685.8 523.5 v TempK 288 341.11 291.7 289.37 v Density 1.205 1.205 1.205 1.205 v TurbVisc 3.7293e-13 0.00011861 7.8941e-05 9.713e-05 v CourantNb 6.5345e-10 0.00041288 2.2833e-05 1.1149e-05 v FourierNb 0.14815 0.62811 0.24438 0.20543 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.8654 4.8655 0.00033057 -1.6647e-07 v volume_forces[Z] -4.8654 4.8655 -0.00033048 2.1413e-07 v ǁvolume_forcesǁ 6.3795e-09 4.8677 0.33648 0.12403 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 291.93 289.52 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.02262 7.6549e-05 4.3604e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14815 0.62811 0.2444 0.20545 INSTANT 0.160821000E+00 TIME STEP NUMBER 167 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.48958E-05 0.33950E-02 Friction velocity uk : 0.51310E-05 0.33946E-02 Dimensionless distance yplus : 0.34167E-04 0.22584E-01 Friction thermal sca. tstar : -0.22658E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.23997E-04 0.15862E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.48958E-05 0.33950E-02 Friction velocity uk : 0.51310E-05 0.33946E-02 Dimensionless distance yplus : 0.34167E-04 0.22584E-01 Friction thermal sca. tstar : -0.22658E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.23997E-04 0.15862E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.52787E-08 4 0.92149E-06 0.41759E-11 0.25736E+01 c Velocity[X] 0.86236E-30 c Velocity[Y] 0.20880E-11 c Velocity[Z] 0.20879E-11 c Pressure 0.85951E-13 26 0.57061E-08 0.68472E-06 0.49723E+01 c k 0.11869E-05 2 0.39033E-06 0.21200E-06 0.41768E+01 c omega 0.13153E+02 1 0.15428E-07 0.16199E+02 0.20953E-01 c TempK 0.94309E+02 1 0.70956E-06 0.18756E+00 0.48217E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -2.1068e-13 1.774e-13 -2.0187e-17 -5.0428e-18 v Velocity[Y] -0.00022134 0.00022187 -6.5751e-10 -4.5802e-12 v Velocity[Z] -0.00022188 0.00022134 6.3646e-10 -7.5886e-13 v ǁVelocityǁ 1.8539e-10 0.00026484 1.4965e-05 7.5628e-06 v Pressure -0.00027582 0.01032 0.00044597 1.1864e-20 v k 3.1118e-08 0.0042898 0.0029492 0.003464 v omega 40.883 1.0313e+05 2685.7 523.37 v TempK 288 341.11 291.71 289.37 v Density 1.205 1.205 1.205 1.205 v TurbVisc 3.6822e-13 0.00011842 7.8857e-05 9.7055e-05 v CourantNb 6.5563e-10 0.00041198 2.278e-05 1.1126e-05 v FourierNb 0.14812 0.62811 0.2441 0.20524 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.8659 4.8659 0.00033124 -1.6806e-07 v volume_forces[Z] -4.8659 4.8659 -0.00033115 2.1601e-07 v ǁvolume_forcesǁ 6.5401e-09 4.8682 0.33716 0.12441 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 291.94 289.52 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.022584 7.6432e-05 4.3535e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14812 0.62811 0.24412 0.20525 INSTANT 0.161784000E+00 TIME STEP NUMBER 168 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.49680E-05 0.33896E-02 Friction velocity uk : 0.51958E-05 0.33892E-02 Dimensionless distance yplus : 0.34599E-04 0.22549E-01 Friction thermal sca. tstar : -0.21553E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.24300E-04 0.15837E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.49680E-05 0.33896E-02 Friction velocity uk : 0.51958E-05 0.33892E-02 Dimensionless distance yplus : 0.34599E-04 0.22549E-01 Friction thermal sca. tstar : -0.21553E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.24300E-04 0.15837E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.52670E-08 4 0.91692E-06 0.42063E-11 0.25887E+01 c Velocity[X] 0.85539E-30 c Velocity[Y] 0.21032E-11 c Velocity[Z] 0.21031E-11 c Pressure 0.85507E-13 26 0.56773E-08 0.68110E-06 0.49430E+01 c k 0.11824E-05 2 0.38554E-06 0.20892E-06 0.41626E+01 c omega 0.13153E+02 1 0.15311E-07 0.15996E+02 0.20821E-01 c TempK 0.94310E+02 1 0.70424E-06 0.18598E+00 0.48013E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -2.1003e-13 1.7685e-13 -2.0119e-17 -5.0262e-18 v Velocity[Y] -0.00022082 0.00022134 -6.6115e-10 -4.5557e-12 v Velocity[Z] -0.00022134 0.00022082 6.3971e-10 -7.5403e-13 v ǁVelocityǁ 1.8991e-10 0.00026415 1.4933e-05 7.5499e-06 v Pressure -0.00027752 0.010352 0.00044799 -2.3533e-21 v k 3.0729e-08 0.0042696 0.0029365 0.0034504 v omega 40.751 1.0313e+05 2685.6 523.25 v TempK 288 341.12 291.72 289.38 v Density 1.205 1.205 1.205 1.205 v TurbVisc 3.6359e-13 0.00011824 7.8774e-05 9.6981e-05 v CourantNb 6.5971e-10 0.00041108 2.2728e-05 1.1103e-05 v FourierNb 0.14809 0.62811 0.24382 0.20505 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.8663 4.8664 0.00033191 -1.6964e-07 v volume_forces[Z] -4.8663 4.8664 -0.00033181 2.1789e-07 v ǁvolume_forcesǁ 6.702e-09 4.8687 0.33784 0.12478 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 291.94 289.52 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.022549 7.6316e-05 4.3467e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14809 0.62811 0.24385 0.20506 INSTANT 0.162747000E+00 TIME STEP NUMBER 169 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.50395E-05 0.33842E-02 Friction velocity uk : 0.52604E-05 0.33838E-02 Dimensionless distance yplus : 0.35028E-04 0.22513E-01 Friction thermal sca. tstar : -0.20590E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.24602E-04 0.15812E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.50395E-05 0.33842E-02 Friction velocity uk : 0.52604E-05 0.33838E-02 Dimensionless distance yplus : 0.35028E-04 0.22513E-01 Friction thermal sca. tstar : -0.20590E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.24602E-04 0.15812E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.52553E-08 4 0.91240E-06 0.42354E-11 0.26035E+01 c Velocity[X] 0.84833E-30 c Velocity[Y] 0.21177E-11 c Velocity[Z] 0.21176E-11 c Pressure 0.85147E-13 26 0.56526E-08 0.67815E-06 0.49140E+01 c k 0.11780E-05 2 0.38084E-06 0.20590E-06 0.41485E+01 c omega 0.13153E+02 1 0.15195E-07 0.15796E+02 0.20690E-01 c TempK 0.94311E+02 1 0.69899E-06 0.18443E+00 0.47811E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -2.0938e-13 1.763e-13 -2.0051e-17 -5.0098e-18 v Velocity[Y] -0.0002203 0.00022081 -6.6477e-10 -4.5313e-12 v Velocity[Z] -0.00022081 0.0002203 6.4294e-10 -7.4963e-13 v ǁVelocityǁ 1.9447e-10 0.00026345 1.4901e-05 7.5369e-06 v Pressure -0.00027922 0.010384 0.00045 3.7726e-20 v k 3.0346e-08 0.0042496 0.0029239 0.0034368 v omega 40.621 1.0313e+05 2685.5 523.13 v TempK 288 341.12 291.72 289.38 v Density 1.205 1.205 1.205 1.205 v TurbVisc 3.5904e-13 0.00011806 7.8692e-05 9.6907e-05 v CourantNb 6.6379e-10 0.00041017 2.2675e-05 1.108e-05 v FourierNb 0.14806 0.62811 0.24355 0.20486 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.8668 4.8669 0.00033258 -1.7121e-07 v volume_forces[Z] -4.8668 4.8669 -0.00033248 2.1975e-07 v ǁvolume_forcesǁ 6.8653e-09 4.8691 0.33851 0.12515 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 291.95 289.53 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.022513 7.62e-05 4.3399e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14807 0.62811 0.24357 0.20487 INSTANT 0.163710000E+00 TIME STEP NUMBER 170 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.51105E-05 0.33789E-02 Friction velocity uk : 0.53247E-05 0.33785E-02 Dimensionless distance yplus : 0.35456E-04 0.22477E-01 Friction thermal sca. tstar : -0.20810E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.24902E-04 0.15787E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.51105E-05 0.33789E-02 Friction velocity uk : 0.53247E-05 0.33785E-02 Dimensionless distance yplus : 0.35456E-04 0.22477E-01 Friction thermal sca. tstar : -0.20810E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.24902E-04 0.15787E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.52436E-08 4 0.90781E-06 0.42631E-11 0.26180E+01 c Velocity[X] 0.84122E-30 c Velocity[Y] 0.21316E-11 c Velocity[Z] 0.21315E-11 c Pressure 0.84486E-13 26 0.56152E-08 0.67280E-06 0.48853E+01 c k 0.11735E-05 2 0.37624E-06 0.20294E-06 0.41345E+01 c omega 0.13153E+02 1 0.15080E-07 0.15598E+02 0.20561E-01 c TempK 0.94312E+02 1 0.69380E-06 0.18289E+00 0.47611E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -2.0874e-13 1.7575e-13 -1.9984e-17 -4.9936e-18 v Velocity[Y] -0.00021978 0.00022028 -6.6837e-10 -4.507e-12 v Velocity[Z] -0.00022028 0.00021978 6.4615e-10 -7.454e-13 v ǁVelocityǁ 1.9907e-10 0.00026275 1.4869e-05 7.5237e-06 v Pressure -0.00028093 0.010415 0.00045201 -4.7923e-20 v k 2.997e-08 0.0042297 0.0029114 0.0034233 v omega 40.491 1.0313e+05 2685.4 523.02 v TempK 288 341.13 291.73 289.39 v Density 1.205 1.205 1.205 1.205 v TurbVisc 3.5457e-13 0.00011787 7.8609e-05 9.6833e-05 v CourantNb 6.6787e-10 0.00040926 2.2622e-05 1.1057e-05 v FourierNb 0.14804 0.62811 0.24327 0.20467 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.8672 4.8673 0.00033324 -1.7277e-07 v volume_forces[Z] -4.8672 4.8673 -0.00033314 2.216e-07 v ǁvolume_forcesǁ 7.03e-09 4.8696 0.33918 0.12553 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 291.96 289.53 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.022477 7.6084e-05 4.3331e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14804 0.62811 0.2433 0.20468 INSTANT 0.164673000E+00 TIME STEP NUMBER 171 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.51810E-05 0.33735E-02 Friction velocity uk : 0.53887E-05 0.33732E-02 Dimensionless distance yplus : 0.35883E-04 0.22442E-01 Friction thermal sca. tstar : -0.22003E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.25202E-04 0.15762E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.51810E-05 0.33735E-02 Friction velocity uk : 0.53887E-05 0.33732E-02 Dimensionless distance yplus : 0.35883E-04 0.22442E-01 Friction thermal sca. tstar : -0.22003E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.25202E-04 0.15762E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.52317E-08 4 0.92249E-06 0.42897E-11 0.26321E+01 c Velocity[X] 0.83402E-30 c Velocity[Y] 0.21449E-11 c Velocity[Z] 0.21448E-11 c Pressure 0.84101E-13 26 0.55903E-08 0.66965E-06 0.48569E+01 c k 0.11691E-05 2 0.37172E-06 0.20002E-06 0.41206E+01 c omega 0.13153E+02 1 0.14966E-07 0.15404E+02 0.20432E-01 c TempK 0.94313E+02 1 0.68868E-06 0.18138E+00 0.47413E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -2.081e-13 1.7521e-13 -1.9917e-17 -4.9775e-18 v Velocity[Y] -0.00021926 0.00021975 -6.7196e-10 -4.4831e-12 v Velocity[Z] -0.00021975 0.00021926 6.4934e-10 -7.4118e-13 v ǁVelocityǁ 2.037e-10 0.00026205 1.4837e-05 7.5105e-06 v Pressure -0.00028263 0.010447 0.00045401 2.444e-20 v k 2.9599e-08 0.00421 0.002899 0.00341 v omega 40.362 1.0313e+05 2685.3 522.9 v TempK 288 341.13 291.74 289.39 v Density 1.205 1.205 1.205 1.205 v TurbVisc 3.5017e-13 0.00011769 7.8528e-05 9.676e-05 v CourantNb 6.7196e-10 0.00040835 2.2569e-05 1.1033e-05 v FourierNb 0.14801 0.62811 0.243 0.20449 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.8677 4.8678 0.0003339 -1.7433e-07 v volume_forces[Z] -4.8677 4.8678 -0.0003338 2.2344e-07 v ǁvolume_forcesǁ 7.1962e-09 4.87 0.33984 0.1259 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 291.96 289.54 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.022442 7.5969e-05 4.3264e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14801 0.62811 0.24303 0.2045 INSTANT 0.165636000E+00 TIME STEP NUMBER 172 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.52510E-05 0.33682E-02 Friction velocity uk : 0.54525E-05 0.33678E-02 Dimensionless distance yplus : 0.36308E-04 0.22406E-01 Friction thermal sca. tstar : -0.23432E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.25500E-04 0.15737E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.52510E-05 0.33682E-02 Friction velocity uk : 0.54525E-05 0.33678E-02 Dimensionless distance yplus : 0.36308E-04 0.22406E-01 Friction thermal sca. tstar : -0.23432E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.25500E-04 0.15737E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.52198E-08 4 0.89879E-06 0.43148E-11 0.26459E+01 c Velocity[X] 0.82676E-30 c Velocity[Y] 0.21575E-11 c Velocity[Z] 0.21574E-11 c Pressure 0.83527E-13 26 0.55567E-08 0.66500E-06 0.48288E+01 c k 0.11648E-05 2 0.36729E-06 0.19716E-06 0.41068E+01 c omega 0.13153E+02 1 0.14854E-07 0.15213E+02 0.20305E-01 c TempK 0.94313E+02 1 0.68362E-06 0.17989E+00 0.47217E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -2.0746e-13 1.7466e-13 -1.9851e-17 -4.9616e-18 v Velocity[Y] -0.00021874 0.00021921 -6.7553e-10 -4.4594e-12 v Velocity[Z] -0.00021922 0.00021874 6.5252e-10 -7.3746e-13 v ǁVelocityǁ 2.0837e-10 0.00026135 1.4805e-05 7.4971e-06 v Pressure -0.00028433 0.010478 0.00045601 4.6085e-21 v k 2.9235e-08 0.0041903 0.0028867 0.0033967 v omega 40.233 1.0313e+05 2685.2 522.78 v TempK 288 341.14 291.74 289.39 v Density 1.205 1.205 1.205 1.205 v TurbVisc 3.4585e-13 0.0001175 7.8446e-05 9.6686e-05 v CourantNb 6.7604e-10 0.00040743 2.2515e-05 1.101e-05 v FourierNb 0.14798 0.62811 0.24273 0.2043 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.8681 4.8682 0.00033455 -1.7587e-07 v volume_forces[Z] -4.8681 4.8682 -0.00033445 2.2527e-07 v ǁvolume_forcesǁ 7.3637e-09 4.8705 0.34051 0.12627 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 291.97 289.54 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.022406 7.5854e-05 4.3196e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14798 0.62811 0.24276 0.20431 INSTANT 0.166599000E+00 TIME STEP NUMBER 173 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.53205E-05 0.33629E-02 Friction velocity uk : 0.55160E-05 0.33625E-02 Dimensionless distance yplus : 0.36731E-04 0.22371E-01 Friction thermal sca. tstar : -0.25187E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.25797E-04 0.15712E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.53205E-05 0.33629E-02 Friction velocity uk : 0.55160E-05 0.33625E-02 Dimensionless distance yplus : 0.36731E-04 0.22371E-01 Friction thermal sca. tstar : -0.25187E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.25797E-04 0.15712E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.52078E-08 4 0.89431E-06 0.43387E-11 0.26593E+01 c Velocity[X] 0.81944E-30 c Velocity[Y] 0.21694E-11 c Velocity[Z] 0.21693E-11 c Pressure 0.83034E-13 26 0.55272E-08 0.66099E-06 0.48011E+01 c k 0.11604E-05 2 0.36294E-06 0.19434E-06 0.40931E+01 c omega 0.13153E+02 1 0.14742E-07 0.15025E+02 0.20179E-01 c TempK 0.94314E+02 1 0.67862E-06 0.17842E+00 0.47023E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -2.0683e-13 1.7412e-13 -1.9786e-17 -4.9458e-18 v Velocity[Y] -0.00021822 0.00021868 -6.7908e-10 -4.4357e-12 v Velocity[Z] -0.00021869 0.00021822 6.5567e-10 -7.3362e-13 v ǁVelocityǁ 2.1308e-10 0.00026065 1.4773e-05 7.4837e-06 v Pressure -0.00028604 0.01051 0.000458 -2.0101e-21 v k 2.8877e-08 0.0041709 0.0028745 0.0033835 v omega 40.106 1.0313e+05 2685.1 522.66 v TempK 288 341.14 291.75 289.4 v Density 1.205 1.205 1.205 1.205 v TurbVisc 3.4159e-13 0.00011737 7.8365e-05 9.6614e-05 v CourantNb 6.8013e-10 0.00040651 2.2462e-05 1.0986e-05 v FourierNb 0.14795 0.62811 0.24247 0.20411 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.8686 4.8687 0.00033521 -1.774e-07 v volume_forces[Z] -4.8686 4.8687 -0.00033511 2.2709e-07 v ǁvolume_forcesǁ 7.5326e-09 4.8709 0.34117 0.12664 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 291.98 289.54 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.022371 7.574e-05 4.3129e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14795 0.62811 0.24249 0.20413 INSTANT 0.167562000E+00 TIME STEP NUMBER 174 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.53896E-05 0.33576E-02 Friction velocity uk : 0.55793E-05 0.33573E-02 Dimensionless distance yplus : 0.37152E-04 0.22336E-01 Friction thermal sca. tstar : -0.27414E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.26093E-04 0.15687E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.53896E-05 0.33576E-02 Friction velocity uk : 0.55793E-05 0.33573E-02 Dimensionless distance yplus : 0.37152E-04 0.22336E-01 Friction thermal sca. tstar : -0.27414E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.26093E-04 0.15687E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.51957E-08 4 0.88979E-06 0.43613E-11 0.26724E+01 c Velocity[X] 0.81206E-30 c Velocity[Y] 0.21807E-11 c Velocity[Z] 0.21806E-11 c Pressure 0.82554E-13 26 0.54975E-08 0.65709E-06 0.47736E+01 c k 0.11561E-05 2 0.35867E-06 0.19158E-06 0.40794E+01 c omega 0.13153E+02 1 0.14632E-07 0.14839E+02 0.20054E-01 c TempK 0.94315E+02 1 0.67369E-06 0.17697E+00 0.46831E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -2.0619e-13 1.7358e-13 -1.9722e-17 -4.9302e-18 v Velocity[Y] -0.0002177 0.00021815 -6.8261e-10 -4.4122e-12 v Velocity[Z] -0.00021816 0.0002177 6.588e-10 -7.2994e-13 v ǁVelocityǁ 2.1783e-10 0.00025995 1.474e-05 7.4702e-06 v Pressure -0.00028774 0.010541 0.00045999 -1.7184e-20 v k 2.8525e-08 0.0041515 0.0028623 0.0033705 v omega 39.979 1.0313e+05 2685 522.55 v TempK 288 341.15 291.76 289.4 v Density 1.205 1.205 1.205 1.205 v TurbVisc 3.3741e-13 0.00011723 7.8285e-05 9.6541e-05 v CourantNb 6.8422e-10 0.00040558 2.2408e-05 1.0962e-05 v FourierNb 0.14792 0.62811 0.2422 0.20393 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.869 4.8691 0.00033586 -1.7893e-07 v volume_forces[Z] -4.869 4.8691 -0.00033576 2.289e-07 v ǁvolume_forcesǁ 7.7029e-09 4.8713 0.34183 0.127 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 291.99 289.55 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.022336 7.5625e-05 4.3062e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14793 0.62811 0.24223 0.20394 INSTANT 0.168525000E+00 TIME STEP NUMBER 175 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.54582E-05 0.33523E-02 Friction velocity uk : 0.56424E-05 0.33520E-02 Dimensionless distance yplus : 0.37572E-04 0.22301E-01 Friction thermal sca. tstar : -0.30368E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.26388E-04 0.15663E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.54582E-05 0.33523E-02 Friction velocity uk : 0.56424E-05 0.33520E-02 Dimensionless distance yplus : 0.37572E-04 0.22301E-01 Friction thermal sca. tstar : -0.30368E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.26388E-04 0.15663E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.51836E-08 4 0.88541E-06 0.43825E-11 0.26852E+01 c Velocity[X] 0.80464E-30 c Velocity[Y] 0.21913E-11 c Velocity[Z] 0.21912E-11 c Pressure 0.82100E-13 25 0.54693E-08 0.65339E-06 0.47465E+01 c k 0.11519E-05 2 0.35449E-06 0.18886E-06 0.40659E+01 c omega 0.13153E+02 1 0.14523E-07 0.14657E+02 0.19930E-01 c TempK 0.94316E+02 1 0.66881E-06 0.17554E+00 0.46640E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -2.0556e-13 1.7303e-13 -1.9658e-17 -4.9147e-18 v Velocity[Y] -0.00021718 0.00021762 -6.8613e-10 -4.3923e-12 v Velocity[Z] -0.00021762 0.00021718 6.6191e-10 -7.2792e-13 v ǁVelocityǁ 2.2261e-10 0.00025925 1.4708e-05 7.4566e-06 v Pressure -0.00028945 0.010572 0.00046198 -5.4174e-21 v k 2.8179e-08 0.0041323 0.0028503 0.0033575 v omega 39.853 1.0313e+05 2684.9 522.43 v TempK 288 341.15 291.77 289.41 v Density 1.205 1.205 1.205 1.205 v TurbVisc 3.333e-13 0.00011709 7.8205e-05 9.6469e-05 v CourantNb 6.8832e-10 0.00040465 2.2354e-05 1.0938e-05 v FourierNb 0.1479 0.62811 0.24194 0.20375 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.8695 4.8695 0.0003365 -1.8045e-07 v volume_forces[Z] -4.8695 4.8695 -0.0003364 2.3069e-07 v ǁvolume_forcesǁ 7.8745e-09 4.8718 0.34248 0.12737 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 291.99 289.55 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.022301 7.5511e-05 4.2996e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.1479 0.62811 0.24196 0.20376 INSTANT 0.169488000E+00 TIME STEP NUMBER 176 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.55264E-05 0.33471E-02 Friction velocity uk : 0.57052E-05 0.33467E-02 Dimensionless distance yplus : 0.37990E-04 0.22266E-01 Friction thermal sca. tstar : -0.34558E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.26682E-04 0.15638E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.55264E-05 0.33471E-02 Friction velocity uk : 0.57052E-05 0.33467E-02 Dimensionless distance yplus : 0.37990E-04 0.22266E-01 Friction thermal sca. tstar : -0.34558E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.26682E-04 0.15638E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.51714E-08 4 0.88101E-06 0.44024E-11 0.26977E+01 c Velocity[X] 0.79719E-30 c Velocity[Y] 0.22012E-11 c Velocity[Z] 0.22011E-11 c Pressure 0.81592E-13 25 0.54407E-08 0.64927E-06 0.47196E+01 c k 0.11476E-05 2 0.35038E-06 0.18620E-06 0.40524E+01 c omega 0.13153E+02 1 0.14415E-07 0.14477E+02 0.19808E-01 c TempK 0.94316E+02 1 0.66399E-06 0.17412E+00 0.46452E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -2.0494e-13 1.725e-13 -1.9594e-17 -4.8994e-18 v Velocity[Y] -0.00021666 0.00021709 -6.8963e-10 -4.3691e-12 v Velocity[Z] -0.00021709 0.00021666 6.65e-10 -7.2441e-13 v ǁVelocityǁ 2.2744e-10 0.00025855 1.4675e-05 7.4429e-06 v Pressure -0.00029116 0.010603 0.00046396 -1.0369e-20 v k 2.7838e-08 0.0041132 0.0028384 0.0033446 v omega 39.728 1.0313e+05 2684.8 522.32 v TempK 288 341.16 291.77 289.41 v Density 1.205 1.205 1.205 1.205 v TurbVisc 3.2925e-13 0.00011696 7.8125e-05 9.6397e-05 v CourantNb 6.9241e-10 0.00040372 2.23e-05 1.0914e-05 v FourierNb 0.14787 0.62811 0.24168 0.20356 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.8699 4.87 0.00033715 -1.8196e-07 v volume_forces[Z] -4.8699 4.87 -0.00033705 2.3248e-07 v ǁvolume_forcesǁ 8.0474e-09 4.8722 0.34313 0.12774 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292 289.56 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.022266 7.5398e-05 4.2929e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14787 0.62811 0.2417 0.20358 INSTANT 0.170451000E+00 TIME STEP NUMBER 177 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.55942E-05 0.33419E-02 Friction velocity uk : 0.57679E-05 0.33415E-02 Dimensionless distance yplus : 0.38408E-04 0.22231E-01 Friction thermal sca. tstar : -0.41178E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.26975E-04 0.15614E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.55942E-05 0.33419E-02 Friction velocity uk : 0.57679E-05 0.33415E-02 Dimensionless distance yplus : 0.38408E-04 0.22231E-01 Friction thermal sca. tstar : -0.41178E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.26975E-04 0.15614E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.51592E-08 4 0.87667E-06 0.44209E-11 0.27097E+01 c Velocity[X] 0.78969E-30 c Velocity[Y] 0.22105E-11 c Velocity[Z] 0.22104E-11 c Pressure 0.81262E-13 25 0.54181E-08 0.64657E-06 0.46931E+01 c k 0.11434E-05 2 0.34634E-06 0.18357E-06 0.40391E+01 c omega 0.13153E+02 1 0.14308E-07 0.14300E+02 0.19686E-01 c TempK 0.94317E+02 1 0.65923E-06 0.17273E+00 0.46265E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -2.0431e-13 1.7196e-13 -1.9531e-17 -4.8842e-18 v Velocity[Y] -0.00021614 0.00021656 -6.931e-10 -4.3459e-12 v Velocity[Z] -0.00021656 0.00021615 6.6808e-10 -7.2104e-13 v ǁVelocityǁ 2.3229e-10 0.00025785 1.4642e-05 7.4291e-06 v Pressure -0.00029286 0.010634 0.00046594 -8.6777e-21 v k 2.7503e-08 0.0040953 0.0028265 0.0033318 v omega 39.604 1.0313e+05 2684.7 522.2 v TempK 288 341.16 291.78 289.41 v Density 1.205 1.205 1.205 1.205 v TurbVisc 3.2527e-13 0.00011682 7.8046e-05 9.6325e-05 v CourantNb 6.9651e-10 0.00040278 2.2246e-05 1.089e-05 v FourierNb 0.14784 0.62811 0.24142 0.20338 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.8703 4.8704 0.00033779 -1.8346e-07 v volume_forces[Z] -4.8703 4.8704 -0.00033769 2.3426e-07 v ǁvolume_forcesǁ 8.2218e-09 4.8726 0.34378 0.1281 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.01 289.56 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.022231 7.5285e-05 4.2863e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14784 0.62811 0.24144 0.20339 INSTANT 0.171414000E+00 TIME STEP NUMBER 178 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.56615E-05 0.33366E-02 Friction velocity uk : 0.58303E-05 0.33363E-02 Dimensionless distance yplus : 0.38823E-04 0.22197E-01 Friction thermal sca. tstar : -0.54109E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.27267E-04 0.15590E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.56615E-05 0.33366E-02 Friction velocity uk : 0.58303E-05 0.33363E-02 Dimensionless distance yplus : 0.38823E-04 0.22197E-01 Friction thermal sca. tstar : -0.54109E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.27267E-04 0.15590E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.51470E-08 4 0.87230E-06 0.44381E-11 0.27215E+01 c Velocity[X] 0.78217E-30 c Velocity[Y] 0.22191E-11 c Velocity[Z] 0.22190E-11 c Pressure 0.80647E-13 25 0.53836E-08 0.64160E-06 0.46668E+01 c k 0.11392E-05 2 0.34239E-06 0.18100E-06 0.40258E+01 c omega 0.13153E+02 1 0.14203E-07 0.14125E+02 0.19566E-01 c TempK 0.94318E+02 1 0.65453E-06 0.17136E+00 0.46080E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -2.0369e-13 1.7142e-13 -1.9469e-17 -4.8691e-18 v Velocity[Y] -0.00021563 0.00021603 -6.9657e-10 -4.3231e-12 v Velocity[Z] -0.00021603 0.00021563 6.7113e-10 -7.1741e-13 v ǁVelocityǁ 2.3719e-10 0.00025715 1.461e-05 7.4153e-06 v Pressure -0.00029457 0.010665 0.00046792 -1.2869e-20 v k 2.7173e-08 0.0040777 0.0028148 0.003319 v omega 39.48 1.0313e+05 2684.6 522.09 v TempK 288 341.17 291.79 289.42 v Density 1.205 1.205 1.205 1.205 v TurbVisc 3.2135e-13 0.00011668 7.7968e-05 9.6254e-05 v CourantNb 7.0061e-10 0.00040185 2.2191e-05 1.0866e-05 v FourierNb 0.14781 0.62811 0.24116 0.2032 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.8708 4.8708 0.00033843 -1.8495e-07 v volume_forces[Z] -4.8708 4.8708 -0.00033833 2.3602e-07 v ǁvolume_forcesǁ 8.3974e-09 4.8731 0.34443 0.12847 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.02 289.57 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.022197 7.5171e-05 4.2796e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14782 0.62811 0.24118 0.20321 INSTANT 0.172377000E+00 TIME STEP NUMBER 179 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.57285E-05 0.33314E-02 Friction velocity uk : 0.58925E-05 0.33311E-02 Dimensionless distance yplus : 0.39237E-04 0.22162E-01 Friction thermal sca. tstar : -0.10385E+05 0.00000E+00 Dim-less thermal sca. tplus : 0.27558E-04 0.15565E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.57285E-05 0.33314E-02 Friction velocity uk : 0.58925E-05 0.33311E-02 Dimensionless distance yplus : 0.39237E-04 0.22162E-01 Friction thermal sca. tstar : -0.10385E+05 0.00000E+00 Dim-less thermal sca. tplus : 0.27558E-04 0.15565E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.51346E-08 4 0.86790E-06 0.44540E-11 0.27329E+01 c Velocity[X] 0.77460E-30 c Velocity[Y] 0.22270E-11 c Velocity[Z] 0.22269E-11 c Pressure 0.80159E-13 25 0.53550E-08 0.63765E-06 0.46408E+01 c k 0.11350E-05 2 0.33850E-06 0.17847E-06 0.40126E+01 c omega 0.13153E+02 1 0.14098E-07 0.13953E+02 0.19446E-01 c TempK 0.94319E+02 1 0.64988E-06 0.17000E+00 0.45896E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -2.0307e-13 1.7089e-13 -1.9408e-17 -4.8543e-18 v Velocity[Y] -0.00021511 0.0002155 -7.0001e-10 -4.3007e-12 v Velocity[Z] -0.0002155 0.00021511 6.7416e-10 -7.1448e-13 v ǁVelocityǁ 2.3843e-10 0.00025645 1.4577e-05 7.4014e-06 v Pressure -0.00029627 0.010696 0.00046989 3.8192e-20 v k 2.6849e-08 0.0040602 0.0028031 0.0033064 v omega 39.358 1.0313e+05 2684.5 521.98 v TempK 288 341.17 291.79 289.42 v Density 1.205 1.205 1.205 1.205 v TurbVisc 3.175e-13 0.00011655 7.7889e-05 9.6183e-05 v CourantNb 7.0471e-10 0.00040091 2.2137e-05 1.0841e-05 v FourierNb 0.14779 0.62811 0.24091 0.20302 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.8712 4.8713 0.00033907 -1.8643e-07 v volume_forces[Z] -4.8712 4.8713 -0.00033897 2.3778e-07 v ǁvolume_forcesǁ 8.5743e-09 4.8735 0.34508 0.12883 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.02 289.57 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.022162 7.5058e-05 4.273e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14779 0.62811 0.24093 0.20304 INSTANT 0.173340000E+00 TIME STEP NUMBER 180 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.57731E-05 0.33263E-02 Friction velocity uk : 0.59226E-05 0.33259E-02 Dimensionless distance yplus : 0.39442E-04 0.22128E-01 Friction thermal sca. tstar : -0.92381E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.27701E-04 0.15541E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.57731E-05 0.33263E-02 Friction velocity uk : 0.59226E-05 0.33259E-02 Dimensionless distance yplus : 0.39442E-04 0.22128E-01 Friction thermal sca. tstar : -0.92381E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.27701E-04 0.15541E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.51223E-08 4 0.86358E-06 0.44685E-11 0.27439E+01 c Velocity[X] 0.76702E-30 c Velocity[Y] 0.22343E-11 c Velocity[Z] 0.22342E-11 c Pressure 0.79704E-13 25 0.53273E-08 0.63395E-06 0.46151E+01 c k 0.11309E-05 2 0.33469E-06 0.17598E-06 0.39995E+01 c omega 0.13153E+02 1 0.13994E-07 0.13784E+02 0.19328E-01 c TempK 0.94319E+02 1 0.64528E-06 0.16866E+00 0.45715E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -2.0246e-13 1.7035e-13 -1.9346e-17 -4.8395e-18 v Velocity[Y] -0.00021459 0.00021497 -7.0344e-10 -4.278e-12 v Velocity[Z] -0.00021498 0.0002146 6.7718e-10 -7.1106e-13 v ǁVelocityǁ 2.3673e-10 0.00025575 1.4544e-05 7.3874e-06 v Pressure -0.00029798 0.010727 0.00047186 6.17e-20 v k 2.6529e-08 0.0040427 0.0027915 0.0032939 v omega 39.236 1.0313e+05 2684.4 521.87 v TempK 288 341.18 291.8 289.43 v Density 1.205 1.205 1.205 1.205 v TurbVisc 3.1371e-13 0.00011641 7.7811e-05 9.6112e-05 v CourantNb 7.0881e-10 0.00039997 2.2083e-05 1.0817e-05 v FourierNb 0.14776 0.62811 0.24065 0.20285 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.8716 4.8717 0.00033971 -1.8791e-07 v volume_forces[Z] -4.8716 4.8717 -0.0003396 2.3952e-07 v ǁvolume_forcesǁ 8.6193e-09 4.8739 0.34572 0.12919 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.03 289.57 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.022128 7.4948e-05 4.2665e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14776 0.62811 0.24067 0.20286 INSTANT 0.174303000E+00 TIME STEP NUMBER 181 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.57491E-05 0.33211E-02 Friction velocity uk : 0.58966E-05 0.33208E-02 Dimensionless distance yplus : 0.39269E-04 0.22093E-01 Friction thermal sca. tstar : -0.52196E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.27580E-04 0.15517E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.57491E-05 0.33211E-02 Friction velocity uk : 0.58966E-05 0.33208E-02 Dimensionless distance yplus : 0.39269E-04 0.22093E-01 Friction thermal sca. tstar : -0.52196E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.27580E-04 0.15517E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.51099E-08 4 0.85929E-06 0.44817E-11 0.27546E+01 c Velocity[X] 0.75942E-30 c Velocity[Y] 0.22409E-11 c Velocity[Z] 0.22408E-11 c Pressure 0.79229E-13 25 0.52994E-08 0.63010E-06 0.45896E+01 c k 0.11268E-05 2 0.33094E-06 0.17353E-06 0.39865E+01 c omega 0.13153E+02 1 0.13892E-07 0.13617E+02 0.19211E-01 c TempK 0.94320E+02 1 0.64075E-06 0.16734E+00 0.45534E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -2.0185e-13 1.6982e-13 -1.9286e-17 -4.8249e-18 v Velocity[Y] -0.00021408 0.00021444 -7.0685e-10 -4.2558e-12 v Velocity[Z] -0.00021445 0.00021408 6.8017e-10 -7.0821e-13 v ǁVelocityǁ 2.3502e-10 0.00025505 1.4511e-05 7.3734e-06 v Pressure -0.00029969 0.010757 0.00047382 -2.0689e-20 v k 2.6215e-08 0.0040254 0.00278 0.0032814 v omega 39.114 1.0313e+05 2684.3 521.76 v TempK 288 341.18 291.81 289.43 v Density 1.205 1.205 1.205 1.205 v TurbVisc 3.0998e-13 0.00011628 7.7734e-05 9.6041e-05 v CourantNb 7.1291e-10 0.00039902 2.2028e-05 1.0792e-05 v FourierNb 0.14773 0.62811 0.2404 0.20267 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.872 4.8721 0.00034034 -1.8938e-07 v volume_forces[Z] -4.872 4.8721 -0.00034024 2.4126e-07 v ǁvolume_forcesǁ 8.558e-09 4.8743 0.34636 0.12956 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.04 289.58 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.022093 7.484e-05 4.2602e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14773 0.62811 0.24042 0.20268 INSTANT 0.175266000E+00 TIME STEP NUMBER 182 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.57248E-05 0.33160E-02 Friction velocity uk : 0.58703E-05 0.33156E-02 Dimensionless distance yplus : 0.39094E-04 0.22059E-01 Friction thermal sca. tstar : -0.40242E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.27457E-04 0.15493E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.57248E-05 0.33160E-02 Friction velocity uk : 0.58703E-05 0.33156E-02 Dimensionless distance yplus : 0.39094E-04 0.22059E-01 Friction thermal sca. tstar : -0.40242E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.27457E-04 0.15493E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.50974E-08 4 0.85501E-06 0.44936E-11 0.27649E+01 c Velocity[X] 0.75180E-30 c Velocity[Y] 0.22468E-11 c Velocity[Z] 0.22467E-11 c Pressure 0.78743E-13 25 0.52692E-08 0.62616E-06 0.45645E+01 c k 0.11227E-05 2 0.32727E-06 0.17113E-06 0.39736E+01 c omega 0.13153E+02 1 0.13790E-07 0.13453E+02 0.19094E-01 c TempK 0.94321E+02 1 0.63626E-06 0.16604E+00 0.45356E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -2.0124e-13 1.6929e-13 -1.9226e-17 -4.8104e-18 v Velocity[Y] -0.00021357 0.00021392 -7.1024e-10 -4.2337e-12 v Velocity[Z] -0.00021392 0.00021357 6.8315e-10 -7.0544e-13 v ǁVelocityǁ 2.333e-10 0.00025435 1.4478e-05 7.3593e-06 v Pressure -0.00030139 0.010788 0.00047578 6.1013e-20 v k 2.5906e-08 0.0040083 0.0027686 0.003269 v omega 38.994 1.0313e+05 2684.2 521.65 v TempK 288 341.19 291.82 289.44 v Density 1.205 1.205 1.205 1.205 v TurbVisc 3.0631e-13 0.00011614 7.7657e-05 9.5971e-05 v CourantNb 7.1701e-10 0.00039808 2.1974e-05 1.0768e-05 v FourierNb 0.1477 0.62811 0.24015 0.20249 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.8725 4.8725 0.00034097 -1.9084e-07 v volume_forces[Z] -4.8725 4.8725 -0.00034087 2.4298e-07 v ǁvolume_forcesǁ 8.4961e-09 4.8747 0.34699 0.12992 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.04 289.58 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.022059 7.4732e-05 4.2539e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14771 0.62811 0.24017 0.2025 INSTANT 0.176229000E+00 TIME STEP NUMBER 183 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.57001E-05 0.33109E-02 Friction velocity uk : 0.58437E-05 0.33105E-02 Dimensionless distance yplus : 0.38916E-04 0.22025E-01 Friction thermal sca. tstar : -0.33931E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.27332E-04 0.15469E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.57001E-05 0.33109E-02 Friction velocity uk : 0.58437E-05 0.33105E-02 Dimensionless distance yplus : 0.38916E-04 0.22025E-01 Friction thermal sca. tstar : -0.33931E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.27332E-04 0.15469E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.50850E-08 4 0.85072E-06 0.45041E-11 0.27749E+01 c Velocity[X] 0.74417E-30 c Velocity[Y] 0.22521E-11 c Velocity[Z] 0.22520E-11 c Pressure 0.78266E-13 25 0.52476E-08 0.62230E-06 0.45396E+01 c k 0.11187E-05 2 0.32366E-06 0.16876E-06 0.39608E+01 c omega 0.13153E+02 1 0.13690E-07 0.13291E+02 0.18979E-01 c TempK 0.94322E+02 1 0.63183E-06 0.16475E+00 0.45179E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -2.0063e-13 1.6877e-13 -1.9167e-17 -4.7961e-18 v Velocity[Y] -0.00021306 0.00021339 -7.1392e-10 -4.503e-12 v Velocity[Z] -0.0002134 0.00021306 6.8592e-10 -8.8715e-13 v ǁVelocityǁ 2.3183e-10 0.00025366 1.4445e-05 7.3452e-06 v Pressure -0.0003031 0.010818 0.00047774 -4.508e-20 v k 2.5602e-08 0.0039912 0.0027572 0.0032567 v omega 38.874 1.0313e+05 2684.1 521.54 v TempK 288 341.19 291.82 289.44 v Density 1.205 1.205 1.205 1.205 v TurbVisc 3.027e-13 0.000116 7.758e-05 9.5901e-05 v CourantNb 7.2114e-10 0.00039713 2.1919e-05 1.0743e-05 v FourierNb 0.14768 0.62811 0.2399 0.20232 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.8729 4.8729 0.0003416 -1.9229e-07 v volume_forces[Z] -4.8729 4.8729 -0.00034149 2.447e-07 v ǁvolume_forcesǁ 8.4336e-09 4.8751 0.34763 0.13028 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.05 289.59 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.022025 7.4625e-05 4.2475e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14768 0.62811 0.23992 0.20233 INSTANT 0.177192000E+00 TIME STEP NUMBER 184 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.56788E-05 0.33058E-02 Friction velocity uk : 0.58205E-05 0.33054E-02 Dimensionless distance yplus : 0.38762E-04 0.21991E-01 Friction thermal sca. tstar : -0.29879E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.27224E-04 0.15445E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.56788E-05 0.33058E-02 Friction velocity uk : 0.58205E-05 0.33054E-02 Dimensionless distance yplus : 0.38762E-04 0.21991E-01 Friction thermal sca. tstar : -0.29879E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.27224E-04 0.15445E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.50725E-08 4 0.84652E-06 0.45134E-11 0.27846E+01 c Velocity[X] 0.73653E-30 c Velocity[Y] 0.22567E-11 c Velocity[Z] 0.22567E-11 c Pressure 0.77904E-13 25 0.52247E-08 0.61935E-06 0.45149E+01 c k 0.11146E-05 2 0.32011E-06 0.16644E-06 0.39480E+01 c omega 0.13153E+02 1 0.13590E-07 0.13131E+02 0.18865E-01 c TempK 0.94323E+02 1 0.62744E-06 0.16348E+00 0.45004E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -2.0003e-13 1.6824e-13 -1.9108e-17 -4.7819e-18 v Velocity[Y] -0.00021255 0.00021287 -7.1727e-10 -4.483e-12 v Velocity[Z] -0.00021287 0.00021255 6.8886e-10 -8.8294e-13 v ǁVelocityǁ 2.2995e-10 0.00025296 1.4412e-05 7.3311e-06 v Pressure -0.00030481 0.010849 0.00047969 -4.4271e-20 v k 2.5303e-08 0.0039742 0.002746 0.0032445 v omega 38.755 1.0313e+05 2684.1 521.43 v TempK 288 341.19 291.83 289.44 v Density 1.205 1.205 1.205 1.205 v TurbVisc 2.9914e-13 0.00011587 7.7504e-05 9.5832e-05 v CourantNb 7.2525e-10 0.00039618 2.1864e-05 1.0718e-05 v FourierNb 0.14765 0.62811 0.23965 0.20215 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.8733 4.8733 0.00034222 -1.9374e-07 v volume_forces[Z] -4.8733 4.8733 -0.00034212 2.4642e-07 v ǁvolume_forcesǁ 8.3807e-09 4.8755 0.34826 0.13063 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.06 289.59 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.021991 7.4517e-05 4.2412e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14765 0.62811 0.23968 0.20216 INSTANT 0.178155000E+00 TIME STEP NUMBER 185 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.56515E-05 0.33007E-02 Friction velocity uk : 0.57914E-05 0.33004E-02 Dimensionless distance yplus : 0.38568E-04 0.21958E-01 Friction thermal sca. tstar : -0.26994E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.27088E-04 0.15422E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.56515E-05 0.33007E-02 Friction velocity uk : 0.57914E-05 0.33004E-02 Dimensionless distance yplus : 0.38568E-04 0.21958E-01 Friction thermal sca. tstar : -0.26994E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.27088E-04 0.15422E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.50600E-08 4 0.84229E-06 0.45214E-11 0.27939E+01 c Velocity[X] 0.72889E-30 c Velocity[Y] 0.22607E-11 c Velocity[Z] 0.22607E-11 c Pressure 0.77323E-13 25 0.51914E-08 0.61466E-06 0.44905E+01 c k 0.11106E-05 2 0.31663E-06 0.16416E-06 0.39354E+01 c omega 0.13153E+02 1 0.13492E-07 0.12974E+02 0.18752E-01 c TempK 0.94323E+02 1 0.62311E-06 0.16222E+00 0.44830E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.9943e-13 1.6772e-13 -1.905e-17 -4.7678e-18 v Velocity[Y] -0.00021204 0.00021234 -7.2061e-10 -4.4591e-12 v Velocity[Z] -0.00021235 0.00021204 6.9178e-10 -8.8114e-13 v ǁVelocityǁ 2.2811e-10 0.00025227 1.4379e-05 7.3169e-06 v Pressure -0.00030652 0.010879 0.00048164 2.3998e-20 v k 2.5008e-08 0.0039573 0.0027348 0.0032324 v omega 38.637 1.0313e+05 2684 521.32 v TempK 288 341.2 291.84 289.45 v Density 1.205 1.205 1.205 1.205 v TurbVisc 2.9564e-13 0.00011573 7.7428e-05 9.5762e-05 v CourantNb 7.2936e-10 0.00039523 2.181e-05 1.0694e-05 v FourierNb 0.14762 0.62811 0.23941 0.20197 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.8737 4.8738 0.00034285 -1.9518e-07 v volume_forces[Z] -4.8737 4.8738 -0.00034274 2.4811e-07 v ǁvolume_forcesǁ 8.3126e-09 4.8759 0.34889 0.13099 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.06 289.59 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.021958 7.441e-05 4.235e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14762 0.62811 0.23943 0.20198 INSTANT 0.179118000E+00 TIME STEP NUMBER 186 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.56246E-05 0.32956E-02 Friction velocity uk : 0.57628E-05 0.32953E-02 Dimensionless distance yplus : 0.38377E-04 0.21924E-01 Friction thermal sca. tstar : -0.24807E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.26954E-04 0.15398E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.56246E-05 0.32956E-02 Friction velocity uk : 0.57628E-05 0.32953E-02 Dimensionless distance yplus : 0.38377E-04 0.21924E-01 Friction thermal sca. tstar : -0.24807E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.26954E-04 0.15398E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.50474E-08 4 0.83808E-06 0.45281E-11 0.28029E+01 c Velocity[X] 0.72124E-30 c Velocity[Y] 0.22641E-11 c Velocity[Z] 0.22640E-11 c Pressure 0.76955E-13 25 0.51688E-08 0.61167E-06 0.44664E+01 c k 0.11067E-05 2 0.31321E-06 0.16191E-06 0.39228E+01 c omega 0.13153E+02 1 0.13395E-07 0.12819E+02 0.18639E-01 c TempK 0.94324E+02 1 0.61883E-06 0.16099E+00 0.44658E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.9883e-13 1.672e-13 -1.8992e-17 -4.7539e-18 v Velocity[Y] -0.00021153 0.00021182 -7.2393e-10 -4.4387e-12 v Velocity[Z] -0.00021183 0.00021153 6.9468e-10 -8.7889e-13 v ǁVelocityǁ 2.2629e-10 0.00025157 1.4345e-05 7.3027e-06 v Pressure -0.00030822 0.010909 0.00048358 2.7504e-20 v k 2.4718e-08 0.0039406 0.0027238 0.0032204 v omega 38.519 1.0313e+05 2683.9 521.21 v TempK 288 341.2 291.84 289.45 v Density 1.205 1.205 1.205 1.205 v TurbVisc 2.922e-13 0.00011559 7.7352e-05 9.5693e-05 v CourantNb 7.3347e-10 0.00039428 2.1755e-05 1.0669e-05 v FourierNb 0.1476 0.62811 0.23916 0.2018 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.8741 4.8742 0.00034347 -1.9661e-07 v volume_forces[Z] -4.8741 4.8742 -0.00034336 2.498e-07 v ǁvolume_forcesǁ 8.2462e-09 4.8763 0.34952 0.13135 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.07 289.6 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.021924 7.4304e-05 4.2287e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.1476 0.62811 0.23919 0.20181 INSTANT 0.180081000E+00 TIME STEP NUMBER 187 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.55977E-05 0.32906E-02 Friction velocity uk : 0.57341E-05 0.32903E-02 Dimensionless distance yplus : 0.38187E-04 0.21890E-01 Friction thermal sca. tstar : -0.23074E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.26820E-04 0.15374E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.55977E-05 0.32906E-02 Friction velocity uk : 0.57341E-05 0.32903E-02 Dimensionless distance yplus : 0.38187E-04 0.21890E-01 Friction thermal sca. tstar : -0.23074E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.26820E-04 0.15374E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.50348E-08 4 0.83379E-06 0.45335E-11 0.28115E+01 c Velocity[X] 0.71359E-30 c Velocity[Y] 0.22668E-11 c Velocity[Z] 0.22667E-11 c Pressure 0.76385E-13 25 0.51350E-08 0.60707E-06 0.44425E+01 c k 0.11027E-05 2 0.30985E-06 0.15970E-06 0.39103E+01 c omega 0.13153E+02 1 0.13298E-07 0.12666E+02 0.18528E-01 c TempK 0.94325E+02 1 0.61460E-06 0.15976E+00 0.44488E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.9824e-13 1.6668e-13 -1.8935e-17 -4.74e-18 v Velocity[Y] -0.00021102 0.0002113 -7.2723e-10 -4.4165e-12 v Velocity[Z] -0.0002113 0.00021102 6.9756e-10 -8.7598e-13 v ǁVelocityǁ 2.2447e-10 0.00025088 1.4312e-05 7.2884e-06 v Pressure -0.00030993 0.01094 0.00048552 4.1207e-20 v k 2.4432e-08 0.0039239 0.0027128 0.0032084 v omega 38.402 1.0313e+05 2683.8 521.1 v TempK 288 341.21 291.85 289.45 v Density 1.205 1.205 1.205 1.205 v TurbVisc 2.8881e-13 0.00011546 7.7277e-05 9.5624e-05 v CourantNb 7.3758e-10 0.00039333 2.17e-05 1.0644e-05 v FourierNb 0.14757 0.62811 0.23892 0.20163 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.8745 4.8746 0.00034408 -1.9803e-07 v volume_forces[Z] -4.8745 4.8746 -0.00034398 2.5148e-07 v ǁvolume_forcesǁ 8.1804e-09 4.8767 0.35014 0.13171 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.08 289.6 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.02189 7.4197e-05 4.2225e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14757 0.62811 0.23894 0.20164 INSTANT 0.181044000E+00 TIME STEP NUMBER 188 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.55705E-05 0.32856E-02 Friction velocity uk : 0.57053E-05 0.32852E-02 Dimensionless distance yplus : 0.37995E-04 0.21857E-01 Friction thermal sca. tstar : -0.21657E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.26685E-04 0.15351E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.55705E-05 0.32856E-02 Friction velocity uk : 0.57053E-05 0.32852E-02 Dimensionless distance yplus : 0.37995E-04 0.21857E-01 Friction thermal sca. tstar : -0.21657E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.26685E-04 0.15351E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.50223E-08 4 0.82973E-06 0.45377E-11 0.28197E+01 c Velocity[X] 0.70596E-30 c Velocity[Y] 0.22689E-11 c Velocity[Z] 0.22688E-11 c Pressure 0.75939E-13 25 0.51065E-08 0.60346E-06 0.44188E+01 c k 0.10988E-05 2 0.30655E-06 0.15753E-06 0.38978E+01 c omega 0.13153E+02 1 0.13203E-07 0.12516E+02 0.18418E-01 c TempK 0.94326E+02 1 0.61041E-06 0.15856E+00 0.44319E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.9764e-13 1.6616e-13 -1.8878e-17 -4.7264e-18 v Velocity[Y] -0.00021052 0.00021078 -7.3052e-10 -4.3944e-12 v Velocity[Z] -0.00021078 0.00021052 7.0043e-10 -8.7346e-13 v ǁVelocityǁ 2.2265e-10 0.00025019 1.4279e-05 7.2742e-06 v Pressure -0.00031164 0.01097 0.00048746 2.2062e-21 v k 2.4151e-08 0.0039074 0.0027018 0.0031965 v omega 38.286 1.0313e+05 2683.7 521 v TempK 288 341.21 291.86 289.46 v Density 1.205 1.205 1.205 1.205 v TurbVisc 2.8547e-13 0.00011532 7.7202e-05 9.5556e-05 v CourantNb 7.4169e-10 0.00039238 2.1646e-05 1.0619e-05 v FourierNb 0.14754 0.62811 0.23868 0.20146 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.8749 4.875 0.0003447 -1.9944e-07 v volume_forces[Z] -4.8749 4.875 -0.00034459 2.5314e-07 v ǁvolume_forcesǁ 8.1146e-09 4.8771 0.35076 0.13206 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.08 289.6 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.021857 7.4092e-05 4.2163e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14754 0.62811 0.2387 0.20147 INSTANT 0.182007000E+00 TIME STEP NUMBER 189 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.55430E-05 0.32806E-02 Friction velocity uk : 0.56762E-05 0.32803E-02 Dimensionless distance yplus : 0.37801E-04 0.21824E-01 Friction thermal sca. tstar : -0.20470E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.26549E-04 0.15328E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.55430E-05 0.32806E-02 Friction velocity uk : 0.56762E-05 0.32803E-02 Dimensionless distance yplus : 0.37801E-04 0.21824E-01 Friction thermal sca. tstar : -0.20470E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.26549E-04 0.15328E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.50097E-08 4 0.82552E-06 0.45406E-11 0.28277E+01 c Velocity[X] 0.69832E-30 c Velocity[Y] 0.22704E-11 c Velocity[Z] 0.22703E-11 c Pressure 0.75480E-13 25 0.50782E-08 0.59975E-06 0.43954E+01 c k 0.10949E-05 2 0.30331E-06 0.15540E-06 0.38855E+01 c omega 0.13153E+02 1 0.13108E-07 0.12368E+02 0.18308E-01 c TempK 0.94326E+02 1 0.60628E-06 0.15736E+00 0.44151E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.9706e-13 1.6564e-13 -1.8822e-17 -4.7128e-18 v Velocity[Y] -0.00021001 0.00021026 -7.3379e-10 -4.3725e-12 v Velocity[Z] -0.00021026 0.00021002 7.0327e-10 -8.7123e-13 v ǁVelocityǁ 2.2082e-10 0.0002495 1.4246e-05 7.2599e-06 v Pressure -0.00031335 0.011 0.0004894 -5.1968e-21 v k 2.3874e-08 0.003891 0.002691 0.0031847 v omega 38.17 1.0313e+05 2683.6 520.89 v TempK 288 341.22 291.86 289.46 v Density 1.205 1.205 1.205 1.205 v TurbVisc 2.8219e-13 0.00011519 7.7128e-05 9.5487e-05 v CourantNb 7.4581e-10 0.00039143 2.1591e-05 1.0594e-05 v FourierNb 0.14751 0.62811 0.23844 0.20129 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.8753 4.8753 0.00034531 -2.0085e-07 v volume_forces[Z] -4.8753 4.8753 -0.00034521 2.548e-07 v ǁvolume_forcesǁ 8.0487e-09 4.8775 0.35138 0.13242 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.09 289.61 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.021824 7.3986e-05 4.2101e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14752 0.62811 0.23847 0.2013 INSTANT 0.182970000E+00 TIME STEP NUMBER 190 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.55152E-05 0.32756E-02 Friction velocity uk : 0.56468E-05 0.32753E-02 Dimensionless distance yplus : 0.37605E-04 0.21791E-01 Friction thermal sca. tstar : -0.19458E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.26411E-04 0.15304E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.55152E-05 0.32756E-02 Friction velocity uk : 0.56468E-05 0.32753E-02 Dimensionless distance yplus : 0.37605E-04 0.21791E-01 Friction thermal sca. tstar : -0.19458E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.26411E-04 0.15304E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.49971E-08 4 0.82143E-06 0.45424E-11 0.28352E+01 c Velocity[X] 0.69036E-30 c Velocity[Y] 0.22712E-11 c Velocity[Z] 0.22711E-11 c Pressure 0.74986E-13 24 0.10578E-07 0.59576E-06 0.43723E+01 c k 0.10910E-05 2 0.30012E-06 0.15330E-06 0.38732E+01 c omega 0.13153E+02 1 0.13014E-07 0.12222E+02 0.18200E-01 c TempK 0.94327E+02 1 0.60219E-06 0.15619E+00 0.43985E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.9647e-13 1.6513e-13 -1.8767e-17 -4.6995e-18 v Velocity[Y] -0.00020951 0.00020974 -7.3704e-10 -4.356e-12 v Velocity[Z] -0.00020975 0.00020951 7.061e-10 -8.663e-13 v ǁVelocityǁ 2.1907e-10 0.00024881 1.4213e-05 7.2456e-06 v Pressure -0.00031506 0.01103 0.00049133 4.3462e-20 v k 2.3602e-08 0.0038746 0.0026802 0.003173 v omega 38.056 1.0313e+05 2683.5 520.79 v TempK 288 341.22 291.87 289.47 v Density 1.205 1.205 1.205 1.205 v TurbVisc 2.7895e-13 0.00011505 7.7054e-05 9.5419e-05 v CourantNb 7.4998e-10 0.00039048 2.1537e-05 1.0569e-05 v FourierNb 0.14749 0.62811 0.23821 0.20112 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.8757 4.8757 0.00034592 -2.0225e-07 v volume_forces[Z] -4.8757 4.8757 -0.00034582 2.5645e-07 v ǁvolume_forcesǁ 7.9825e-09 4.8779 0.352 0.13277 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.1 289.61 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.021791 7.3881e-05 4.2039e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14749 0.62811 0.23823 0.20113 INSTANT 0.183933000E+00 TIME STEP NUMBER 191 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.54883E-05 0.32706E-02 Friction velocity uk : 0.56183E-05 0.32703E-02 Dimensionless distance yplus : 0.37415E-04 0.21758E-01 Friction thermal sca. tstar : -0.18580E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.26278E-04 0.15281E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.54883E-05 0.32706E-02 Friction velocity uk : 0.56183E-05 0.32703E-02 Dimensionless distance yplus : 0.37415E-04 0.21758E-01 Friction thermal sca. tstar : -0.18580E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.26278E-04 0.15281E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.49844E-08 4 0.81817E-06 0.45429E-11 0.28425E+01 c Velocity[X] 0.68313E-30 c Velocity[Y] 0.22715E-11 c Velocity[Z] 0.22714E-11 c Pressure 0.74593E-13 24 0.10544E-07 0.59257E-06 0.43493E+01 c k 0.10872E-05 2 0.29699E-06 0.15124E-06 0.38610E+01 c omega 0.13153E+02 1 0.12922E-07 0.12078E+02 0.18092E-01 c TempK 0.94328E+02 1 0.59814E-06 0.15502E+00 0.43821E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.9589e-13 1.6462e-13 -1.8711e-17 -4.6861e-18 v Velocity[Y] -0.00020901 0.00020923 -7.4027e-10 -4.3342e-12 v Velocity[Z] -0.00020923 0.00020901 7.0891e-10 -8.6404e-13 v ǁVelocityǁ 2.1721e-10 0.00024813 1.418e-05 7.2313e-06 v Pressure -0.00031676 0.01106 0.00049325 3.5103e-20 v k 2.3333e-08 0.0038584 0.0026695 0.0031614 v omega 37.942 1.0313e+05 2683.4 520.68 v TempK 288 341.22 291.88 289.47 v Density 1.205 1.205 1.205 1.205 v TurbVisc 2.7577e-13 0.00011491 7.698e-05 9.5352e-05 v CourantNb 7.5409e-10 0.00038952 2.1482e-05 1.0544e-05 v FourierNb 0.14746 0.62811 0.23797 0.20095 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.8761 4.8761 0.00034653 -2.0364e-07 v volume_forces[Z] -4.8761 4.8761 -0.00034643 2.5809e-07 v ǁvolume_forcesǁ 7.9193e-09 4.8783 0.35261 0.13312 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.1 289.62 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.021758 7.3777e-05 4.1978e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14746 0.62811 0.23799 0.20097 INSTANT 0.184896000E+00 TIME STEP NUMBER 192 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.54596E-05 0.32657E-02 Friction velocity uk : 0.55881E-05 0.32654E-02 Dimensionless distance yplus : 0.37214E-04 0.21725E-01 Friction thermal sca. tstar : -0.17810E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.26137E-04 0.15258E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.54596E-05 0.32657E-02 Friction velocity uk : 0.55881E-05 0.32654E-02 Dimensionless distance yplus : 0.37214E-04 0.21725E-01 Friction thermal sca. tstar : -0.17810E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.26137E-04 0.15258E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.49718E-08 4 0.81381E-06 0.45422E-11 0.28494E+01 c Velocity[X] 0.67557E-30 c Velocity[Y] 0.22712E-11 c Velocity[Z] 0.22711E-11 c Pressure 0.74105E-13 24 0.10509E-07 0.58863E-06 0.43266E+01 c k 0.10834E-05 2 0.29391E-06 0.14921E-06 0.38489E+01 c omega 0.13153E+02 1 0.12830E-07 0.11936E+02 0.17986E-01 c TempK 0.94329E+02 1 0.59414E-06 0.15388E+00 0.43657E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.9531e-13 1.6411e-13 -1.8657e-17 -4.6729e-18 v Velocity[Y] -0.00020851 0.00020871 -7.4349e-10 -4.3127e-12 v Velocity[Z] -0.00020872 0.00020851 7.117e-10 -8.621e-13 v ǁVelocityǁ 2.1535e-10 0.00024744 1.4147e-05 7.2169e-06 v Pressure -0.00031847 0.011089 0.00049518 7.2559e-21 v k 2.3069e-08 0.0038423 0.0026589 0.0031498 v omega 37.828 1.0313e+05 2683.4 520.58 v TempK 288 341.23 291.88 289.47 v Density 1.205 1.205 1.205 1.205 v TurbVisc 2.7263e-13 0.00011478 7.6907e-05 9.5284e-05 v CourantNb 7.5821e-10 0.00038857 2.1427e-05 1.052e-05 v FourierNb 0.14743 0.62811 0.23774 0.20079 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.8764 4.8765 0.00034714 -2.0502e-07 v volume_forces[Z] -4.8764 4.8765 -0.00034703 2.5972e-07 v ǁvolume_forcesǁ 7.8523e-09 4.8787 0.35323 0.13347 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.11 289.62 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.021725 7.3673e-05 4.1917e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14743 0.62811 0.23776 0.2008 INSTANT 0.185859000E+00 TIME STEP NUMBER 193 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.54305E-05 0.32608E-02 Friction velocity uk : 0.55576E-05 0.32605E-02 Dimensionless distance yplus : 0.37011E-04 0.21692E-01 Friction thermal sca. tstar : -0.17127E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.25994E-04 0.15235E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.54305E-05 0.32608E-02 Friction velocity uk : 0.55576E-05 0.32605E-02 Dimensionless distance yplus : 0.37011E-04 0.21692E-01 Friction thermal sca. tstar : -0.17127E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.25994E-04 0.15235E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.49592E-08 4 0.80967E-06 0.45404E-11 0.28560E+01 c Velocity[X] 0.66799E-30 c Velocity[Y] 0.22703E-11 c Velocity[Z] 0.22702E-11 c Pressure 0.73718E-13 24 0.10467E-07 0.58550E-06 0.43042E+01 c k 0.10796E-05 2 0.29089E-06 0.14721E-06 0.38369E+01 c omega 0.13153E+02 1 0.12739E-07 0.11796E+02 0.17880E-01 c TempK 0.94329E+02 1 0.59019E-06 0.15274E+00 0.43496E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.9473e-13 1.636e-13 -1.8603e-17 -4.6599e-18 v Velocity[Y] -0.00020801 0.0002082 -7.4666e-10 -4.2714e-12 v Velocity[Z] -0.0002082 0.00020802 7.1456e-10 -7.7027e-13 v ǁVelocityǁ 2.1333e-10 0.00024676 1.4114e-05 7.2026e-06 v Pressure -0.00032018 0.011119 0.0004971 -3.4269e-20 v k 2.2809e-08 0.0038263 0.0026484 0.0031383 v omega 37.715 1.0313e+05 2683.3 520.47 v TempK 288 341.23 291.89 289.48 v Density 1.205 1.205 1.205 1.205 v TurbVisc 2.6954e-13 0.00011464 7.6834e-05 9.5217e-05 v CourantNb 7.623e-10 0.00038762 2.1373e-05 1.0495e-05 v FourierNb 0.14741 0.62811 0.23751 0.20062 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.8768 4.8769 0.00034774 -2.064e-07 v volume_forces[Z] -4.8768 4.8769 -0.00034764 2.6134e-07 v ǁvolume_forcesǁ 7.785e-09 4.879 0.35384 0.13382 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.12 289.62 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.021692 7.3569e-05 4.1856e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14741 0.62811 0.23753 0.20063 INSTANT 0.186822000E+00 TIME STEP NUMBER 194 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.53988E-05 0.32559E-02 Friction velocity uk : 0.55244E-05 0.32556E-02 Dimensionless distance yplus : 0.36790E-04 0.21660E-01 Friction thermal sca. tstar : -0.16516E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.25839E-04 0.15212E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.53988E-05 0.32559E-02 Friction velocity uk : 0.55244E-05 0.32556E-02 Dimensionless distance yplus : 0.36790E-04 0.21660E-01 Friction thermal sca. tstar : -0.16516E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.25839E-04 0.15212E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.49465E-08 4 0.80557E-06 0.45375E-11 0.28622E+01 c Velocity[X] 0.66044E-30 c Velocity[Y] 0.22688E-11 c Velocity[Z] 0.22687E-11 c Pressure 0.73177E-13 24 0.10431E-07 0.58114E-06 0.42819E+01 c k 0.10758E-05 2 0.28792E-06 0.14525E-06 0.38249E+01 c omega 0.13153E+02 1 0.12649E-07 0.11658E+02 0.17776E-01 c TempK 0.94330E+02 1 0.58628E-06 0.15162E+00 0.43335E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.9416e-13 1.631e-13 -1.8549e-17 -4.6469e-18 v Velocity[Y] -0.00020752 0.00020769 -7.4984e-10 -4.2494e-12 v Velocity[Z] -0.00020769 0.00020752 7.1731e-10 -7.6837e-13 v ǁVelocityǁ 2.1152e-10 0.00024608 1.408e-05 7.1883e-06 v Pressure -0.00032189 0.011149 0.00049901 -1.5272e-20 v k 2.2552e-08 0.0038104 0.0026379 0.0031269 v omega 37.603 1.0313e+05 2683.2 520.37 v TempK 288 341.24 291.9 289.48 v Density 1.205 1.205 1.205 1.205 v TurbVisc 2.665e-13 0.00011451 7.6761e-05 9.515e-05 v CourantNb 7.6642e-10 0.00038667 2.1319e-05 1.047e-05 v FourierNb 0.14738 0.62811 0.23727 0.20046 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.8772 4.8773 0.00034835 -2.0777e-07 v volume_forces[Z] -4.8772 4.8773 -0.00034824 2.6296e-07 v ǁvolume_forcesǁ 7.712e-09 4.8794 0.35445 0.13417 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.12 289.63 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.02166 7.3466e-05 4.1796e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14738 0.62811 0.2373 0.20047 INSTANT 0.187785000E+00 TIME STEP NUMBER 195 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.53698E-05 0.32510E-02 Friction velocity uk : 0.54941E-05 0.32507E-02 Dimensionless distance yplus : 0.36588E-04 0.21627E-01 Friction thermal sca. tstar : -0.15966E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.25697E-04 0.15190E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.53698E-05 0.32510E-02 Friction velocity uk : 0.54941E-05 0.32507E-02 Dimensionless distance yplus : 0.36588E-04 0.21627E-01 Friction thermal sca. tstar : -0.15966E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.25697E-04 0.15190E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.49339E-08 4 0.80152E-06 0.45334E-11 0.28682E+01 c Velocity[X] 0.65290E-30 c Velocity[Y] 0.22667E-11 c Velocity[Z] 0.22666E-11 c Pressure 0.72715E-13 24 0.10394E-07 0.57741E-06 0.42599E+01 c k 0.10721E-05 2 0.28499E-06 0.14331E-06 0.38131E+01 c omega 0.13153E+02 1 0.12560E-07 0.11523E+02 0.17672E-01 c TempK 0.94331E+02 1 0.58241E-06 0.15052E+00 0.43176E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.9359e-13 1.626e-13 -1.8496e-17 -4.6341e-18 v Velocity[Y] -0.00020702 0.00020718 -7.5301e-10 -4.2286e-12 v Velocity[Z] -0.00020718 0.00020703 7.2004e-10 -7.6732e-13 v ǁVelocityǁ 2.0967e-10 0.0002454 1.4047e-05 7.1739e-06 v Pressure -0.0003236 0.011178 0.00050092 -5.1968e-21 v k 2.23e-08 0.0037945 0.0026276 0.0031155 v omega 37.492 1.0313e+05 2683.1 520.27 v TempK 288 341.24 291.9 289.49 v Density 1.205 1.205 1.205 1.205 v TurbVisc 2.6351e-13 0.00011437 7.6689e-05 9.5083e-05 v CourantNb 7.7054e-10 0.00038571 2.1264e-05 1.0445e-05 v FourierNb 0.14735 0.62811 0.23705 0.20029 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.8776 4.8776 0.00034895 -2.0913e-07 v volume_forces[Z] -4.8776 4.8776 -0.00034884 2.6456e-07 v ǁvolume_forcesǁ 7.6465e-09 4.8798 0.35505 0.13452 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.13 289.63 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.021627 7.3364e-05 4.1736e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14735 0.62811 0.23707 0.2003 INSTANT 0.188748000E+00 TIME STEP NUMBER 196 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.53400E-05 0.32462E-02 Friction velocity uk : 0.54628E-05 0.32459E-02 Dimensionless distance yplus : 0.36380E-04 0.21595E-01 Friction thermal sca. tstar : -0.15466E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.25551E-04 0.15167E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.53400E-05 0.32462E-02 Friction velocity uk : 0.54628E-05 0.32459E-02 Dimensionless distance yplus : 0.36380E-04 0.21595E-01 Friction thermal sca. tstar : -0.15466E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.25551E-04 0.15167E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.49213E-08 4 0.79755E-06 0.45282E-11 0.28738E+01 c Velocity[X] 0.64540E-30 c Velocity[Y] 0.22641E-11 c Velocity[Z] 0.22641E-11 c Pressure 0.72263E-13 24 0.10358E-07 0.57377E-06 0.42381E+01 c k 0.10683E-05 2 0.28212E-06 0.14141E-06 0.38012E+01 c omega 0.13153E+02 1 0.12472E-07 0.11389E+02 0.17569E-01 c TempK 0.94332E+02 1 0.57859E-06 0.14942E+00 0.43019E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.9302e-13 1.621e-13 -1.8443e-17 -4.6214e-18 v Velocity[Y] -0.00020653 0.00020667 -7.5615e-10 -4.2075e-12 v Velocity[Z] -0.00020667 0.00020653 7.2275e-10 -7.6654e-13 v ǁVelocityǁ 2.0779e-10 0.00024472 1.4015e-05 7.1596e-06 v Pressure -0.00032531 0.011208 0.00050283 -2.0689e-20 v k 2.2051e-08 0.0037788 0.0026172 0.0031043 v omega 37.381 1.0313e+05 2683 520.17 v TempK 288 341.25 291.91 289.49 v Density 1.205 1.205 1.205 1.205 v TurbVisc 2.6056e-13 0.00011424 7.6617e-05 9.5017e-05 v CourantNb 7.7467e-10 0.00038476 2.121e-05 1.042e-05 v FourierNb 0.14732 0.62811 0.23682 0.20013 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.878 4.878 0.00034954 -2.1048e-07 v volume_forces[Z] -4.878 4.878 -0.00034943 2.6616e-07 v ǁvolume_forcesǁ 7.5796e-09 4.8802 0.35565 0.13487 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.14 289.64 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.021595 7.3262e-05 4.1676e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14733 0.62811 0.23684 0.20014 INSTANT 0.189711000E+00 TIME STEP NUMBER 197 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.53095E-05 0.32413E-02 Friction velocity uk : 0.54310E-05 0.32410E-02 Dimensionless distance yplus : 0.36168E-04 0.21563E-01 Friction thermal sca. tstar : -0.15396E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.25402E-04 0.15144E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.53095E-05 0.32413E-02 Friction velocity uk : 0.54310E-05 0.32410E-02 Dimensionless distance yplus : 0.36168E-04 0.21563E-01 Friction thermal sca. tstar : -0.15396E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.25402E-04 0.15144E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.49087E-08 4 0.79356E-06 0.45220E-11 0.28790E+01 c Velocity[X] 0.63793E-30 c Velocity[Y] 0.22610E-11 c Velocity[Z] 0.22609E-11 c Pressure 0.71869E-13 24 0.10320E-07 0.57058E-06 0.42165E+01 c k 0.10646E-05 2 0.27930E-06 0.13955E-06 0.37895E+01 c omega 0.13153E+02 1 0.12385E-07 0.11257E+02 0.17467E-01 c TempK 0.94332E+02 1 0.57480E-06 0.14834E+00 0.42862E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.9246e-13 1.616e-13 -1.8391e-17 -4.6088e-18 v Velocity[Y] -0.00020604 0.00020616 -7.5928e-10 -4.1874e-12 v Velocity[Z] -0.00020616 0.00020604 7.2545e-10 -7.6505e-13 v ǁVelocityǁ 2.059e-10 0.00024404 1.3982e-05 7.1453e-06 v Pressure -0.00032702 0.011237 0.00050474 -3.2382e-20 v k 2.1807e-08 0.0037632 0.002607 0.0030931 v omega 37.271 1.0313e+05 2682.9 520.07 v TempK 288 341.25 291.92 289.49 v Density 1.205 1.205 1.205 1.205 v TurbVisc 2.5766e-13 0.0001141 7.6545e-05 9.495e-05 v CourantNb 7.7879e-10 0.00038381 2.1156e-05 1.0395e-05 v FourierNb 0.1473 0.62811 0.23659 0.19997 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.8783 4.8784 0.00035014 -2.1183e-07 v volume_forces[Z] -4.8783 4.8784 -0.00035003 2.6774e-07 v ǁvolume_forcesǁ 7.5118e-09 4.8805 0.35626 0.13522 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.14 289.64 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.021563 7.316e-05 4.1616e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.1473 0.62811 0.23661 0.19998 INSTANT 0.190674000E+00 TIME STEP NUMBER 198 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.52784E-05 0.32365E-02 Friction velocity uk : 0.53986E-05 0.32362E-02 Dimensionless distance yplus : 0.35952E-04 0.21531E-01 Friction thermal sca. tstar : -0.15328E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.25251E-04 0.15122E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.52784E-05 0.32365E-02 Friction velocity uk : 0.53986E-05 0.32362E-02 Dimensionless distance yplus : 0.35952E-04 0.21531E-01 Friction thermal sca. tstar : -0.15328E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.25251E-04 0.15122E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.48960E-08 4 0.79262E-06 0.45147E-11 0.28840E+01 c Velocity[X] 0.63049E-30 c Velocity[Y] 0.22574E-11 c Velocity[Z] 0.22573E-11 c Pressure 0.71340E-13 24 0.10276E-07 0.56632E-06 0.41951E+01 c k 0.10610E-05 2 0.27652E-06 0.13771E-06 0.37779E+01 c omega 0.13153E+02 1 0.12298E-07 0.11127E+02 0.17365E-01 c TempK 0.94333E+02 1 0.57106E-06 0.14728E+00 0.42707E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.919e-13 1.611e-13 -1.834e-17 -4.5964e-18 v Velocity[Y] -0.00020555 0.00020565 -7.6239e-10 -4.1663e-12 v Velocity[Z] -0.00020566 0.00020556 7.2812e-10 -7.641e-13 v ǁVelocityǁ 2.04e-10 0.00024337 1.3949e-05 7.131e-06 v Pressure -0.00032874 0.011266 0.00050664 2.6965e-21 v k 2.1565e-08 0.0037477 0.0025968 0.003082 v omega 37.162 1.0313e+05 2682.8 519.97 v TempK 288 341.25 291.92 289.5 v Density 1.205 1.205 1.205 1.205 v TurbVisc 2.5479e-13 0.00011397 7.6474e-05 9.4885e-05 v CourantNb 7.8292e-10 0.00038286 2.1102e-05 1.037e-05 v FourierNb 0.14727 0.62811 0.23637 0.19981 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.8787 4.8788 0.00035073 -2.1317e-07 v volume_forces[Z] -4.8787 4.8788 -0.00035062 2.6932e-07 v ǁvolume_forcesǁ 7.4434e-09 4.8809 0.35686 0.13556 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.15 289.64 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.021531 7.3059e-05 4.1557e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14727 0.62811 0.23639 0.19982 INSTANT 0.191637000E+00 TIME STEP NUMBER 199 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.52467E-05 0.32317E-02 Friction velocity uk : 0.53657E-05 0.32314E-02 Dimensionless distance yplus : 0.35733E-04 0.21499E-01 Friction thermal sca. tstar : -0.15262E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.25097E-04 0.15099E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.52467E-05 0.32317E-02 Friction velocity uk : 0.53657E-05 0.32314E-02 Dimensionless distance yplus : 0.35733E-04 0.21499E-01 Friction thermal sca. tstar : -0.15262E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.25097E-04 0.15099E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.48834E-08 4 0.78560E-06 0.45063E-11 0.28886E+01 c Velocity[X] 0.62309E-30 c Velocity[Y] 0.22532E-11 c Velocity[Z] 0.22531E-11 c Pressure 0.70893E-13 24 0.10236E-07 0.56272E-06 0.41739E+01 c k 0.10573E-05 2 0.27379E-06 0.13590E-06 0.37663E+01 c omega 0.13153E+02 1 0.12212E-07 0.10998E+02 0.17265E-01 c TempK 0.94334E+02 1 0.56736E-06 0.14622E+00 0.42554E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.9134e-13 1.6061e-13 -1.8288e-17 -4.584e-18 v Velocity[Y] -0.00020507 0.00020515 -7.6549e-10 -4.1456e-12 v Velocity[Z] -0.00020516 0.00020507 7.3078e-10 -7.634e-13 v ǁVelocityǁ 2.0209e-10 0.0002427 1.3916e-05 7.1167e-06 v Pressure -0.00033045 0.011296 0.00050854 5.638e-21 v k 2.1328e-08 0.0037323 0.0025868 0.0030709 v omega 37.053 1.0313e+05 2682.8 519.87 v TempK 288 341.26 291.93 289.5 v Density 1.205 1.205 1.205 1.205 v TurbVisc 2.5198e-13 0.00011383 7.6403e-05 9.4819e-05 v CourantNb 7.8704e-10 0.00038191 2.1048e-05 1.0345e-05 v FourierNb 0.14724 0.62811 0.23614 0.19965 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.8791 4.8791 0.00035132 -2.1451e-07 v volume_forces[Z] -4.8791 4.8791 -0.00035121 2.7089e-07 v ǁvolume_forcesǁ 7.3746e-09 4.8812 0.35745 0.13591 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.16 289.65 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.021499 7.2958e-05 4.1498e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14725 0.62811 0.23616 0.19966 INSTANT 0.192600000E+00 TIME STEP NUMBER 200 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.52146E-05 0.32270E-02 Friction velocity uk : 0.53324E-05 0.32267E-02 Dimensionless distance yplus : 0.35511E-04 0.21467E-01 Friction thermal sca. tstar : -0.15197E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.24941E-04 0.15077E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.52146E-05 0.32270E-02 Friction velocity uk : 0.53324E-05 0.32267E-02 Dimensionless distance yplus : 0.35511E-04 0.21467E-01 Friction thermal sca. tstar : -0.15197E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.24941E-04 0.15077E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.48708E-08 4 0.78160E-06 0.44969E-11 0.28929E+01 c Velocity[X] 0.61573E-30 c Velocity[Y] 0.22485E-11 c Velocity[Z] 0.22484E-11 c Pressure 0.70431E-13 24 0.10193E-07 0.55899E-06 0.41529E+01 c k 0.10537E-05 2 0.27111E-06 0.13412E-06 0.37547E+01 c omega 0.13153E+02 1 0.12128E-07 0.10872E+02 0.17166E-01 c TempK 0.94335E+02 1 0.56370E-06 0.14518E+00 0.42401E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.9079e-13 1.6012e-13 -1.8238e-17 -4.5718e-18 v Velocity[Y] -0.00020458 0.00020465 -7.6856e-10 -4.1254e-12 v Velocity[Z] -0.00020465 0.00020459 7.3342e-10 -7.6261e-13 v ǁVelocityǁ 2.0016e-10 0.00024203 1.3883e-05 7.1024e-06 v Pressure -0.00033216 0.011325 0.00051043 -6.545e-21 v k 2.1094e-08 0.003717 0.0025767 0.00306 v omega 36.945 1.0313e+05 2682.7 519.77 v TempK 288 341.26 291.94 289.51 v Density 1.205 1.205 1.205 1.205 v TurbVisc 2.492e-13 0.0001137 7.6333e-05 9.4753e-05 v CourantNb 7.9117e-10 0.00038096 2.0994e-05 1.032e-05 v FourierNb 0.14722 0.62811 0.23592 0.19949 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.8794 4.8795 0.00035191 -2.1584e-07 v volume_forces[Z] -4.8794 4.8795 -0.0003518 2.7245e-07 v ǁvolume_forcesǁ 7.3054e-09 4.8816 0.35805 0.13626 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.16 289.65 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.021467 7.2858e-05 4.1439e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14722 0.62811 0.23594 0.1995 INSTANT 0.193563000E+00 TIME STEP NUMBER 201 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.51819E-05 0.32222E-02 Friction velocity uk : 0.52985E-05 0.32219E-02 Dimensionless distance yplus : 0.35286E-04 0.21436E-01 Friction thermal sca. tstar : -0.15132E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.24783E-04 0.15055E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.51819E-05 0.32222E-02 Friction velocity uk : 0.52985E-05 0.32219E-02 Dimensionless distance yplus : 0.35286E-04 0.21436E-01 Friction thermal sca. tstar : -0.15132E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.24783E-04 0.15055E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.48583E-08 4 0.77771E-06 0.44866E-11 0.28969E+01 c Velocity[X] 0.60839E-30 c Velocity[Y] 0.22433E-11 c Velocity[Z] 0.22433E-11 c Pressure 0.70057E-13 24 0.10153E-07 0.55597E-06 0.41321E+01 c k 0.10501E-05 2 0.26847E-06 0.13237E-06 0.37433E+01 c omega 0.13153E+02 1 0.12044E-07 0.10747E+02 0.17067E-01 c TempK 0.94336E+02 1 0.56008E-06 0.14415E+00 0.42250E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.9023e-13 1.5963e-13 -1.8187e-17 -4.5597e-18 v Velocity[Y] -0.0002041 0.00020415 -7.7162e-10 -4.1051e-12 v Velocity[Z] -0.00020415 0.0002041 7.3604e-10 -7.6178e-13 v ǁVelocityǁ 1.9824e-10 0.00024136 1.3851e-05 7.0882e-06 v Pressure -0.00033387 0.011354 0.00051233 -6.8956e-20 v k 2.0863e-08 0.0037018 0.0025668 0.0030491 v omega 36.837 1.0313e+05 2682.6 519.67 v TempK 288 341.27 291.94 289.51 v Density 1.205 1.205 1.205 1.205 v TurbVisc 2.4646e-13 0.00011357 7.6262e-05 9.4688e-05 v CourantNb 7.953e-10 0.00038002 2.094e-05 1.0296e-05 v FourierNb 0.14719 0.62811 0.2357 0.19933 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.8798 4.8799 0.0003525 -2.1716e-07 v volume_forces[Z] -4.8798 4.8799 -0.00035239 2.7401e-07 v ǁvolume_forcesǁ 7.236e-09 4.882 0.35864 0.1366 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.17 289.66 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.021436 7.2759e-05 4.138e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14719 0.62811 0.23572 0.19934 INSTANT 0.194526000E+00 TIME STEP NUMBER 202 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.51488E-05 0.32175E-02 Friction velocity uk : 0.52642E-05 0.32172E-02 Dimensionless distance yplus : 0.35058E-04 0.21404E-01 Friction thermal sca. tstar : -0.15069E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.24622E-04 0.15033E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.51488E-05 0.32175E-02 Friction velocity uk : 0.52642E-05 0.32172E-02 Dimensionless distance yplus : 0.35058E-04 0.21404E-01 Friction thermal sca. tstar : -0.15069E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.24622E-04 0.15033E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.48457E-08 4 0.77378E-06 0.44753E-11 0.29006E+01 c Velocity[X] 0.60111E-30 c Velocity[Y] 0.22377E-11 c Velocity[Z] 0.22376E-11 c Pressure 0.69543E-13 24 0.10109E-07 0.55184E-06 0.41116E+01 c k 0.10465E-05 2 0.26587E-06 0.13065E-06 0.37319E+01 c omega 0.13153E+02 1 0.11961E-07 0.10625E+02 0.16969E-01 c TempK 0.94336E+02 1 0.55649E-06 0.14313E+00 0.42100E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.8969e-13 1.5915e-13 -1.8138e-17 -4.5476e-18 v Velocity[Y] -0.00020362 0.00020365 -7.7466e-10 -4.0849e-12 v Velocity[Z] -0.00020366 0.00020362 7.3864e-10 -7.6145e-13 v ǁVelocityǁ 1.963e-10 0.00024069 1.3818e-05 7.0739e-06 v Pressure -0.00033558 0.011383 0.00051421 -2.14e-20 v k 2.0636e-08 0.0036867 0.0025569 0.0030382 v omega 36.73 1.0313e+05 2682.5 519.57 v TempK 288 341.27 291.95 289.51 v Density 1.205 1.205 1.205 1.205 v TurbVisc 2.4377e-13 0.00011343 7.6193e-05 9.4623e-05 v CourantNb 7.9944e-10 0.00037907 2.0887e-05 1.0271e-05 v FourierNb 0.14716 0.62811 0.23548 0.19917 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.8801 4.8802 0.00035308 -2.1847e-07 v volume_forces[Z] -4.8801 4.8802 -0.00035297 2.7555e-07 v ǁvolume_forcesǁ 7.1663e-09 4.8823 0.35923 0.13694 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.18 289.66 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.021404 7.266e-05 4.1322e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14717 0.62811 0.2355 0.19918 INSTANT 0.195489000E+00 TIME STEP NUMBER 203 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.51151E-05 0.32128E-02 Friction velocity uk : 0.52294E-05 0.32125E-02 Dimensionless distance yplus : 0.34826E-04 0.21373E-01 Friction thermal sca. tstar : -0.15007E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.24459E-04 0.15011E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.51151E-05 0.32128E-02 Friction velocity uk : 0.52294E-05 0.32125E-02 Dimensionless distance yplus : 0.34826E-04 0.21373E-01 Friction thermal sca. tstar : -0.15007E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.24459E-04 0.15011E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.48332E-08 4 0.76993E-06 0.44631E-11 0.29040E+01 c Velocity[X] 0.59388E-30 c Velocity[Y] 0.22316E-11 c Velocity[Z] 0.22315E-11 c Pressure 0.69212E-13 23 0.10071E-07 0.54916E-06 0.40912E+01 c k 0.10429E-05 2 0.26332E-06 0.12895E-06 0.37206E+01 c omega 0.13153E+02 1 0.11878E-07 0.10503E+02 0.16872E-01 c TempK 0.94337E+02 1 0.55295E-06 0.14213E+00 0.41952E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.8914e-13 1.5866e-13 -1.8088e-17 -4.5357e-18 v Velocity[Y] -0.00020314 0.00020316 -7.7799e-10 -4.3501e-12 v Velocity[Z] -0.00020316 0.00020314 7.4112e-10 -8.5679e-13 v ǁVelocityǁ 1.9443e-10 0.00024003 1.3786e-05 7.0597e-06 v Pressure -0.00033729 0.011412 0.0005161 -1.2698e-20 v k 2.0412e-08 0.0036717 0.0025471 0.0030275 v omega 36.624 1.0313e+05 2682.4 519.47 v TempK 288 341.27 291.96 289.52 v Density 1.205 1.205 1.205 1.205 v TurbVisc 2.4111e-13 0.0001133 7.6123e-05 9.4558e-05 v CourantNb 8.0355e-10 0.00037813 2.0833e-05 1.0246e-05 v FourierNb 0.14714 0.62811 0.23527 0.19902 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.8805 4.8806 0.00035367 -2.1978e-07 v volume_forces[Z] -4.8805 4.8806 -0.00035356 2.7709e-07 v ǁvolume_forcesǁ 7.0962e-09 4.8827 0.35982 0.13728 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.18 289.66 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.021373 7.2561e-05 4.1264e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14714 0.62811 0.23529 0.19903 INSTANT 0.196452000E+00 TIME STEP NUMBER 204 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.50820E-05 0.32081E-02 Friction velocity uk : 0.51953E-05 0.32078E-02 Dimensionless distance yplus : 0.34598E-04 0.21342E-01 Friction thermal sca. tstar : -0.14946E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.24300E-04 0.14989E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.50820E-05 0.32081E-02 Friction velocity uk : 0.51953E-05 0.32078E-02 Dimensionless distance yplus : 0.34598E-04 0.21342E-01 Friction thermal sca. tstar : -0.14946E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.24300E-04 0.14989E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.48206E-08 4 0.76601E-06 0.44499E-11 0.29071E+01 c Velocity[X] 0.58667E-30 c Velocity[Y] 0.22250E-11 c Velocity[Z] 0.22249E-11 c Pressure 0.68610E-13 23 0.10024E-07 0.54433E-06 0.40710E+01 c k 0.10394E-05 2 0.26081E-06 0.12728E-06 0.37094E+01 c omega 0.13153E+02 1 0.11797E-07 0.10384E+02 0.16776E-01 c TempK 0.94338E+02 1 0.54944E-06 0.14114E+00 0.41804E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.886e-13 1.5818e-13 -1.8039e-17 -4.5239e-18 v Velocity[Y] -0.00020266 0.00020266 -7.8099e-10 -4.3305e-12 v Velocity[Z] -0.00020267 0.00020267 7.4369e-10 -8.5458e-13 v ǁVelocityǁ 1.923e-10 0.00023937 1.3753e-05 7.0456e-06 v Pressure -0.000339 0.011441 0.00051798 3.1254e-20 v k 2.0191e-08 0.0036568 0.0025373 0.0030168 v omega 36.518 1.0313e+05 2682.4 519.38 v TempK 288 341.28 291.96 289.52 v Density 1.205 1.205 1.205 1.205 v TurbVisc 2.385e-13 0.00011317 7.6054e-05 9.4494e-05 v CourantNb 8.077e-10 0.00037719 2.078e-05 1.0222e-05 v FourierNb 0.14711 0.62811 0.23505 0.19886 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.8809 4.8809 0.00035425 -2.2109e-07 v volume_forces[Z] -4.8809 4.8809 -0.00035414 2.7863e-07 v ǁvolume_forcesǁ 7.0287e-09 4.883 0.3604 0.13763 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.19 289.67 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.021342 7.2463e-05 4.1207e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14711 0.62811 0.23507 0.19887 INSTANT 0.197415000E+00 TIME STEP NUMBER 205 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.50443E-05 0.32034E-02 Friction velocity uk : 0.51565E-05 0.32032E-02 Dimensionless distance yplus : 0.34340E-04 0.21311E-01 Friction thermal sca. tstar : -0.14885E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.24118E-04 0.14967E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.50443E-05 0.32034E-02 Friction velocity uk : 0.51565E-05 0.32032E-02 Dimensionless distance yplus : 0.34340E-04 0.21311E-01 Friction thermal sca. tstar : -0.14885E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.24118E-04 0.14967E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.48081E-08 4 0.76218E-06 0.44358E-11 0.29099E+01 c Velocity[X] 0.57950E-30 c Velocity[Y] 0.22179E-11 c Velocity[Z] 0.22179E-11 c Pressure 0.68165E-13 23 0.99789E-08 0.54075E-06 0.40510E+01 c k 0.10359E-05 2 0.25834E-06 0.12564E-06 0.36982E+01 c omega 0.13153E+02 1 0.11716E-07 0.10266E+02 0.16680E-01 c TempK 0.94339E+02 1 0.54597E-06 0.14015E+00 0.41658E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.8806e-13 1.577e-13 -1.7991e-17 -4.5122e-18 v Velocity[Y] -0.00020219 0.00020217 -7.8397e-10 -4.3075e-12 v Velocity[Z] -0.00020218 0.00020219 7.4624e-10 -8.5443e-13 v ǁVelocityǁ 1.9025e-10 0.00023871 1.3721e-05 7.0314e-06 v Pressure -0.00034072 0.01147 0.00051986 1.1325e-20 v k 1.9974e-08 0.0036419 0.0025277 0.0030061 v omega 36.413 1.0313e+05 2682.3 519.28 v TempK 288 341.28 291.97 289.52 v Density 1.205 1.205 1.205 1.205 v TurbVisc 2.3592e-13 0.00011303 7.5985e-05 9.443e-05 v CourantNb 8.1185e-10 0.00037624 2.0727e-05 1.0197e-05 v FourierNb 0.14708 0.62811 0.23483 0.1987 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.8812 4.8813 0.00035483 -2.2238e-07 v volume_forces[Z] -4.8812 4.8813 -0.00035471 2.8015e-07 v ǁvolume_forcesǁ 6.9517e-09 4.8834 0.36099 0.13797 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.2 289.67 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.021311 7.2365e-05 4.115e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14709 0.62811 0.23485 0.19871 INSTANT 0.198378000E+00 TIME STEP NUMBER 206 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.50073E-05 0.31988E-02 Friction velocity uk : 0.51186E-05 0.31985E-02 Dimensionless distance yplus : 0.34087E-04 0.21280E-01 Friction thermal sca. tstar : -0.14826E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.23941E-04 0.14946E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.50073E-05 0.31988E-02 Friction velocity uk : 0.51186E-05 0.31985E-02 Dimensionless distance yplus : 0.34087E-04 0.21280E-01 Friction thermal sca. tstar : -0.14826E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.23941E-04 0.14946E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.47957E-08 4 0.75832E-06 0.44208E-11 0.29123E+01 c Velocity[X] 0.57238E-30 c Velocity[Y] 0.22105E-11 c Velocity[Z] 0.22104E-11 c Pressure 0.67732E-13 23 0.99332E-08 0.53725E-06 0.40312E+01 c k 0.10324E-05 2 0.25591E-06 0.12402E-06 0.36871E+01 c omega 0.13153E+02 1 0.11636E-07 0.10150E+02 0.16586E-01 c TempK 0.94339E+02 1 0.54254E-06 0.13918E+00 0.41513E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.8752e-13 1.5723e-13 -1.7943e-17 -4.5006e-18 v Velocity[Y] -0.00020172 0.00020168 -7.8694e-10 -4.286e-12 v Velocity[Z] -0.00020169 0.00020172 7.4876e-10 -8.5362e-13 v ǁVelocityǁ 1.8824e-10 0.00023805 1.3689e-05 7.0173e-06 v Pressure -0.00034243 0.011499 0.00052173 -1.336e-20 v k 1.9759e-08 0.0036272 0.002518 0.0029956 v omega 36.309 1.0313e+05 2682.2 519.18 v TempK 288 341.28 291.98 289.53 v Density 1.205 1.205 1.205 1.205 v TurbVisc 2.3338e-13 0.0001129 7.5916e-05 9.4365e-05 v CourantNb 8.1599e-10 0.00037531 2.0674e-05 1.0172e-05 v FourierNb 0.14706 0.62811 0.23462 0.19855 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.8816 4.8816 0.0003554 -2.2367e-07 v volume_forces[Z] -4.8816 4.8816 -0.00035529 2.8166e-07 v ǁvolume_forcesǁ 6.8776e-09 4.8837 0.36157 0.13831 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.2 289.67 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.02128 7.2268e-05 4.1093e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14706 0.62811 0.23464 0.19856 INSTANT 0.199341000E+00 TIME STEP NUMBER 207 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.49705E-05 0.31942E-02 Friction velocity uk : 0.50808E-05 0.31939E-02 Dimensionless distance yplus : 0.33836E-04 0.21249E-01 Friction thermal sca. tstar : -0.14767E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.23764E-04 0.14924E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.49705E-05 0.31942E-02 Friction velocity uk : 0.50808E-05 0.31939E-02 Dimensionless distance yplus : 0.33836E-04 0.21249E-01 Friction thermal sca. tstar : -0.14767E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.23764E-04 0.14924E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.47832E-08 4 0.75450E-06 0.44051E-11 0.29145E+01 c Velocity[X] 0.56531E-30 c Velocity[Y] 0.22026E-11 c Velocity[Z] 0.22025E-11 c Pressure 0.67284E-13 23 0.98854E-08 0.53365E-06 0.40116E+01 c k 0.10289E-05 2 0.25351E-06 0.12243E-06 0.36761E+01 c omega 0.13153E+02 1 0.11557E-07 0.10035E+02 0.16492E-01 c TempK 0.94340E+02 1 0.53914E-06 0.13822E+00 0.41369E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.8699e-13 1.5676e-13 -1.7895e-17 -4.4892e-18 v Velocity[Y] -0.00020125 0.00020119 -7.8989e-10 -4.2647e-12 v Velocity[Z] -0.0002012 0.00020125 7.5127e-10 -8.5317e-13 v ǁVelocityǁ 1.8625e-10 0.0002374 1.3656e-05 7.0032e-06 v Pressure -0.00034414 0.011527 0.0005236 -1.1276e-21 v k 1.9548e-08 0.0036126 0.0025085 0.0029851 v omega 36.205 1.0313e+05 2682.1 519.09 v TempK 288 341.29 291.98 289.53 v Density 1.205 1.205 1.205 1.205 v TurbVisc 2.3087e-13 0.00011276 7.5848e-05 9.4302e-05 v CourantNb 8.2013e-10 0.00037437 2.0621e-05 1.0148e-05 v FourierNb 0.14703 0.62811 0.23441 0.19839 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.8819 4.882 0.00035598 -2.2495e-07 v volume_forces[Z] -4.8819 4.882 -0.00035586 2.8317e-07 v ǁvolume_forcesǁ 6.8049e-09 4.8841 0.36215 0.13865 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.21 289.68 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.021249 7.2172e-05 4.1036e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14703 0.62811 0.23443 0.19841 INSTANT 0.200304000E+00 TIME STEP NUMBER 208 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.49335E-05 0.31896E-02 Friction velocity uk : 0.50429E-05 0.31893E-02 Dimensionless distance yplus : 0.33583E-04 0.21219E-01 Friction thermal sca. tstar : -0.14710E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.23587E-04 0.14903E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.49335E-05 0.31896E-02 Friction velocity uk : 0.50429E-05 0.31893E-02 Dimensionless distance yplus : 0.33583E-04 0.21219E-01 Friction thermal sca. tstar : -0.14710E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.23587E-04 0.14903E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.47708E-08 4 0.75275E-06 0.43885E-11 0.29164E+01 c Velocity[X] 0.55829E-30 c Velocity[Y] 0.21943E-11 c Velocity[Z] 0.21942E-11 c Pressure 0.66976E-13 23 0.98431E-08 0.53116E-06 0.39921E+01 c k 0.10255E-05 2 0.25116E-06 0.12087E-06 0.36651E+01 c omega 0.13153E+02 1 0.11478E-07 0.99225E+01 0.16399E-01 c TempK 0.94341E+02 1 0.53578E-06 0.13727E+00 0.41226E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.8646e-13 1.5628e-13 -1.7848e-17 -4.4778e-18 v Velocity[Y] -0.00020078 0.00020071 -7.9283e-10 -4.2436e-12 v Velocity[Z] -0.00020071 0.00020078 7.5377e-10 -8.5198e-13 v ǁVelocityǁ 1.8426e-10 0.00023675 1.3624e-05 6.9892e-06 v Pressure -0.00034585 0.011556 0.00052547 -4.6943e-20 v k 1.934e-08 0.003598 0.002499 0.0029747 v omega 36.101 1.0313e+05 2682 518.99 v TempK 288 341.29 291.99 289.54 v Density 1.205 1.205 1.205 1.205 v TurbVisc 2.284e-13 0.00011263 7.578e-05 9.4238e-05 v CourantNb 8.2427e-10 0.00037343 2.0568e-05 1.0124e-05 v FourierNb 0.147 0.62811 0.2342 0.19824 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.8822 4.8823 0.00035655 -2.2623e-07 v volume_forces[Z] -4.8822 4.8823 -0.00035644 2.8466e-07 v ǁvolume_forcesǁ 6.7328e-09 4.8844 0.36273 0.13899 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.22 289.68 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.021219 7.2076e-05 4.0979e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.147 0.62811 0.23422 0.19825 INSTANT 0.201267000E+00 TIME STEP NUMBER 209 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.48961E-05 0.31850E-02 Friction velocity uk : 0.50046E-05 0.31847E-02 Dimensionless distance yplus : 0.33328E-04 0.21188E-01 Friction thermal sca. tstar : -0.14653E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.23408E-04 0.14881E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.48961E-05 0.31850E-02 Friction velocity uk : 0.50046E-05 0.31847E-02 Dimensionless distance yplus : 0.33328E-04 0.21188E-01 Friction thermal sca. tstar : -0.14653E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.23408E-04 0.14881E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.47584E-08 4 0.74692E-06 0.43710E-11 0.29180E+01 c Velocity[X] 0.55133E-30 c Velocity[Y] 0.21856E-11 c Velocity[Z] 0.21855E-11 c Pressure 0.66391E-13 23 0.97905E-08 0.52647E-06 0.39729E+01 c k 0.10220E-05 2 0.24884E-06 0.11933E-06 0.36542E+01 c omega 0.13153E+02 1 0.11400E-07 0.98111E+01 0.16306E-01 c TempK 0.94342E+02 1 0.53245E-06 0.13634E+00 0.41084E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.8593e-13 1.5582e-13 -1.7801e-17 -4.4665e-18 v Velocity[Y] -0.00020032 0.00020022 -7.9574e-10 -4.2226e-12 v Velocity[Z] -0.00020023 0.00020032 7.5624e-10 -8.5223e-13 v ǁVelocityǁ 1.8228e-10 0.0002361 1.3593e-05 6.9752e-06 v Pressure -0.00034757 0.011584 0.00052734 3.9295e-20 v k 1.9135e-08 0.0035836 0.0024896 0.0029643 v omega 35.999 1.0313e+05 2682 518.9 v TempK 288 341.3 292 289.54 v Density 1.205 1.205 1.205 1.205 v TurbVisc 2.2597e-13 0.0001125 7.5712e-05 9.4175e-05 v CourantNb 8.2842e-10 0.0003725 2.0515e-05 1.0099e-05 v FourierNb 0.14698 0.62811 0.23399 0.19809 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.8826 4.8827 0.00035712 -2.275e-07 v volume_forces[Z] -4.8826 4.8827 -0.00035701 2.8615e-07 v ǁvolume_forcesǁ 6.6611e-09 4.8847 0.3633 0.13932 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.22 289.69 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.021188 7.198e-05 4.0923e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14698 0.62811 0.23401 0.1981 INSTANT 0.202230000E+00 TIME STEP NUMBER 210 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.48583E-05 0.31805E-02 Friction velocity uk : 0.49659E-05 0.31802E-02 Dimensionless distance yplus : 0.33071E-04 0.21158E-01 Friction thermal sca. tstar : -0.14597E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.23227E-04 0.14860E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.48583E-05 0.31805E-02 Friction velocity uk : 0.49659E-05 0.31802E-02 Dimensionless distance yplus : 0.33071E-04 0.21158E-01 Friction thermal sca. tstar : -0.14597E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.23227E-04 0.14860E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.47460E-08 4 0.74314E-06 0.43528E-11 0.29193E+01 c Velocity[X] 0.54441E-30 c Velocity[Y] 0.21765E-11 c Velocity[Z] 0.21764E-11 c Pressure 0.65950E-13 23 0.97427E-08 0.52293E-06 0.39538E+01 c k 0.10186E-05 2 0.24657E-06 0.11781E-06 0.36434E+01 c omega 0.13153E+02 1 0.11323E-07 0.97012E+01 0.16215E-01 c TempK 0.94342E+02 1 0.52915E-06 0.13541E+00 0.40944E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.8541e-13 1.5535e-13 -1.7755e-17 -4.4553e-18 v Velocity[Y] -0.00019985 0.00019974 -7.9864e-10 -4.2018e-12 v Velocity[Z] -0.00019975 0.00019986 7.5869e-10 -8.5196e-13 v ǁVelocityǁ 1.8031e-10 0.00023545 1.3561e-05 6.9613e-06 v Pressure -0.00034928 0.011613 0.0005292 -6.4543e-20 v k 1.8932e-08 0.0035692 0.0024802 0.002954 v omega 35.897 1.0313e+05 2681.9 518.81 v TempK 288 341.3 292 289.54 v Density 1.205 1.205 1.205 1.205 v TurbVisc 2.2357e-13 0.00011237 7.5645e-05 9.4112e-05 v CourantNb 8.3256e-10 0.00037157 2.0463e-05 1.0075e-05 v FourierNb 0.14695 0.62811 0.23378 0.19794 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.8829 4.883 0.00035769 -2.2876e-07 v volume_forces[Z] -4.8829 4.883 -0.00035757 2.8763e-07 v ǁvolume_forcesǁ 6.5896e-09 4.8851 0.36388 0.13966 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.23 289.69 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.021158 7.1885e-05 4.0868e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14695 0.62811 0.2338 0.19795 INSTANT 0.203193000E+00 TIME STEP NUMBER 211 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.48200E-05 0.31759E-02 Friction velocity uk : 0.49267E-05 0.31757E-02 Dimensionless distance yplus : 0.32810E-04 0.21128E-01 Friction thermal sca. tstar : -0.14541E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.23043E-04 0.14839E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.48200E-05 0.31759E-02 Friction velocity uk : 0.49267E-05 0.31757E-02 Dimensionless distance yplus : 0.32810E-04 0.21128E-01 Friction thermal sca. tstar : -0.14541E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.23043E-04 0.14839E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.47337E-08 4 0.75414E-06 0.43339E-11 0.29204E+01 c Velocity[X] 0.53754E-30 c Velocity[Y] 0.21670E-11 c Velocity[Z] 0.21669E-11 c Pressure 0.65544E-13 23 0.96948E-08 0.51965E-06 0.39349E+01 c k 0.10152E-05 2 0.24432E-06 0.11632E-06 0.36326E+01 c omega 0.13153E+02 1 0.11247E-07 0.95929E+01 0.16124E-01 c TempK 0.94343E+02 1 0.52590E-06 0.13449E+00 0.40805E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.8489e-13 1.5489e-13 -1.7709e-17 -4.4443e-18 v Velocity[Y] -0.00019939 0.00019926 -8.0153e-10 -4.1811e-12 v Velocity[Z] -0.00019927 0.00019939 7.6113e-10 -8.5153e-13 v ǁVelocityǁ 1.7834e-10 0.00023481 1.3529e-05 6.9474e-06 v Pressure -0.00035099 0.011641 0.00053105 -7.7707e-20 v k 1.8733e-08 0.0035549 0.0024709 0.0029438 v omega 35.795 1.0313e+05 2681.8 518.71 v TempK 288 341.3 292.01 289.55 v Density 1.205 1.205 1.205 1.205 v TurbVisc 2.2121e-13 0.00011223 7.5578e-05 9.4049e-05 v CourantNb 8.367e-10 0.00037064 2.0411e-05 1.0051e-05 v FourierNb 0.14692 0.62811 0.23357 0.19779 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.8833 4.8833 0.00035826 -2.3002e-07 v volume_forces[Z] -4.8833 4.8833 -0.00035814 2.8911e-07 v ǁvolume_forcesǁ 6.5182e-09 4.8854 0.36445 0.14 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.23 289.69 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.021128 7.1791e-05 4.0812e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14692 0.62811 0.23359 0.1978 INSTANT 0.204156000E+00 TIME STEP NUMBER 212 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.47811E-05 0.31714E-02 Friction velocity uk : 0.48870E-05 0.31712E-02 Dimensionless distance yplus : 0.32545E-04 0.21098E-01 Friction thermal sca. tstar : -0.14487E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.22858E-04 0.14818E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.47811E-05 0.31714E-02 Friction velocity uk : 0.48870E-05 0.31712E-02 Dimensionless distance yplus : 0.32545E-04 0.21098E-01 Friction thermal sca. tstar : -0.14487E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.22858E-04 0.14818E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.47214E-08 4 0.73569E-06 0.43142E-11 0.29211E+01 c Velocity[X] 0.53072E-30 c Velocity[Y] 0.21572E-11 c Velocity[Z] 0.21571E-11 c Pressure 0.65161E-13 23 0.96476E-08 0.51658E-06 0.39162E+01 c k 0.10119E-05 2 0.24211E-06 0.11485E-06 0.36219E+01 c omega 0.13153E+02 1 0.11171E-07 0.94860E+01 0.16034E-01 c TempK 0.94344E+02 1 0.52267E-06 0.13359E+00 0.40666E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.8437e-13 1.5443e-13 -1.7663e-17 -4.4333e-18 v Velocity[Y] -0.00019893 0.00019879 -8.0439e-10 -4.1604e-12 v Velocity[Z] -0.00019879 0.00019894 7.6355e-10 -8.5145e-13 v ǁVelocityǁ 1.7637e-10 0.00023417 1.3497e-05 6.9335e-06 v Pressure -0.0003527 0.01167 0.00053291 4.1672e-20 v k 1.8536e-08 0.0035407 0.0024617 0.0029336 v omega 35.694 1.0313e+05 2681.7 518.62 v TempK 288 341.31 292.01 289.55 v Density 1.205 1.205 1.205 1.205 v TurbVisc 2.1888e-13 0.0001121 7.5511e-05 9.3986e-05 v CourantNb 8.4085e-10 0.00036971 2.0359e-05 1.0026e-05 v FourierNb 0.1469 0.62811 0.23337 0.19764 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.8836 4.8837 0.00035882 -2.3127e-07 v volume_forces[Z] -4.8836 4.8837 -0.00035871 2.9057e-07 v ǁvolume_forcesǁ 6.4469e-09 4.8857 0.36502 0.14033 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.24 289.7 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.021098 7.1697e-05 4.0757e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.1469 0.62811 0.23339 0.19765 INSTANT 0.205119000E+00 TIME STEP NUMBER 213 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.47416E-05 0.31669E-02 Friction velocity uk : 0.48468E-05 0.31667E-02 Dimensionless distance yplus : 0.32277E-04 0.21068E-01 Friction thermal sca. tstar : -0.14433E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.22670E-04 0.14797E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.47416E-05 0.31669E-02 Friction velocity uk : 0.48468E-05 0.31667E-02 Dimensionless distance yplus : 0.32277E-04 0.21068E-01 Friction thermal sca. tstar : -0.14433E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.22670E-04 0.14797E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.47091E-08 4 0.81306E-06 0.42939E-11 0.29216E+01 c Velocity[X] 0.52396E-30 c Velocity[Y] 0.21470E-11 c Velocity[Z] 0.21469E-11 c Pressure 0.64663E-13 23 0.95970E-08 0.51258E-06 0.38976E+01 c k 0.10085E-05 2 0.23994E-06 0.11340E-06 0.36113E+01 c omega 0.13153E+02 1 0.11097E-07 0.93806E+01 0.15945E-01 c TempK 0.94345E+02 1 0.51948E-06 0.13269E+00 0.40529E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.8386e-13 1.5397e-13 -1.7618e-17 -4.4224e-18 v Velocity[Y] -0.00019848 0.00019831 -8.0724e-10 -4.1394e-12 v Velocity[Z] -0.00019832 0.00019848 7.6595e-10 -8.5155e-13 v ǁVelocityǁ 1.744e-10 0.00023353 1.3466e-05 6.9197e-06 v Pressure -0.00035442 0.011698 0.00053476 -2.5494e-21 v k 1.8342e-08 0.0035266 0.0024526 0.0029235 v omega 35.594 1.0313e+05 2681.7 518.53 v TempK 288 341.31 292.02 289.55 v Density 1.205 1.205 1.205 1.205 v TurbVisc 2.1658e-13 0.00011197 7.5445e-05 9.3924e-05 v CourantNb 8.4499e-10 0.00036879 2.0307e-05 1.0002e-05 v FourierNb 0.14687 0.62811 0.23316 0.19749 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.8839 4.884 0.00035938 -2.3251e-07 v volume_forces[Z] -4.8839 4.884 -0.00035927 2.9203e-07 v ǁvolume_forcesǁ 6.3758e-09 4.8861 0.36559 0.14067 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.25 289.7 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.021068 7.1603e-05 4.0702e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14687 0.62811 0.23318 0.1975 INSTANT 0.206082000E+00 TIME STEP NUMBER 214 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.47015E-05 0.31625E-02 Friction velocity uk : 0.48059E-05 0.31622E-02 Dimensionless distance yplus : 0.32005E-04 0.21038E-01 Friction thermal sca. tstar : -0.14380E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.22479E-04 0.14776E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.47015E-05 0.31625E-02 Friction velocity uk : 0.48059E-05 0.31622E-02 Dimensionless distance yplus : 0.32005E-04 0.21038E-01 Friction thermal sca. tstar : -0.14380E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.22479E-04 0.14776E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.46969E-08 4 0.72828E-06 0.42728E-11 0.29218E+01 c Velocity[X] 0.51725E-30 c Velocity[Y] 0.21364E-11 c Velocity[Z] 0.21364E-11 c Pressure 0.64230E-13 23 0.95499E-08 0.50910E-06 0.38792E+01 c k 0.10052E-05 2 0.23780E-06 0.11198E-06 0.36007E+01 c omega 0.13153E+02 1 0.11022E-07 0.92767E+01 0.15856E-01 c TempK 0.94345E+02 1 0.51632E-06 0.13180E+00 0.40393E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.8335e-13 1.5351e-13 -1.7573e-17 -4.4116e-18 v Velocity[Y] -0.00019802 0.00019784 -8.1008e-10 -4.1194e-12 v Velocity[Z] -0.00019784 0.00019803 7.6833e-10 -8.5147e-13 v ǁVelocityǁ 1.7244e-10 0.00023289 1.3435e-05 6.906e-06 v Pressure -0.00035613 0.011726 0.00053661 -4.0692e-20 v k 1.8151e-08 0.0035126 0.0024434 0.0029135 v omega 35.494 1.0313e+05 2681.6 518.44 v TempK 288 341.31 292.03 289.56 v Density 1.205 1.205 1.205 1.205 v TurbVisc 2.1432e-13 0.00011183 7.5379e-05 9.3861e-05 v CourantNb 8.4721e-10 0.00036787 2.0255e-05 9.9784e-06 v FourierNb 0.14684 0.62811 0.23296 0.19734 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.8843 4.8843 0.00035994 -2.3375e-07 v volume_forces[Z] -4.8843 4.8843 -0.00035983 2.9349e-07 v ǁvolume_forcesǁ 6.3047e-09 4.8864 0.36615 0.141 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.25 289.7 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.021038 7.151e-05 4.0647e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14684 0.62811 0.23298 0.19735 INSTANT 0.207045000E+00 TIME STEP NUMBER 215 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.46609E-05 0.31580E-02 Friction velocity uk : 0.47645E-05 0.31578E-02 Dimensionless distance yplus : 0.31730E-04 0.21009E-01 Friction thermal sca. tstar : -0.14327E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.22285E-04 0.14755E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.46609E-05 0.31580E-02 Friction velocity uk : 0.47645E-05 0.31578E-02 Dimensionless distance yplus : 0.31730E-04 0.21009E-01 Friction thermal sca. tstar : -0.14327E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.22285E-04 0.14755E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.46848E-08 4 0.72457E-06 0.42511E-11 0.29218E+01 c Velocity[X] 0.51059E-30 c Velocity[Y] 0.21256E-11 c Velocity[Z] 0.21255E-11 c Pressure 0.63816E-13 23 0.94972E-08 0.50577E-06 0.38610E+01 c k 0.10019E-05 2 0.23570E-06 0.11058E-06 0.35902E+01 c omega 0.13153E+02 1 0.10949E-07 0.91741E+01 0.15768E-01 c TempK 0.94346E+02 1 0.51319E-06 0.13093E+00 0.40258E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.8284e-13 1.5306e-13 -1.7529e-17 -4.4009e-18 v Velocity[Y] -0.00019757 0.00019737 -8.1289e-10 -4.0989e-12 v Velocity[Z] -0.00019737 0.00019757 7.707e-10 -8.5142e-13 v ǁVelocityǁ 1.7049e-10 0.00023226 1.3403e-05 6.8923e-06 v Pressure -0.00035784 0.011754 0.00053845 -1.613e-20 v k 1.7963e-08 0.0034987 0.0024344 0.0029035 v omega 35.395 1.0313e+05 2681.5 518.34 v TempK 288 341.32 292.03 289.56 v Density 1.205 1.205 1.205 1.205 v TurbVisc 2.1209e-13 0.0001117 7.5313e-05 9.3799e-05 v CourantNb 8.4749e-10 0.00036695 2.0204e-05 9.9544e-06 v FourierNb 0.14682 0.62811 0.23276 0.19719 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.8846 4.8847 0.0003605 -2.3498e-07 v volume_forces[Z] -4.8846 4.8847 -0.00036039 2.9493e-07 v ǁvolume_forcesǁ 6.2338e-09 4.8867 0.36672 0.14133 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.26 289.71 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.021009 7.1418e-05 4.0593e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14682 0.62811 0.23278 0.1972 INSTANT 0.208008000E+00 TIME STEP NUMBER 216 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.46195E-05 0.31536E-02 Friction velocity uk : 0.47225E-05 0.31534E-02 Dimensionless distance yplus : 0.31450E-04 0.20980E-01 Friction thermal sca. tstar : -0.14275E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.22088E-04 0.14735E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.46195E-05 0.31536E-02 Friction velocity uk : 0.47225E-05 0.31534E-02 Dimensionless distance yplus : 0.31450E-04 0.20980E-01 Friction thermal sca. tstar : -0.14275E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.22088E-04 0.14735E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.46726E-08 4 0.73277E-06 0.42288E-11 0.29215E+01 c Velocity[X] 0.50400E-30 c Velocity[Y] 0.21144E-11 c Velocity[Z] 0.21144E-11 c Pressure 0.63370E-13 23 0.94479E-08 0.50219E-06 0.38429E+01 c k 0.99858E-06 2 0.23362E-06 0.10920E-06 0.35798E+01 c omega 0.13153E+02 1 0.10876E-07 0.90730E+01 0.15681E-01 c TempK 0.94347E+02 1 0.51009E-06 0.13006E+00 0.40124E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.8233e-13 1.5261e-13 -1.7485e-17 -4.3904e-18 v Velocity[Y] -0.00019712 0.0001969 -8.1569e-10 -4.0786e-12 v Velocity[Z] -0.0001969 0.00019712 7.7305e-10 -8.5127e-13 v ǁVelocityǁ 1.6853e-10 0.00023163 1.3372e-05 6.8787e-06 v Pressure -0.00035956 0.011782 0.00054029 -1.3409e-20 v k 1.7777e-08 0.0034848 0.0024254 0.0028936 v omega 35.296 1.0313e+05 2681.4 518.25 v TempK 288 341.32 292.04 289.57 v Density 1.205 1.205 1.205 1.205 v TurbVisc 2.0988e-13 0.00011157 7.5247e-05 9.3738e-05 v CourantNb 8.4774e-10 0.00036603 2.0152e-05 9.9306e-06 v FourierNb 0.14679 0.62811 0.23256 0.19704 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.8849 4.885 0.00036106 -2.3621e-07 v volume_forces[Z] -4.8849 4.885 -0.00036094 2.9637e-07 v ǁvolume_forcesǁ 6.163e-09 4.887 0.36728 0.14167 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.27 289.71 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.02098 7.1326e-05 4.0539e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14679 0.62811 0.23258 0.19705 INSTANT 0.208971000E+00 TIME STEP NUMBER 217 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.45775E-05 0.31492E-02 Friction velocity uk : 0.46798E-05 0.31490E-02 Dimensionless distance yplus : 0.31166E-04 0.20950E-01 Friction thermal sca. tstar : -0.14224E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.21889E-04 0.14714E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.45775E-05 0.31492E-02 Friction velocity uk : 0.46798E-05 0.31490E-02 Dimensionless distance yplus : 0.31166E-04 0.20950E-01 Friction thermal sca. tstar : -0.14224E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.21889E-04 0.14714E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.46605E-08 4 0.72246E-06 0.42058E-11 0.29209E+01 c Velocity[X] 0.49746E-30 c Velocity[Y] 0.21029E-11 c Velocity[Z] 0.21029E-11 c Pressure 0.62929E-13 23 0.93982E-08 0.49866E-06 0.38250E+01 c k 0.99532E-06 2 0.23158E-06 0.10784E-06 0.35694E+01 c omega 0.13153E+02 1 0.10804E-07 0.89732E+01 0.15595E-01 c TempK 0.94348E+02 1 0.50703E-06 0.12920E+00 0.39991E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.8183e-13 1.5216e-13 -1.7441e-17 -4.3799e-18 v Velocity[Y] -0.00019667 0.00019643 -8.1847e-10 -4.0584e-12 v Velocity[Z] -0.00019644 0.00019668 7.7538e-10 -8.5144e-13 v ǁVelocityǁ 1.6659e-10 0.000231 1.3341e-05 6.8651e-06 v Pressure -0.00036127 0.011811 0.00054213 1.0296e-21 v k 1.7594e-08 0.003471 0.0024165 0.0028838 v omega 35.198 1.0313e+05 2681.4 518.16 v TempK 288 341.32 292.05 289.57 v Density 1.205 1.205 1.205 1.205 v TurbVisc 2.0771e-13 0.00011144 7.5182e-05 9.3676e-05 v CourantNb 8.4798e-10 0.00036512 2.0101e-05 9.9068e-06 v FourierNb 0.14676 0.62811 0.23236 0.1969 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.8852 4.8853 0.00036161 -2.3743e-07 v volume_forces[Z] -4.8852 4.8853 -0.0003615 2.978e-07 v ǁvolume_forcesǁ 6.0925e-09 4.8874 0.36784 0.142 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.27 289.72 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.02095 7.1234e-05 4.0485e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14676 0.62811 0.23238 0.19691 INSTANT 0.209934000E+00 TIME STEP NUMBER 218 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.45348E-05 0.31449E-02 Friction velocity uk : 0.46365E-05 0.31446E-02 Dimensionless distance yplus : 0.30877E-04 0.20921E-01 Friction thermal sca. tstar : -0.14174E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.21686E-04 0.14694E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.45348E-05 0.31449E-02 Friction velocity uk : 0.46365E-05 0.31446E-02 Dimensionless distance yplus : 0.30877E-04 0.20921E-01 Friction thermal sca. tstar : -0.14174E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.21686E-04 0.14694E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.46485E-08 4 0.71881E-06 0.41823E-11 0.29200E+01 c Velocity[X] 0.49098E-30 c Velocity[Y] 0.20912E-11 c Velocity[Z] 0.20911E-11 c Pressure 0.62500E-13 23 0.93461E-08 0.49521E-06 0.38073E+01 c k 0.99207E-06 2 0.22957E-06 0.10650E-06 0.35591E+01 c omega 0.13153E+02 1 0.10733E-07 0.88748E+01 0.15509E-01 c TempK 0.94348E+02 1 0.50399E-06 0.12836E+00 0.39859E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.8133e-13 1.5172e-13 -1.7398e-17 -4.3695e-18 v Velocity[Y] -0.00019623 0.00019597 -8.2124e-10 -4.0382e-12 v Velocity[Z] -0.00019598 0.00019623 7.7769e-10 -8.5152e-13 v ǁVelocityǁ 1.6465e-10 0.00023037 1.3311e-05 6.8516e-06 v Pressure -0.00036298 0.011838 0.00054397 3.3877e-20 v k 1.7413e-08 0.0034574 0.0024076 0.002874 v omega 35.1 1.0313e+05 2681.3 518.07 v TempK 288 341.33 292.05 289.57 v Density 1.205 1.205 1.205 1.205 v TurbVisc 2.0557e-13 0.00011134 7.5117e-05 9.3615e-05 v CourantNb 8.4971e-10 0.0003642 2.005e-05 9.8831e-06 v FourierNb 0.14674 0.62811 0.23216 0.19675 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.8856 4.8856 0.00036217 -2.3864e-07 v volume_forces[Z] -4.8856 4.8856 -0.00036205 2.9922e-07 v ǁvolume_forcesǁ 6.0221e-09 4.8877 0.3684 0.14233 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.28 289.72 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.020921 7.1143e-05 4.0432e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14674 0.62811 0.23218 0.19676 INSTANT 0.210897000E+00 TIME STEP NUMBER 219 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.44915E-05 0.31405E-02 Friction velocity uk : 0.45926E-05 0.31402E-02 Dimensionless distance yplus : 0.30585E-04 0.20892E-01 Friction thermal sca. tstar : -0.14124E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.21481E-04 0.14673E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.44915E-05 0.31405E-02 Friction velocity uk : 0.45926E-05 0.31402E-02 Dimensionless distance yplus : 0.30585E-04 0.20892E-01 Friction thermal sca. tstar : -0.14124E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.21481E-04 0.14673E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.46365E-08 4 0.70998E-06 0.41582E-11 0.29189E+01 c Velocity[X] 0.48455E-30 c Velocity[Y] 0.20791E-11 c Velocity[Z] 0.20791E-11 c Pressure 0.62087E-13 23 0.92942E-08 0.49189E-06 0.37897E+01 c k 0.98884E-06 2 0.22759E-06 0.10518E-06 0.35488E+01 c omega 0.13153E+02 1 0.10662E-07 0.87777E+01 0.15424E-01 c TempK 0.94349E+02 1 0.50099E-06 0.12752E+00 0.39728E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.8084e-13 1.5127e-13 -1.7355e-17 -4.3591e-18 v Velocity[Y] -0.00019579 0.00019551 -8.2399e-10 -4.0181e-12 v Velocity[Z] -0.00019551 0.00019579 7.7999e-10 -8.5177e-13 v ǁVelocityǁ 1.6272e-10 0.00022975 1.328e-05 6.8382e-06 v Pressure -0.00036469 0.011866 0.0005458 -1.6522e-20 v k 1.7235e-08 0.0034438 0.0023988 0.0028643 v omega 35.003 1.0313e+05 2681.2 517.98 v TempK 288 341.33 292.06 289.58 v Density 1.205 1.205 1.205 1.205 v TurbVisc 2.0346e-13 0.00011124 7.5052e-05 9.3553e-05 v CourantNb 8.5377e-10 0.0003633 1.9999e-05 9.8595e-06 v FourierNb 0.14671 0.62811 0.23196 0.19661 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.8859 4.8859 0.00036272 -2.3985e-07 v volume_forces[Z] -4.8859 4.8859 -0.0003626 3.0063e-07 v ǁvolume_forcesǁ 5.952e-09 4.888 0.36895 0.14266 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.28 289.72 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.020892 7.1053e-05 4.0379e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14671 0.62811 0.23198 0.19662 INSTANT 0.211860000E+00 TIME STEP NUMBER 220 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.44474E-05 0.31362E-02 Friction velocity uk : 0.45479E-05 0.31359E-02 Dimensionless distance yplus : 0.30287E-04 0.20863E-01 Friction thermal sca. tstar : -0.14074E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.21272E-04 0.14653E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.44474E-05 0.31362E-02 Friction velocity uk : 0.45479E-05 0.31359E-02 Dimensionless distance yplus : 0.30287E-04 0.20863E-01 Friction thermal sca. tstar : -0.14074E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.21272E-04 0.14653E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.46245E-08 4 0.70641E-06 0.41335E-11 0.29176E+01 c Velocity[X] 0.47819E-30 c Velocity[Y] 0.20668E-11 c Velocity[Z] 0.20667E-11 c Pressure 0.61665E-13 23 0.92420E-08 0.48851E-06 0.37723E+01 c k 0.98563E-06 2 0.22564E-06 0.10388E-06 0.35386E+01 c omega 0.13153E+02 1 0.10592E-07 0.86819E+01 0.15339E-01 c TempK 0.94350E+02 1 0.49801E-06 0.12669E+00 0.39598E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.8035e-13 1.5083e-13 -1.7313e-17 -4.3489e-18 v Velocity[Y] -0.00019535 0.00019505 -8.2672e-10 -3.9982e-12 v Velocity[Z] -0.00019505 0.00019535 7.8226e-10 -8.521e-13 v ǁVelocityǁ 1.608e-10 0.00022913 1.3249e-05 6.8248e-06 v Pressure -0.00036641 0.011894 0.00054763 -3.6181e-20 v k 1.7059e-08 0.0034302 0.0023901 0.0028546 v omega 34.906 1.0313e+05 2681.1 517.9 v TempK 288 341.33 292.06 289.58 v Density 1.205 1.205 1.205 1.205 v TurbVisc 2.0138e-13 0.00011114 7.4988e-05 9.3493e-05 v CourantNb 8.5783e-10 0.00036239 1.9949e-05 9.836e-06 v FourierNb 0.14668 0.62811 0.23176 0.19646 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.8862 4.8863 0.00036327 -2.4106e-07 v volume_forces[Z] -4.8862 4.8863 -0.00036315 3.0204e-07 v ǁvolume_forcesǁ 5.8822e-09 4.8883 0.36951 0.14299 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.29 289.73 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.020863 7.0963e-05 4.0326e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14668 0.62811 0.23178 0.19647 INSTANT 0.212823000E+00 TIME STEP NUMBER 221 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.44025E-05 0.31319E-02 Friction velocity uk : 0.45026E-05 0.31316E-02 Dimensionless distance yplus : 0.29985E-04 0.20835E-01 Friction thermal sca. tstar : -0.14026E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.21060E-04 0.14633E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.44025E-05 0.31319E-02 Friction velocity uk : 0.45026E-05 0.31316E-02 Dimensionless distance yplus : 0.29985E-04 0.20835E-01 Friction thermal sca. tstar : -0.14026E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.21060E-04 0.14633E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.46126E-08 4 0.70283E-06 0.41084E-11 0.29160E+01 c Velocity[X] 0.47188E-30 c Velocity[Y] 0.20542E-11 c Velocity[Z] 0.20541E-11 c Pressure 0.61243E-13 23 0.91909E-08 0.48512E-06 0.37550E+01 c k 0.98244E-06 2 0.22372E-06 0.10261E-06 0.35284E+01 c omega 0.13153E+02 1 0.10522E-07 0.85874E+01 0.15256E-01 c TempK 0.94351E+02 1 0.49507E-06 0.12587E+00 0.39469E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.7986e-13 1.504e-13 -1.7271e-17 -4.3388e-18 v Velocity[Y] -0.00019491 0.00019459 -8.2944e-10 -3.9784e-12 v Velocity[Z] -0.0001946 0.00019491 7.8452e-10 -8.5237e-13 v ǁVelocityǁ 1.5888e-10 0.00022851 1.3219e-05 6.8115e-06 v Pressure -0.00036812 0.011922 0.00054945 1.1178e-20 v k 1.6886e-08 0.0034168 0.0023814 0.002845 v omega 34.81 1.0313e+05 2681.1 517.81 v TempK 288 341.34 292.07 289.58 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.9933e-13 0.00011105 7.4924e-05 9.3432e-05 v CourantNb 8.6189e-10 0.00036149 1.9899e-05 9.8126e-06 v FourierNb 0.14666 0.62811 0.23157 0.19632 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.8865 4.8866 0.00036382 -2.4226e-07 v volume_forces[Z] -4.8865 4.8866 -0.0003637 3.0344e-07 v ǁvolume_forcesǁ 5.8128e-09 4.8886 0.37006 0.14332 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.3 289.73 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.020835 7.0874e-05 4.0273e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14666 0.62811 0.23159 0.19633 INSTANT 0.213786000E+00 TIME STEP NUMBER 222 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.43569E-05 0.31276E-02 Friction velocity uk : 0.44565E-05 0.31273E-02 Dimensionless distance yplus : 0.29678E-04 0.20806E-01 Friction thermal sca. tstar : -0.13977E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.20844E-04 0.14613E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.43569E-05 0.31276E-02 Friction velocity uk : 0.44565E-05 0.31273E-02 Dimensionless distance yplus : 0.29678E-04 0.20806E-01 Friction thermal sca. tstar : -0.13977E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.20844E-04 0.14613E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.46007E-08 4 0.69932E-06 0.40827E-11 0.29142E+01 c Velocity[X] 0.46563E-30 c Velocity[Y] 0.20414E-11 c Velocity[Z] 0.20413E-11 c Pressure 0.60951E-13 23 0.91423E-08 0.48277E-06 0.37379E+01 c k 0.97927E-06 2 0.22183E-06 0.10135E-06 0.35184E+01 c omega 0.13153E+02 1 0.10454E-07 0.84942E+01 0.15173E-01 c TempK 0.94351E+02 1 0.49215E-06 0.12506E+00 0.39341E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.7937e-13 1.4996e-13 -1.7229e-17 -4.3287e-18 v Velocity[Y] -0.00019448 0.00019414 -8.3214e-10 -3.9588e-12 v Velocity[Z] -0.00019414 0.00019448 7.8676e-10 -8.53e-13 v ǁVelocityǁ 1.5699e-10 0.0002279 1.3189e-05 6.7983e-06 v Pressure -0.00036983 0.01195 0.00055127 -2.5052e-20 v k 1.6715e-08 0.0034034 0.0023728 0.0028354 v omega 34.715 1.0313e+05 2681 517.72 v TempK 288 341.34 292.08 289.59 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.973e-13 0.00011095 7.486e-05 9.3371e-05 v CourantNb 8.6596e-10 0.00036059 1.9849e-05 9.7893e-06 v FourierNb 0.14663 0.62811 0.23138 0.19618 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.8868 4.8869 0.00036436 -2.4345e-07 v volume_forces[Z] -4.8868 4.8869 -0.00036424 3.0484e-07 v ǁvolume_forcesǁ 5.7437e-09 4.8889 0.37061 0.14365 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.3 289.73 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.020806 7.0785e-05 4.0221e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14663 0.62811 0.2314 0.19619 INSTANT 0.214749000E+00 TIME STEP NUMBER 223 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.43106E-05 0.31233E-02 Friction velocity uk : 0.44097E-05 0.31231E-02 Dimensionless distance yplus : 0.29366E-04 0.20778E-01 Friction thermal sca. tstar : -0.13930E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.20625E-04 0.14593E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.43106E-05 0.31233E-02 Friction velocity uk : 0.44097E-05 0.31231E-02 Dimensionless distance yplus : 0.29366E-04 0.20778E-01 Friction thermal sca. tstar : -0.13930E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.20625E-04 0.14593E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.45889E-08 4 0.69573E-06 0.40566E-11 0.29121E+01 c Velocity[X] 0.45945E-30 c Velocity[Y] 0.20283E-11 c Velocity[Z] 0.20283E-11 c Pressure 0.60399E-13 23 0.90867E-08 0.47835E-06 0.37209E+01 c k 0.97611E-06 2 0.21996E-06 0.10011E-06 0.35083E+01 c omega 0.13153E+02 1 0.10385E-07 0.84022E+01 0.15090E-01 c TempK 0.94352E+02 1 0.48927E-06 0.12425E+00 0.39214E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.7889e-13 1.4953e-13 -1.7188e-17 -4.3188e-18 v Velocity[Y] -0.00019404 0.00019369 -8.3482e-10 -3.9388e-12 v Velocity[Z] -0.00019369 0.00019405 7.8899e-10 -8.5301e-13 v ǁVelocityǁ 1.551e-10 0.00022729 1.3159e-05 6.7851e-06 v Pressure -0.00037155 0.011977 0.00055309 6.2754e-21 v k 1.6547e-08 0.0033902 0.0023642 0.0028259 v omega 34.62 1.0313e+05 2680.9 517.63 v TempK 288 341.34 292.08 289.59 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.953e-13 0.00011085 7.4796e-05 9.3311e-05 v CourantNb 8.7002e-10 0.00035969 1.9799e-05 9.7661e-06 v FourierNb 0.1466 0.62811 0.23118 0.19603 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.8871 4.8872 0.00036491 -2.4463e-07 v volume_forces[Z] -4.8871 4.8872 -0.00036479 3.0623e-07 v ǁvolume_forcesǁ 5.6751e-09 4.8892 0.37116 0.14397 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.31 289.74 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.020778 7.0696e-05 4.0169e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.1466 0.62811 0.2312 0.19604 INSTANT 0.215712000E+00 TIME STEP NUMBER 224 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.42634E-05 0.31191E-02 Friction velocity uk : 0.43620E-05 0.31188E-02 Dimensionless distance yplus : 0.29049E-04 0.20750E-01 Friction thermal sca. tstar : -0.13883E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.20402E-04 0.14573E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.42634E-05 0.31191E-02 Friction velocity uk : 0.43620E-05 0.31188E-02 Dimensionless distance yplus : 0.29049E-04 0.20750E-01 Friction thermal sca. tstar : -0.13883E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.20402E-04 0.14573E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.45772E-08 4 0.69220E-06 0.40300E-11 0.29098E+01 c Velocity[X] 0.45333E-30 c Velocity[Y] 0.20150E-11 c Velocity[Z] 0.20150E-11 c Pressure 0.59985E-13 23 0.90352E-08 0.47503E-06 0.37041E+01 c k 0.97298E-06 2 0.21813E-06 0.98885E-07 0.34984E+01 c omega 0.13153E+02 1 0.10318E-07 0.83114E+01 0.15009E-01 c TempK 0.94353E+02 1 0.48641E-06 0.12346E+00 0.39088E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.7841e-13 1.491e-13 -1.7147e-17 -4.3089e-18 v Velocity[Y] -0.00019361 0.00019324 -8.3749e-10 -3.9191e-12 v Velocity[Z] -0.00019324 0.00019362 7.912e-10 -8.5362e-13 v ǁVelocityǁ 1.5323e-10 0.00022668 1.3129e-05 6.772e-06 v Pressure -0.00037326 0.012005 0.00055491 2.6229e-20 v k 1.638e-08 0.003377 0.0023557 0.0028165 v omega 34.525 1.0313e+05 2680.8 517.55 v TempK 288 341.35 292.09 289.59 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.9333e-13 0.00011075 7.4733e-05 9.3251e-05 v CourantNb 8.7409e-10 0.0003588 1.9749e-05 9.743e-06 v FourierNb 0.14658 0.62811 0.23099 0.19589 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.8875 4.8875 0.00036545 -2.4582e-07 v volume_forces[Z] -4.8875 4.8875 -0.00036533 3.0761e-07 v ǁvolume_forcesǁ 5.6069e-09 4.8895 0.37171 0.1443 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.31 289.74 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.02075 7.0608e-05 4.0117e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14658 0.62811 0.23101 0.1959 INSTANT 0.216675000E+00 TIME STEP NUMBER 225 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.42153E-05 0.31149E-02 Friction velocity uk : 0.43136E-05 0.31146E-02 Dimensionless distance yplus : 0.28727E-04 0.20722E-01 Friction thermal sca. tstar : -0.13836E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.20176E-04 0.14554E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.42153E-05 0.31149E-02 Friction velocity uk : 0.43136E-05 0.31146E-02 Dimensionless distance yplus : 0.28727E-04 0.20722E-01 Friction thermal sca. tstar : -0.13836E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.20176E-04 0.14554E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.45655E-08 4 0.68882E-06 0.40030E-11 0.29072E+01 c Velocity[X] 0.44726E-30 c Velocity[Y] 0.20015E-11 c Velocity[Z] 0.20015E-11 c Pressure 0.59868E-13 23 0.89963E-08 0.47407E-06 0.36874E+01 c k 0.96986E-06 2 0.21632E-06 0.97682E-07 0.34885E+01 c omega 0.13153E+02 1 0.10251E-07 0.82219E+01 0.14928E-01 c TempK 0.94353E+02 1 0.48357E-06 0.12267E+00 0.38963E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.7793e-13 1.4868e-13 -1.7106e-17 -4.2991e-18 v Velocity[Y] -0.00019319 0.00019279 -8.4014e-10 -3.8996e-12 v Velocity[Z] -0.0001928 0.00019319 7.9339e-10 -8.5396e-13 v ǁVelocityǁ 1.5138e-10 0.00022607 1.3099e-05 6.759e-06 v Pressure -0.00037497 0.012032 0.00055672 9.8053e-21 v k 1.6216e-08 0.0033643 0.0023472 0.0028071 v omega 34.431 1.0313e+05 2680.8 517.46 v TempK 288 341.35 292.09 289.6 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.9139e-13 0.00011065 7.467e-05 9.3191e-05 v CourantNb 8.7815e-10 0.00035791 1.97e-05 9.72e-06 v FourierNb 0.14655 0.62811 0.2308 0.19575 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.8878 4.8878 0.00036599 -2.4699e-07 v volume_forces[Z] -4.8878 4.8878 -0.00036587 3.0898e-07 v ǁvolume_forcesǁ 5.5392e-09 4.8898 0.37225 0.14463 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.32 289.74 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.020722 7.0521e-05 4.0066e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14655 0.62811 0.23082 0.19576 INSTANT 0.217638000E+00 TIME STEP NUMBER 226 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.41665E-05 0.31107E-02 Friction velocity uk : 0.42644E-05 0.31104E-02 Dimensionless distance yplus : 0.28399E-04 0.20694E-01 Friction thermal sca. tstar : -0.13958E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.19946E-04 0.14534E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.41665E-05 0.31107E-02 Friction velocity uk : 0.42644E-05 0.31104E-02 Dimensionless distance yplus : 0.28399E-04 0.20694E-01 Friction thermal sca. tstar : -0.13958E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.19946E-04 0.14534E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.45538E-08 4 0.68522E-06 0.39756E-11 0.29044E+01 c Velocity[X] 0.44127E-30 c Velocity[Y] 0.19878E-11 c Velocity[Z] 0.19878E-11 c Pressure 0.59180E-13 23 0.89319E-08 0.46858E-06 0.36709E+01 c k 0.96677E-06 2 0.21454E-06 0.96497E-07 0.34786E+01 c omega 0.13153E+02 1 0.10185E-07 0.81335E+01 0.14847E-01 c TempK 0.94354E+02 1 0.48077E-06 0.12189E+00 0.38839E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.7745e-13 1.4825e-13 -1.7066e-17 -4.2894e-18 v Velocity[Y] -0.00019276 0.00019235 -8.4277e-10 -3.8798e-12 v Velocity[Z] -0.00019235 0.00019276 7.9556e-10 -8.5419e-13 v ǁVelocityǁ 1.4954e-10 0.00022547 1.3069e-05 6.746e-06 v Pressure -0.00037669 0.01206 0.00055853 1.0688e-20 v k 1.6054e-08 0.003352 0.0023388 0.0027978 v omega 34.338 1.0313e+05 2680.7 517.37 v TempK 288 341.35 292.1 289.6 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.8947e-13 0.00011055 7.4607e-05 9.3131e-05 v CourantNb 8.8222e-10 0.00035702 1.9651e-05 9.6971e-06 v FourierNb 0.14652 0.62811 0.23061 0.19561 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.8881 4.8881 0.00036653 -2.4816e-07 v volume_forces[Z] -4.8881 4.8881 -0.00036641 3.1035e-07 v ǁvolume_forcesǁ 5.4722e-09 4.8901 0.3728 0.14495 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.33 289.75 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.020694 7.0434e-05 4.0015e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14652 0.62811 0.23063 0.19562 INSTANT 0.218601000E+00 TIME STEP NUMBER 227 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.41166E-05 0.31065E-02 Friction velocity uk : 0.42143E-05 0.31062E-02 Dimensionless distance yplus : 0.28065E-04 0.20666E-01 Friction thermal sca. tstar : -0.14204E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.19711E-04 0.14514E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.41166E-05 0.31065E-02 Friction velocity uk : 0.42143E-05 0.31062E-02 Dimensionless distance yplus : 0.28065E-04 0.20666E-01 Friction thermal sca. tstar : -0.14204E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.19711E-04 0.14514E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.45422E-08 4 0.68172E-06 0.39478E-11 0.29014E+01 c Velocity[X] 0.43532E-30 c Velocity[Y] 0.19739E-11 c Velocity[Z] 0.19739E-11 c Pressure 0.58789E-13 23 0.88790E-08 0.46545E-06 0.36545E+01 c k 0.96369E-06 2 0.21278E-06 0.95330E-07 0.34688E+01 c omega 0.13153E+02 1 0.10119E-07 0.80463E+01 0.14767E-01 c TempK 0.94355E+02 1 0.47799E-06 0.12112E+00 0.38715E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.7698e-13 1.4783e-13 -1.7026e-17 -4.2798e-18 v Velocity[Y] -0.00019234 0.0001919 -8.4539e-10 -3.8604e-12 v Velocity[Z] -0.00019191 0.00019234 7.9772e-10 -8.5449e-13 v ǁVelocityǁ 1.4772e-10 0.00022487 1.304e-05 6.7332e-06 v Pressure -0.0003784 0.012087 0.00056034 1.3874e-20 v k 1.5895e-08 0.0033398 0.0023304 0.0027885 v omega 34.245 1.0313e+05 2680.6 517.29 v TempK 288 341.36 292.11 289.61 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.8758e-13 0.00011045 7.4545e-05 9.3072e-05 v CourantNb 8.8628e-10 0.00035614 1.9602e-05 9.6743e-06 v FourierNb 0.14649 0.62811 0.23042 0.19547 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.8884 4.8884 0.00036707 -2.4933e-07 v volume_forces[Z] -4.8884 4.8884 -0.00036695 3.1171e-07 v ǁvolume_forcesǁ 5.4057e-09 4.8904 0.37334 0.14527 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.33 289.75 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.020666 7.0348e-05 3.9964e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.1465 0.62811 0.23044 0.19548 INSTANT 0.219564000E+00 TIME STEP NUMBER 228 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.40659E-05 0.31023E-02 Friction velocity uk : 0.41633E-05 0.31021E-02 Dimensionless distance yplus : 0.27726E-04 0.20638E-01 Friction thermal sca. tstar : -0.14466E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.19473E-04 0.14495E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.40659E-05 0.31023E-02 Friction velocity uk : 0.41633E-05 0.31021E-02 Dimensionless distance yplus : 0.27726E-04 0.20638E-01 Friction thermal sca. tstar : -0.14466E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.19473E-04 0.14495E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.45307E-08 4 0.67830E-06 0.39196E-11 0.28982E+01 c Velocity[X] 0.42944E-30 c Velocity[Y] 0.19598E-11 c Velocity[Z] 0.19598E-11 c Pressure 0.58465E-13 23 0.88282E-08 0.46284E-06 0.36383E+01 c k 0.96063E-06 2 0.21105E-06 0.94180E-07 0.34591E+01 c omega 0.13153E+02 1 0.10054E-07 0.79602E+01 0.14688E-01 c TempK 0.94356E+02 1 0.47524E-06 0.12036E+00 0.38593E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.7651e-13 1.4741e-13 -1.6986e-17 -4.2702e-18 v Velocity[Y] -0.00019192 0.00019147 -8.4799e-10 -3.8414e-12 v Velocity[Z] -0.00019147 0.00019192 7.9986e-10 -8.5515e-13 v ǁVelocityǁ 1.4592e-10 0.00022427 1.3011e-05 6.7204e-06 v Pressure -0.00038012 0.012115 0.00056214 4.307e-20 v k 1.5737e-08 0.0033277 0.0023221 0.0027793 v omega 34.153 1.0313e+05 2680.6 517.2 v TempK 288 341.36 292.11 289.61 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.8572e-13 0.00011035 7.4482e-05 9.3012e-05 v CourantNb 8.9035e-10 0.00035526 1.9553e-05 9.6516e-06 v FourierNb 0.14647 0.62811 0.23024 0.19533 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.8887 4.8887 0.0003676 -2.5049e-07 v volume_forces[Z] -4.8887 4.8887 -0.00036748 3.1307e-07 v ǁvolume_forcesǁ 5.3399e-09 4.8907 0.37388 0.1456 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.34 289.76 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.020638 7.0262e-05 3.9913e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14647 0.62811 0.23026 0.19534 INSTANT 0.220527000E+00 TIME STEP NUMBER 229 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.40142E-05 0.30982E-02 Friction velocity uk : 0.41114E-05 0.30980E-02 Dimensionless distance yplus : 0.27380E-04 0.20611E-01 Friction thermal sca. tstar : -0.14742E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.19230E-04 0.14476E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.40142E-05 0.30982E-02 Friction velocity uk : 0.41114E-05 0.30980E-02 Dimensionless distance yplus : 0.27380E-04 0.20611E-01 Friction thermal sca. tstar : -0.14742E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.19230E-04 0.14476E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.45192E-08 4 0.67484E-06 0.38910E-11 0.28948E+01 c Velocity[X] 0.42362E-30 c Velocity[Y] 0.19455E-11 c Velocity[Z] 0.19455E-11 c Pressure 0.58018E-13 23 0.87762E-08 0.45927E-06 0.36222E+01 c k 0.95758E-06 2 0.20935E-06 0.93047E-07 0.34494E+01 c omega 0.13153E+02 1 0.99892E-08 0.78753E+01 0.14610E-01 c TempK 0.94356E+02 1 0.47252E-06 0.11961E+00 0.38472E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.7605e-13 1.47e-13 -1.6947e-17 -4.2608e-18 v Velocity[Y] -0.0001915 0.00019103 -8.5057e-10 -3.8221e-12 v Velocity[Z] -0.00019103 0.0001915 8.0198e-10 -8.5548e-13 v ǁVelocityǁ 1.4414e-10 0.00022368 1.2981e-05 6.7077e-06 v Pressure -0.00038183 0.012142 0.00056394 -2.944e-20 v k 1.5582e-08 0.0033157 0.0023139 0.0027701 v omega 34.061 1.0313e+05 2680.5 517.12 v TempK 288 341.36 292.12 289.61 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.8388e-13 0.00011025 7.442e-05 9.2953e-05 v CourantNb 8.9442e-10 0.00035438 1.9505e-05 9.6291e-06 v FourierNb 0.14644 0.62811 0.23005 0.19519 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.889 4.889 0.00036814 -2.5164e-07 v volume_forces[Z] -4.889 4.889 -0.00036802 3.1441e-07 v ǁvolume_forcesǁ 5.275e-09 4.891 0.37442 0.14592 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.34 289.76 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.020611 7.0176e-05 3.9863e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14644 0.62811 0.23007 0.1952 INSTANT 0.221490000E+00 TIME STEP NUMBER 230 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.39616E-05 0.30941E-02 Friction velocity uk : 0.40585E-05 0.30938E-02 Dimensionless distance yplus : 0.27028E-04 0.20584E-01 Friction thermal sca. tstar : -0.15034E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.18983E-04 0.14457E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.39616E-05 0.30941E-02 Friction velocity uk : 0.40585E-05 0.30938E-02 Dimensionless distance yplus : 0.27028E-04 0.20584E-01 Friction thermal sca. tstar : -0.15034E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.18983E-04 0.14457E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.45077E-08 4 0.67137E-06 0.38622E-11 0.28911E+01 c Velocity[X] 0.41786E-30 c Velocity[Y] 0.19311E-11 c Velocity[Z] 0.19311E-11 c Pressure 0.57542E-13 23 0.87226E-08 0.45546E-06 0.36062E+01 c k 0.95456E-06 2 0.20767E-06 0.91930E-07 0.34397E+01 c omega 0.13153E+02 1 0.99253E-08 0.77915E+01 0.14532E-01 c TempK 0.94357E+02 1 0.46982E-06 0.11886E+00 0.38351E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.7558e-13 1.4658e-13 -1.6908e-17 -4.2514e-18 v Velocity[Y] -0.00019109 0.00019059 -8.5314e-10 -3.8026e-12 v Velocity[Z] -0.0001906 0.00019109 8.0409e-10 -8.5553e-13 v ǁVelocityǁ 1.4239e-10 0.00022309 1.2952e-05 6.695e-06 v Pressure -0.00038355 0.012169 0.00056574 2.6548e-20 v k 1.5428e-08 0.0033037 0.0023057 0.002761 v omega 33.969 1.0313e+05 2680.4 517.04 v TempK 288 341.37 292.12 289.62 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.8206e-13 0.00011015 7.4359e-05 9.2894e-05 v CourantNb 8.9849e-10 0.00035351 1.9457e-05 9.6066e-06 v FourierNb 0.14641 0.62811 0.22987 0.19506 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.8893 4.8893 0.00036867 -2.5279e-07 v volume_forces[Z] -4.8893 4.8893 -0.00036855 3.1575e-07 v ǁvolume_forcesǁ 5.2108e-09 4.8913 0.37495 0.14624 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.35 289.76 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.020584 7.0091e-05 3.9813e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14642 0.62811 0.22988 0.19506 INSTANT 0.222453000E+00 TIME STEP NUMBER 231 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.39078E-05 0.30900E-02 Friction velocity uk : 0.40047E-05 0.30898E-02 Dimensionless distance yplus : 0.26669E-04 0.20556E-01 Friction thermal sca. tstar : -0.15345E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.18731E-04 0.14437E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.39078E-05 0.30900E-02 Friction velocity uk : 0.40047E-05 0.30898E-02 Dimensionless distance yplus : 0.26669E-04 0.20556E-01 Friction thermal sca. tstar : -0.15345E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.18731E-04 0.14437E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.44964E-08 4 0.66796E-06 0.38330E-11 0.28872E+01 c Velocity[X] 0.41217E-30 c Velocity[Y] 0.19165E-11 c Velocity[Z] 0.19165E-11 c Pressure 0.57152E-13 23 0.86673E-08 0.45234E-06 0.35904E+01 c k 0.95155E-06 2 0.20601E-06 0.90831E-07 0.34302E+01 c omega 0.13153E+02 1 0.98619E-08 0.77088E+01 0.14454E-01 c TempK 0.94358E+02 1 0.46715E-06 0.11813E+00 0.38231E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.7513e-13 1.4617e-13 -1.6869e-17 -4.2421e-18 v Velocity[Y] -0.00019067 0.00019016 -8.557e-10 -3.7835e-12 v Velocity[Z] -0.00019017 0.00019068 8.0617e-10 -8.5602e-13 v ǁVelocityǁ 1.4067e-10 0.0002225 1.2924e-05 6.6825e-06 v Pressure -0.00038526 0.012196 0.00056753 9.4131e-21 v k 1.5277e-08 0.0032918 0.0022975 0.002752 v omega 33.878 1.0313e+05 2680.4 516.95 v TempK 288 341.37 292.13 289.62 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.8027e-13 0.00011005 7.4297e-05 9.2836e-05 v CourantNb 9.0256e-10 0.00035264 1.9409e-05 9.5843e-06 v FourierNb 0.14639 0.62811 0.22968 0.19492 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.8896 4.8896 0.0003692 -2.5393e-07 v volume_forces[Z] -4.8896 4.8896 -0.00036908 3.1709e-07 v ǁvolume_forcesǁ 5.1475e-09 4.8916 0.37549 0.14657 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.36 289.77 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.020556 7.0007e-05 3.9763e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14639 0.62811 0.2297 0.19493 INSTANT 0.223416000E+00 TIME STEP NUMBER 232 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.38530E-05 0.30859E-02 Friction velocity uk : 0.39498E-05 0.30857E-02 Dimensionless distance yplus : 0.26304E-04 0.20529E-01 Friction thermal sca. tstar : -0.15677E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.18474E-04 0.14418E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.38530E-05 0.30859E-02 Friction velocity uk : 0.39498E-05 0.30857E-02 Dimensionless distance yplus : 0.26304E-04 0.20529E-01 Friction thermal sca. tstar : -0.15677E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.18474E-04 0.14418E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.44851E-08 4 0.66457E-06 0.38035E-11 0.28831E+01 c Velocity[X] 0.40654E-30 c Velocity[Y] 0.19018E-11 c Velocity[Z] 0.19017E-11 c Pressure 0.56750E-13 22 0.86187E-08 0.44911E-06 0.35747E+01 c k 0.94856E-06 2 0.20438E-06 0.89747E-07 0.34206E+01 c omega 0.13153E+02 1 0.97991E-08 0.76271E+01 0.14378E-01 c TempK 0.94359E+02 1 0.46450E-06 0.11739E+00 0.38112E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.7467e-13 1.4576e-13 -1.6831e-17 -4.2329e-18 v Velocity[Y] -0.00019026 0.00018973 -8.5823e-10 -3.7658e-12 v Velocity[Z] -0.00018974 0.00019027 8.0824e-10 -8.6055e-13 v ǁVelocityǁ 1.3898e-10 0.00022192 1.2895e-05 6.67e-06 v Pressure -0.00038698 0.012223 0.00056932 1.2355e-20 v k 1.5127e-08 0.00328 0.0022894 0.002743 v omega 33.788 1.0313e+05 2680.3 516.87 v TempK 288 341.37 292.14 289.62 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.785e-13 0.00010995 7.4236e-05 9.2777e-05 v CourantNb 9.0664e-10 0.00035177 1.9361e-05 9.5621e-06 v FourierNb 0.14636 0.62811 0.2295 0.19478 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.8899 4.8899 0.00036973 -2.5507e-07 v volume_forces[Z] -4.8899 4.8899 -0.00036961 3.1842e-07 v ǁvolume_forcesǁ 5.0851e-09 4.8919 0.37602 0.14689 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.36 289.77 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.020529 6.9923e-05 3.9714e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14636 0.62811 0.22952 0.19479 INSTANT 0.224379000E+00 TIME STEP NUMBER 233 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.37973E-05 0.30819E-02 Friction velocity uk : 0.38941E-05 0.30817E-02 Dimensionless distance yplus : 0.25933E-04 0.20502E-01 Friction thermal sca. tstar : -0.16030E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.18213E-04 0.14400E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.37973E-05 0.30819E-02 Friction velocity uk : 0.38941E-05 0.30817E-02 Dimensionless distance yplus : 0.25933E-04 0.20502E-01 Friction thermal sca. tstar : -0.16030E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.18213E-04 0.14400E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.44738E-08 4 0.66123E-06 0.37738E-11 0.28788E+01 c Velocity[X] 0.40097E-30 c Velocity[Y] 0.18869E-11 c Velocity[Z] 0.18869E-11 c Pressure 0.56353E-13 22 0.85672E-08 0.44594E-06 0.35591E+01 c k 0.94558E-06 2 0.20277E-06 0.88680E-07 0.34112E+01 c omega 0.13153E+02 1 0.97368E-08 0.75466E+01 0.14301E-01 c TempK 0.94359E+02 1 0.46188E-06 0.11667E+00 0.37994E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.7421e-13 1.4536e-13 -1.6793e-17 -4.2237e-18 v Velocity[Y] -0.00018986 0.0001893 -8.6075e-10 -3.7467e-12 v Velocity[Z] -0.00018931 0.00018986 8.1029e-10 -8.6118e-13 v ǁVelocityǁ 1.3731e-10 0.00022133 1.2866e-05 6.6576e-06 v Pressure -0.00038869 0.01225 0.00057111 3.574e-20 v k 1.498e-08 0.0032682 0.0022814 0.0027341 v omega 33.698 1.0313e+05 2680.2 516.79 v TempK 288 341.38 292.14 289.63 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.7675e-13 0.00010986 7.4175e-05 9.2719e-05 v CourantNb 9.1071e-10 0.00035091 1.9314e-05 9.5401e-06 v FourierNb 0.14633 0.62811 0.22932 0.19465 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.8902 4.8902 0.00037025 -2.562e-07 v volume_forces[Z] -4.8902 4.8902 -0.00037013 3.1974e-07 v ǁvolume_forcesǁ 5.0241e-09 4.8922 0.37655 0.14721 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.37 289.77 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.020502 6.984e-05 3.9665e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14634 0.62811 0.22934 0.19466 INSTANT 0.225342000E+00 TIME STEP NUMBER 234 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.37401E-05 0.30779E-02 Friction velocity uk : 0.38369E-05 0.30776E-02 Dimensionless distance yplus : 0.25552E-04 0.20476E-01 Friction thermal sca. tstar : -0.16407E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.17946E-04 0.14381E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.37401E-05 0.30779E-02 Friction velocity uk : 0.38369E-05 0.30776E-02 Dimensionless distance yplus : 0.25552E-04 0.20476E-01 Friction thermal sca. tstar : -0.16407E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.17946E-04 0.14381E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.44626E-08 4 0.65790E-06 0.37438E-11 0.28744E+01 c Velocity[X] 0.39546E-30 c Velocity[Y] 0.18719E-11 c Velocity[Z] 0.18719E-11 c Pressure 0.55970E-13 22 0.85147E-08 0.44288E-06 0.35436E+01 c k 0.94263E-06 2 0.20118E-06 0.87627E-07 0.34017E+01 c omega 0.13153E+02 1 0.96752E-08 0.74671E+01 0.14226E-01 c TempK 0.94360E+02 1 0.45929E-06 0.11596E+00 0.37877E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.7376e-13 1.4495e-13 -1.6755e-17 -4.2147e-18 v Velocity[Y] -0.00018945 0.00018888 -8.6325e-10 -3.7276e-12 v Velocity[Z] -0.00018888 0.00018945 8.1233e-10 -8.6141e-13 v ǁVelocityǁ 1.3568e-10 0.00022076 1.2838e-05 6.6454e-06 v Pressure -0.00039041 0.012277 0.0005729 -3.4318e-20 v k 1.4835e-08 0.0032565 0.0022734 0.0027252 v omega 33.608 1.0313e+05 2680.1 516.7 v TempK 288 341.38 292.15 289.63 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.7503e-13 0.00010976 7.4114e-05 9.2661e-05 v CourantNb 9.1478e-10 0.00035005 1.9267e-05 9.5181e-06 v FourierNb 0.14631 0.62811 0.22914 0.19451 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.8905 4.8905 0.00037078 -2.5733e-07 v volume_forces[Z] -4.8905 4.8905 -0.00037066 3.2106e-07 v ǁvolume_forcesǁ 4.9638e-09 4.8925 0.37708 0.14753 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.37 289.78 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.020476 6.9757e-05 3.9616e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14631 0.62811 0.22915 0.19452 INSTANT 0.226305000E+00 TIME STEP NUMBER 235 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.36818E-05 0.30739E-02 Friction velocity uk : 0.37786E-05 0.30736E-02 Dimensionless distance yplus : 0.25164E-04 0.20449E-01 Friction thermal sca. tstar : -0.16812E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.17674E-04 0.14362E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.36818E-05 0.30739E-02 Friction velocity uk : 0.37786E-05 0.30736E-02 Dimensionless distance yplus : 0.25164E-04 0.20449E-01 Friction thermal sca. tstar : -0.16812E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.17674E-04 0.14362E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.44515E-08 4 0.65451E-06 0.37136E-11 0.28697E+01 c Velocity[X] 0.39001E-30 c Velocity[Y] 0.18568E-11 c Velocity[Z] 0.18568E-11 c Pressure 0.55573E-13 22 0.84635E-08 0.43970E-06 0.35283E+01 c k 0.93969E-06 2 0.19962E-06 0.86591E-07 0.33924E+01 c omega 0.13153E+02 1 0.96140E-08 0.73886E+01 0.14151E-01 c TempK 0.94361E+02 1 0.45671E-06 0.11525E+00 0.37761E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.7332e-13 1.4455e-13 -1.6718e-17 -4.2057e-18 v Velocity[Y] -0.00018905 0.00018846 -8.6574e-10 -3.709e-12 v Velocity[Z] -0.00018846 0.00018905 8.1435e-10 -8.6238e-13 v ǁVelocityǁ 1.3408e-10 0.00022018 1.281e-05 6.6331e-06 v Pressure -0.00039212 0.012304 0.00057468 -4.3266e-20 v k 1.4691e-08 0.0032448 0.0022655 0.0027163 v omega 33.519 1.0313e+05 2680.1 516.62 v TempK 288 341.38 292.15 289.63 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.7333e-13 0.00010966 7.4054e-05 9.2603e-05 v CourantNb 9.1886e-10 0.0003492 1.922e-05 9.4963e-06 v FourierNb 0.14628 0.62811 0.22896 0.19438 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.8907 4.8908 0.0003713 -2.5845e-07 v volume_forces[Z] -4.8907 4.8908 -0.00037118 3.2237e-07 v ǁvolume_forcesǁ 4.9048e-09 4.8928 0.37761 0.14785 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.38 289.78 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.020449 6.9674e-05 3.9568e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14628 0.62811 0.22897 0.19438 INSTANT 0.227268000E+00 TIME STEP NUMBER 236 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.36222E-05 0.30699E-02 Friction velocity uk : 0.37192E-05 0.30697E-02 Dimensionless distance yplus : 0.24768E-04 0.20423E-01 Friction thermal sca. tstar : -0.17250E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.17395E-04 0.14344E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.36222E-05 0.30699E-02 Friction velocity uk : 0.37192E-05 0.30697E-02 Dimensionless distance yplus : 0.24768E-04 0.20423E-01 Friction thermal sca. tstar : -0.17250E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.17395E-04 0.14344E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.44404E-08 4 0.65979E-06 0.36832E-11 0.28648E+01 c Velocity[X] 0.38462E-30 c Velocity[Y] 0.18416E-11 c Velocity[Z] 0.18416E-11 c Pressure 0.55210E-13 22 0.84095E-08 0.43679E-06 0.35131E+01 c k 0.93676E-06 2 0.19808E-06 0.85569E-07 0.33831E+01 c omega 0.13153E+02 1 0.95534E-08 0.73111E+01 0.14076E-01 c TempK 0.94362E+02 1 0.45417E-06 0.11455E+00 0.37645E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.7287e-13 1.4416e-13 -1.6681e-17 -4.1968e-18 v Velocity[Y] -0.00018865 0.00018804 -8.6821e-10 -3.6904e-12 v Velocity[Z] -0.00018804 0.00018865 8.1636e-10 -8.6321e-13 v ǁVelocityǁ 1.3252e-10 0.00021961 1.2782e-05 6.621e-06 v Pressure -0.00039384 0.012331 0.00057646 3.1867e-21 v k 1.4549e-08 0.0032332 0.0022576 0.0027076 v omega 33.431 1.0313e+05 2680 516.54 v TempK 288 341.39 292.16 289.64 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.7165e-13 0.00010956 7.3994e-05 9.2545e-05 v CourantNb 9.2293e-10 0.00034834 1.9173e-05 9.4746e-06 v FourierNb 0.14625 0.62811 0.22878 0.19424 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.891 4.8911 0.00037182 -2.5957e-07 v volume_forces[Z] -4.891 4.8911 -0.0003717 3.2367e-07 v ǁvolume_forcesǁ 4.847e-09 4.8931 0.37813 0.14817 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.38 289.78 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.020423 6.9592e-05 3.9519e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14626 0.62811 0.2288 0.19425 INSTANT 0.228231000E+00 TIME STEP NUMBER 237 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.35612E-05 0.30659E-02 Friction velocity uk : 0.36584E-05 0.30657E-02 Dimensionless distance yplus : 0.24363E-04 0.20396E-01 Friction thermal sca. tstar : -0.17725E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.17111E-04 0.14325E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.35612E-05 0.30659E-02 Friction velocity uk : 0.36584E-05 0.30657E-02 Dimensionless distance yplus : 0.24363E-04 0.20396E-01 Friction thermal sca. tstar : -0.17725E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.17111E-04 0.14325E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.44294E-08 4 0.64784E-06 0.36525E-11 0.28597E+01 c Velocity[X] 0.37930E-30 c Velocity[Y] 0.18263E-11 c Velocity[Z] 0.18262E-11 c Pressure 0.54830E-13 22 0.83581E-08 0.43375E-06 0.34981E+01 c k 0.93386E-06 2 0.19656E-06 0.84562E-07 0.33738E+01 c omega 0.13153E+02 1 0.94933E-08 0.72346E+01 0.14003E-01 c TempK 0.94362E+02 1 0.45164E-06 0.11385E+00 0.37530E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.7243e-13 1.4376e-13 -1.6644e-17 -4.1879e-18 v Velocity[Y] -0.00018825 0.00018762 -8.7067e-10 -3.672e-12 v Velocity[Z] -0.00018762 0.00018825 8.1835e-10 -8.6401e-13 v ǁVelocityǁ 1.31e-10 0.00021904 1.2754e-05 6.609e-06 v Pressure -0.00039556 0.012358 0.00057824 4.1182e-21 v k 1.4409e-08 0.0032217 0.0022497 0.0026988 v omega 33.343 1.0313e+05 2679.9 516.46 v TempK 288 341.39 292.17 289.64 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.7e-13 0.00010946 7.3934e-05 9.2487e-05 v CourantNb 9.2701e-10 0.0003475 1.9127e-05 9.4531e-06 v FourierNb 0.14623 0.62811 0.2286 0.19411 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.8913 4.8914 0.00037235 -2.6068e-07 v volume_forces[Z] -4.8913 4.8914 -0.00037222 3.2497e-07 v ǁvolume_forcesǁ 4.7906e-09 4.8933 0.37866 0.14848 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.39 289.79 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.020396 6.9511e-05 3.9471e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14623 0.62811 0.22862 0.19412 INSTANT 0.229194000E+00 TIME STEP NUMBER 238 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.34988E-05 0.30620E-02 Friction velocity uk : 0.35963E-05 0.30618E-02 Dimensionless distance yplus : 0.23950E-04 0.20370E-01 Friction thermal sca. tstar : -0.18242E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.16821E-04 0.14307E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.34988E-05 0.30620E-02 Friction velocity uk : 0.35963E-05 0.30618E-02 Dimensionless distance yplus : 0.23950E-04 0.20370E-01 Friction thermal sca. tstar : -0.18242E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.16821E-04 0.14307E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.44185E-08 4 0.64460E-06 0.36217E-11 0.28545E+01 c Velocity[X] 0.37404E-30 c Velocity[Y] 0.18109E-11 c Velocity[Z] 0.18108E-11 c Pressure 0.54552E-13 22 0.83125E-08 0.43152E-06 0.34832E+01 c k 0.93097E-06 2 0.19506E-06 0.83570E-07 0.33646E+01 c omega 0.13153E+02 1 0.94338E-08 0.71591E+01 0.13929E-01 c TempK 0.94363E+02 1 0.44914E-06 0.11317E+00 0.37417E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.7199e-13 1.4337e-13 -1.6607e-17 -4.1792e-18 v Velocity[Y] -0.00018786 0.0001872 -8.7311e-10 -3.6536e-12 v Velocity[Z] -0.00018721 0.00018786 8.2032e-10 -8.6499e-13 v ǁVelocityǁ 1.2952e-10 0.00021847 1.2727e-05 6.5971e-06 v Pressure -0.00039727 0.012385 0.00058001 2.4513e-22 v k 1.4271e-08 0.0032102 0.0022419 0.0026901 v omega 33.255 1.0313e+05 2679.9 516.38 v TempK 288 341.39 292.17 289.64 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.6836e-13 0.00010936 7.3874e-05 9.243e-05 v CourantNb 9.3108e-10 0.00034665 1.9081e-05 9.4316e-06 v FourierNb 0.1462 0.62811 0.22842 0.19397 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.8916 4.8917 0.00037286 -2.6179e-07 v volume_forces[Z] -4.8916 4.8917 -0.00037274 3.2626e-07 v ǁvolume_forcesǁ 4.7357e-09 4.8936 0.37918 0.1488 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.4 289.79 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.02037 6.9429e-05 3.9424e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.1462 0.62811 0.22844 0.19398 INSTANT 0.230157000E+00 TIME STEP NUMBER 239 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.34350E-05 0.30581E-02 Friction velocity uk : 0.35328E-05 0.30578E-02 Dimensionless distance yplus : 0.23527E-04 0.20344E-01 Friction thermal sca. tstar : -0.18808E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.16524E-04 0.14288E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.34350E-05 0.30581E-02 Friction velocity uk : 0.35328E-05 0.30578E-02 Dimensionless distance yplus : 0.23527E-04 0.20344E-01 Friction thermal sca. tstar : -0.18808E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.16524E-04 0.14288E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.44076E-08 4 0.64126E-06 0.35907E-11 0.28490E+01 c Velocity[X] 0.36885E-30 c Velocity[Y] 0.17954E-11 c Velocity[Z] 0.17953E-11 c Pressure 0.54024E-13 22 0.82541E-08 0.42730E-06 0.34683E+01 c k 0.92809E-06 2 0.19358E-06 0.82592E-07 0.33555E+01 c omega 0.13153E+02 1 0.93748E-08 0.70846E+01 0.13857E-01 c TempK 0.94364E+02 1 0.44666E-06 0.11249E+00 0.37303E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.7155e-13 1.4298e-13 -1.6571e-17 -4.1705e-18 v Velocity[Y] -0.00018746 0.00018679 -8.7553e-10 -3.6349e-12 v Velocity[Z] -0.0001868 0.00018747 8.2227e-10 -8.6563e-13 v ǁVelocityǁ 1.2809e-10 0.00021791 1.2699e-05 6.5852e-06 v Pressure -0.00039899 0.012411 0.00058178 -3.0838e-20 v k 1.4135e-08 0.0031988 0.0022342 0.0026815 v omega 33.168 1.0313e+05 2679.8 516.3 v TempK 288 341.4 292.18 289.65 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.6675e-13 0.00010926 7.3814e-05 9.2373e-05 v CourantNb 9.3516e-10 0.00034581 1.9035e-05 9.4103e-06 v FourierNb 0.14617 0.62811 0.22825 0.19384 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.8919 4.8919 0.00037338 -2.629e-07 v volume_forces[Z] -4.8919 4.8919 -0.00037326 3.2755e-07 v ǁvolume_forcesǁ 4.6823e-09 4.8939 0.3797 0.14912 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.4 289.79 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.020344 6.9349e-05 3.9376e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14618 0.62811 0.22826 0.19385 INSTANT 0.231120000E+00 TIME STEP NUMBER 240 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.33695E-05 0.30542E-02 Friction velocity uk : 0.34677E-05 0.30540E-02 Dimensionless distance yplus : 0.23094E-04 0.20318E-01 Friction thermal sca. tstar : -0.19429E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.16219E-04 0.14270E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.33695E-05 0.30542E-02 Friction velocity uk : 0.34677E-05 0.30540E-02 Dimensionless distance yplus : 0.23094E-04 0.20318E-01 Friction thermal sca. tstar : -0.19429E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.16219E-04 0.14270E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.43968E-08 4 0.63800E-06 0.35596E-11 0.28434E+01 c Velocity[X] 0.36371E-30 c Velocity[Y] 0.17798E-11 c Velocity[Z] 0.17798E-11 c Pressure 0.53650E-13 22 0.82017E-08 0.42431E-06 0.34536E+01 c k 0.92524E-06 2 0.19212E-06 0.81628E-07 0.33463E+01 c omega 0.13153E+02 1 0.93163E-08 0.70111E+01 0.13785E-01 c TempK 0.94365E+02 1 0.44421E-06 0.11181E+00 0.37191E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.7112e-13 1.4259e-13 -1.6535e-17 -4.1618e-18 v Velocity[Y] -0.00018707 0.00018638 -8.7794e-10 -3.6166e-12 v Velocity[Z] -0.00018639 0.00018708 8.2421e-10 -8.6661e-13 v ǁVelocityǁ 1.2671e-10 0.00021735 1.2672e-05 6.5735e-06 v Pressure -0.0004007 0.012438 0.00058355 6.1675e-20 v k 1.4e-08 0.0031875 0.0022265 0.0026729 v omega 33.081 1.0313e+05 2679.7 516.22 v TempK 288 341.4 292.18 289.65 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.6516e-13 0.00010916 7.3755e-05 9.2316e-05 v CourantNb 9.3924e-10 0.00034498 1.8989e-05 9.3891e-06 v FourierNb 0.14615 0.62811 0.22807 0.19371 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.8922 4.8922 0.0003739 -2.6399e-07 v volume_forces[Z] -4.8922 4.8922 -0.00037377 3.2883e-07 v ǁvolume_forcesǁ 4.6305e-09 4.8942 0.38022 0.14943 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.41 289.8 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.020318 6.9269e-05 3.9329e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14615 0.62811 0.22809 0.19372 INSTANT 0.232083000E+00 TIME STEP NUMBER 241 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.33024E-05 0.30503E-02 Friction velocity uk : 0.34011E-05 0.30501E-02 Dimensionless distance yplus : 0.22650E-04 0.20292E-01 Friction thermal sca. tstar : -0.20117E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.15908E-04 0.14252E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.33024E-05 0.30503E-02 Friction velocity uk : 0.34011E-05 0.30501E-02 Dimensionless distance yplus : 0.22650E-04 0.20292E-01 Friction thermal sca. tstar : -0.20117E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.15908E-04 0.14252E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.43861E-08 4 0.63479E-06 0.35283E-11 0.28376E+01 c Velocity[X] 0.35864E-30 c Velocity[Y] 0.17642E-11 c Velocity[Z] 0.17641E-11 c Pressure 0.53364E-13 22 0.81520E-08 0.42202E-06 0.34391E+01 c k 0.92240E-06 2 0.19068E-06 0.80679E-07 0.33373E+01 c omega 0.13153E+02 1 0.92583E-08 0.69384E+01 0.13713E-01 c TempK 0.94365E+02 1 0.44177E-06 0.11114E+00 0.37080E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.7069e-13 1.4221e-13 -1.65e-17 -4.1533e-18 v Velocity[Y] -0.00018669 0.00018597 -8.8033e-10 -3.5985e-12 v Velocity[Z] -0.00018598 0.00018669 8.2613e-10 -8.6752e-13 v ǁVelocityǁ 1.2537e-10 0.00021679 1.2645e-05 6.5618e-06 v Pressure -0.00040242 0.012465 0.00058531 -5.2458e-21 v k 1.3868e-08 0.0031762 0.0022189 0.0026644 v omega 32.995 1.0313e+05 2679.7 516.14 v TempK 288 341.4 292.19 289.66 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.6359e-13 0.00010907 7.3696e-05 9.2259e-05 v CourantNb 9.4332e-10 0.00034414 1.8944e-05 9.3681e-06 v FourierNb 0.14612 0.62811 0.2279 0.19358 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.8924 4.8925 0.00037441 -2.6509e-07 v volume_forces[Z] -4.8924 4.8925 -0.00037429 3.301e-07 v ǁvolume_forcesǁ 4.5804e-09 4.8945 0.38074 0.14975 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.41 289.8 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.020292 6.9189e-05 3.9282e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14612 0.62811 0.22792 0.19359 INSTANT 0.233046000E+00 TIME STEP NUMBER 242 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.32335E-05 0.30465E-02 Friction velocity uk : 0.33329E-05 0.30462E-02 Dimensionless distance yplus : 0.22195E-04 0.20267E-01 Friction thermal sca. tstar : -0.20885E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.15589E-04 0.14234E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.32335E-05 0.30465E-02 Friction velocity uk : 0.33329E-05 0.30462E-02 Dimensionless distance yplus : 0.22195E-04 0.20267E-01 Friction thermal sca. tstar : -0.20885E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.15589E-04 0.14234E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.43754E-08 4 0.63150E-06 0.34969E-11 0.28316E+01 c Velocity[X] 0.35363E-30 c Velocity[Y] 0.17485E-11 c Velocity[Z] 0.17484E-11 c Pressure 0.52890E-13 22 0.80986E-08 0.41824E-06 0.34246E+01 c k 0.91957E-06 2 0.18926E-06 0.79742E-07 0.33283E+01 c omega 0.13153E+02 1 0.92009E-08 0.68667E+01 0.13642E-01 c TempK 0.94366E+02 1 0.43936E-06 0.11048E+00 0.36969E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.7026e-13 1.4183e-13 -1.6464e-17 -4.1448e-18 v Velocity[Y] -0.0001863 0.00018557 -8.8271e-10 -3.5805e-12 v Velocity[Z] -0.00018557 0.0001863 8.2804e-10 -8.6834e-13 v ǁVelocityǁ 1.2409e-10 0.00021624 1.2618e-05 6.5502e-06 v Pressure -0.00040413 0.012491 0.00058707 3.7064e-20 v k 1.3737e-08 0.003165 0.0022113 0.0026559 v omega 32.909 1.0313e+05 2679.6 516.06 v TempK 288 341.41 292.19 289.66 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.6203e-13 0.00010897 7.3637e-05 9.2202e-05 v CourantNb 9.474e-10 0.00034332 1.8899e-05 9.3472e-06 v FourierNb 0.14609 0.62811 0.22772 0.19345 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.8927 4.8928 0.00037492 -2.6618e-07 v volume_forces[Z] -4.8927 4.8928 -0.0003748 3.3137e-07 v ǁvolume_forcesǁ 4.5322e-09 4.8947 0.38126 0.15006 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.42 289.8 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.020267 6.911e-05 3.9235e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14609 0.62811 0.22774 0.19346 INSTANT 0.234009000E+00 TIME STEP NUMBER 243 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.31627E-05 0.30426E-02 Friction velocity uk : 0.32628E-05 0.30424E-02 Dimensionless distance yplus : 0.21729E-04 0.20241E-01 Friction thermal sca. tstar : -0.21747E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.15261E-04 0.14216E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.31627E-05 0.30426E-02 Friction velocity uk : 0.32628E-05 0.30424E-02 Dimensionless distance yplus : 0.21729E-04 0.20241E-01 Friction thermal sca. tstar : -0.21747E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.15261E-04 0.14216E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.43648E-08 4 0.62849E-06 0.34654E-11 0.28255E+01 c Velocity[X] 0.34865E-30 c Velocity[Y] 0.17327E-11 c Velocity[Z] 0.17327E-11 c Pressure 0.52494E-13 23 0.95665E-08 0.41508E-06 0.34103E+01 c k 0.91676E-06 2 0.18787E-06 0.78819E-07 0.33193E+01 c omega 0.13153E+02 1 0.91439E-08 0.67959E+01 0.13572E-01 c TempK 0.94367E+02 1 0.43697E-06 0.10983E+00 0.36859E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.6984e-13 1.4145e-13 -1.6429e-17 -4.1364e-18 v Velocity[Y] -0.00018592 0.00018517 -8.877e-10 -6.0733e-12 v Velocity[Z] -0.00018517 0.00018592 8.2906e-10 -1.7354e-12 v ǁVelocityǁ 1.2265e-10 0.00021569 1.2591e-05 6.5388e-06 v Pressure -0.00040585 0.012518 0.00058883 2.9367e-20 v k 1.3607e-08 0.0031539 0.0022037 0.0026475 v omega 32.824 1.0313e+05 2679.6 515.98 v TempK 288 341.41 292.2 289.66 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.605e-13 0.00010887 7.3579e-05 9.2146e-05 v CourantNb 9.5023e-10 0.00034249 1.8854e-05 9.3264e-06 v FourierNb 0.14607 0.62811 0.22755 0.19332 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.893 4.8931 0.00037543 -2.6726e-07 v volume_forces[Z] -4.893 4.8931 -0.00037531 3.3263e-07 v ǁvolume_forcesǁ 4.4859e-09 4.895 0.38177 0.15038 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.42 289.81 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.020241 6.9031e-05 3.9189e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14607 0.62811 0.22757 0.19333 INSTANT 0.234972000E+00 TIME STEP NUMBER 244 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.30874E-05 0.30388E-02 Friction velocity uk : 0.31884E-05 0.30386E-02 Dimensionless distance yplus : 0.21233E-04 0.20216E-01 Friction thermal sca. tstar : -0.22727E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.14913E-04 0.14198E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.30874E-05 0.30388E-02 Friction velocity uk : 0.31884E-05 0.30386E-02 Dimensionless distance yplus : 0.21233E-04 0.20216E-01 Friction thermal sca. tstar : -0.22727E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.14913E-04 0.14198E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.43542E-08 4 0.63817E-06 0.34338E-11 0.28192E+01 c Velocity[X] 0.34379E-30 c Velocity[Y] 0.17169E-11 c Velocity[Z] 0.17169E-11 c Pressure 0.52131E-13 23 0.95108E-08 0.41218E-06 0.33961E+01 c k 0.91397E-06 2 0.18649E-06 0.77909E-07 0.33104E+01 c omega 0.13153E+02 1 0.90875E-08 0.67261E+01 0.13502E-01 c TempK 0.94367E+02 1 0.43461E-06 0.10918E+00 0.36750E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.6941e-13 1.4107e-13 -1.6395e-17 -4.128e-18 v Velocity[Y] -0.00018554 0.00018477 -8.9003e-10 -6.0705e-12 v Velocity[Z] -0.00018477 0.00018554 8.3094e-10 -1.7293e-12 v ǁVelocityǁ 1.2001e-10 0.00021514 1.2565e-05 6.5274e-06 v Pressure -0.00040756 0.012544 0.00059059 8.9718e-21 v k 1.3479e-08 0.0031428 0.0021962 0.0026391 v omega 32.739 1.0313e+05 2679.5 515.91 v TempK 288 341.41 292.21 289.67 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.5899e-13 0.00010877 7.3521e-05 9.209e-05 v CourantNb 9.5408e-10 0.00034167 1.881e-05 9.3058e-06 v FourierNb 0.14604 0.62811 0.22738 0.19319 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.8933 4.8933 0.00037594 -2.6837e-07 v volume_forces[Z] -4.8933 4.8933 -0.00037582 3.3398e-07 v ǁvolume_forcesǁ 4.4338e-09 4.8953 0.38229 0.15069 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.43 289.81 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.020216 6.8953e-05 3.9143e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14604 0.62811 0.2274 0.1932 INSTANT 0.235935000E+00 TIME STEP NUMBER 245 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.29390E-05 0.30350E-02 Friction velocity uk : 0.30434E-05 0.30348E-02 Dimensionless distance yplus : 0.20267E-04 0.20191E-01 Friction thermal sca. tstar : -0.23853E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.14235E-04 0.14181E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.29390E-05 0.30350E-02 Friction velocity uk : 0.30434E-05 0.30348E-02 Dimensionless distance yplus : 0.20267E-04 0.20191E-01 Friction thermal sca. tstar : -0.23853E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.14235E-04 0.14181E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.43438E-08 4 0.63931E-06 0.34021E-11 0.28127E+01 c Velocity[X] 0.33897E-30 c Velocity[Y] 0.17011E-11 c Velocity[Z] 0.17010E-11 c Pressure 0.51763E-13 23 0.94489E-08 0.40924E-06 0.33819E+01 c k 0.91119E-06 2 0.18512E-06 0.77012E-07 0.33016E+01 c omega 0.13153E+02 1 0.90315E-08 0.66571E+01 0.13432E-01 c TempK 0.94368E+02 1 0.43226E-06 0.10854E+00 0.36641E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.6899e-13 1.407e-13 -1.636e-17 -4.1197e-18 v Velocity[Y] -0.00018516 0.00018437 -8.9233e-10 -6.0415e-12 v Velocity[Z] -0.00018437 0.00018516 8.328e-10 -1.7322e-12 v ǁVelocityǁ 1.1822e-10 0.0002146 1.2538e-05 6.5161e-06 v Pressure -0.00040928 0.01257 0.00059234 -2.694e-20 v k 1.3353e-08 0.0031318 0.0021887 0.0026308 v omega 32.654 1.0313e+05 2679.4 515.83 v TempK 288 341.41 292.21 289.67 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.575e-13 0.00010867 7.3462e-05 9.2034e-05 v CourantNb 9.5811e-10 0.00034086 1.8766e-05 9.2852e-06 v FourierNb 0.14601 0.62811 0.22721 0.19306 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.8935 4.8936 0.00037645 -2.6944e-07 v volume_forces[Z] -4.8935 4.8936 -0.00037633 3.3523e-07 v ǁvolume_forcesǁ 4.3384e-09 4.8955 0.3828 0.151 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.44 289.82 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.020191 6.8875e-05 3.9097e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14601 0.62811 0.22723 0.19307 INSTANT 0.236898000E+00 TIME STEP NUMBER 246 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.28179E-05 0.30313E-02 Friction velocity uk : 0.29250E-05 0.30310E-02 Dimensionless distance yplus : 0.19479E-04 0.20166E-01 Friction thermal sca. tstar : -0.25166E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.13681E-04 0.14163E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.28179E-05 0.30313E-02 Friction velocity uk : 0.29250E-05 0.30310E-02 Dimensionless distance yplus : 0.19479E-04 0.20166E-01 Friction thermal sca. tstar : -0.25166E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.13681E-04 0.14163E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.43334E-08 4 0.61888E-06 0.33704E-11 0.28061E+01 c Velocity[X] 0.33420E-30 c Velocity[Y] 0.16852E-11 c Velocity[Z] 0.16852E-11 c Pressure 0.51390E-13 23 0.93912E-08 0.40626E-06 0.33680E+01 c k 0.90843E-06 2 0.18378E-06 0.76128E-07 0.32927E+01 c omega 0.13153E+02 1 0.89760E-08 0.65889E+01 0.13363E-01 c TempK 0.94369E+02 1 0.42994E-06 0.10791E+00 0.36533E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.6858e-13 1.4032e-13 -1.6326e-17 -4.1115e-18 v Velocity[Y] -0.00018479 0.00018398 -8.9463e-10 -6.0222e-12 v Velocity[Z] -0.00018398 0.00018479 8.3465e-10 -1.7326e-12 v ǁVelocityǁ 1.1688e-10 0.00021405 1.2512e-05 6.5049e-06 v Pressure -0.00041099 0.012597 0.00059409 5.9077e-21 v k 1.3228e-08 0.0031208 0.0021813 0.0026225 v omega 32.57 1.0313e+05 2679.4 515.75 v TempK 288 341.42 292.22 289.67 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.5602e-13 0.00010857 7.3405e-05 9.1978e-05 v CourantNb 9.6214e-10 0.00034004 1.8722e-05 9.2649e-06 v FourierNb 0.14598 0.62811 0.22704 0.19293 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.8938 4.8939 0.00037696 -2.7051e-07 v volume_forces[Z] -4.8938 4.8939 -0.00037683 3.3647e-07 v ǁvolume_forcesǁ 4.2737e-09 4.8958 0.38331 0.15132 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.44 289.82 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.020166 6.8798e-05 3.9051e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14599 0.62811 0.22706 0.19294 INSTANT 0.237861000E+00 TIME STEP NUMBER 247 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.27094E-05 0.30275E-02 Friction velocity uk : 0.28189E-05 0.30273E-02 Dimensionless distance yplus : 0.18773E-04 0.20141E-01 Friction thermal sca. tstar : -0.26722E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.13185E-04 0.14146E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.27094E-05 0.30275E-02 Friction velocity uk : 0.28189E-05 0.30273E-02 Dimensionless distance yplus : 0.18773E-04 0.20141E-01 Friction thermal sca. tstar : -0.26722E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.13185E-04 0.14146E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.43230E-08 4 0.61568E-06 0.33386E-11 0.27993E+01 c Velocity[X] 0.32949E-30 c Velocity[Y] 0.16693E-11 c Velocity[Z] 0.16693E-11 c Pressure 0.51024E-13 23 0.93321E-08 0.40333E-06 0.33541E+01 c k 0.90568E-06 2 0.18246E-06 0.75256E-07 0.32840E+01 c omega 0.13153E+02 1 0.89210E-08 0.65217E+01 0.13295E-01 c TempK 0.94370E+02 1 0.42763E-06 0.10728E+00 0.36426E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.6816e-13 1.3996e-13 -1.6292e-17 -4.1034e-18 v Velocity[Y] -0.00018442 0.00018358 -8.9691e-10 -6.0025e-12 v Velocity[Z] -0.00018359 0.00018442 8.3647e-10 -1.7328e-12 v ǁVelocityǁ 1.1579e-10 0.00021352 1.2486e-05 6.4939e-06 v Pressure -0.00041271 0.012623 0.00059584 2.569e-20 v k 1.3105e-08 0.0031099 0.002174 0.0026142 v omega 32.487 1.0313e+05 2679.3 515.67 v TempK 288 341.42 292.22 289.68 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.5457e-13 0.00010848 7.3347e-05 9.1922e-05 v CourantNb 9.662e-10 0.00033923 1.8678e-05 9.2446e-06 v FourierNb 0.14596 0.62811 0.22687 0.1928 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.8941 4.8941 0.00037746 -2.7158e-07 v volume_forces[Z] -4.8941 4.8941 -0.00037734 3.3771e-07 v ǁvolume_forcesǁ 4.2252e-09 4.8961 0.38382 0.15163 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.45 289.82 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.020141 6.8721e-05 3.9006e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14596 0.62811 0.22689 0.19281 INSTANT 0.238824000E+00 TIME STEP NUMBER 248 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.26053E-05 0.30238E-02 Friction velocity uk : 0.27174E-05 0.30236E-02 Dimensionless distance yplus : 0.18097E-04 0.20116E-01 Friction thermal sca. tstar : -0.28609E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.12710E-04 0.14128E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.26053E-05 0.30238E-02 Friction velocity uk : 0.27174E-05 0.30236E-02 Dimensionless distance yplus : 0.18097E-04 0.20116E-01 Friction thermal sca. tstar : -0.28609E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.12710E-04 0.14128E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.43128E-08 4 0.61257E-06 0.33068E-11 0.27924E+01 c Velocity[X] 0.32484E-30 c Velocity[Y] 0.16534E-11 c Velocity[Z] 0.16534E-11 c Pressure 0.50653E-13 23 0.92736E-08 0.40037E-06 0.33403E+01 c k 0.90295E-06 2 0.18115E-06 0.74397E-07 0.32753E+01 c omega 0.13153E+02 1 0.88664E-08 0.64552E+01 0.13227E-01 c TempK 0.94370E+02 1 0.42535E-06 0.10666E+00 0.36320E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.6775e-13 1.3959e-13 -1.6258e-17 -4.0953e-18 v Velocity[Y] -0.00018405 0.00018319 -8.9918e-10 -5.9828e-12 v Velocity[Z] -0.0001832 0.00018405 8.3829e-10 -1.7331e-12 v ǁVelocityǁ 1.1488e-10 0.00021298 1.246e-05 6.4829e-06 v Pressure -0.00041442 0.012649 0.00059758 5.6184e-20 v k 1.2984e-08 0.0030991 0.0021666 0.002606 v omega 32.403 1.0313e+05 2679.2 515.6 v TempK 288 341.42 292.23 289.68 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.5313e-13 0.00010838 7.329e-05 9.1866e-05 v CourantNb 9.7026e-10 0.00033843 1.8635e-05 9.2246e-06 v FourierNb 0.14593 0.62811 0.2267 0.19268 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.8944 4.8944 0.00037797 -2.7264e-07 v volume_forces[Z] -4.8944 4.8944 -0.00037784 3.3895e-07 v ǁvolume_forcesǁ 4.1859e-09 4.8963 0.38432 0.15194 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.45 289.83 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.020116 6.8644e-05 3.8961e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14593 0.62811 0.22672 0.19269 INSTANT 0.239787000E+00 TIME STEP NUMBER 249 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.25020E-05 0.30201E-02 Friction velocity uk : 0.26168E-05 0.30199E-02 Dimensionless distance yplus : 0.17427E-04 0.20091E-01 Friction thermal sca. tstar : -0.30963E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.12239E-04 0.14111E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.25020E-05 0.30201E-02 Friction velocity uk : 0.26168E-05 0.30199E-02 Dimensionless distance yplus : 0.17427E-04 0.20091E-01 Friction thermal sca. tstar : -0.30963E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.12239E-04 0.14111E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.43026E-08 4 0.60946E-06 0.32750E-11 0.27853E+01 c Velocity[X] 0.32025E-30 c Velocity[Y] 0.16375E-11 c Velocity[Z] 0.16375E-11 c Pressure 0.50299E-13 23 0.92160E-08 0.39754E-06 0.33266E+01 c k 0.90023E-06 2 0.17986E-06 0.73549E-07 0.32666E+01 c omega 0.13153E+02 1 0.88124E-08 0.63896E+01 0.13160E-01 c TempK 0.94371E+02 1 0.42309E-06 0.10604E+00 0.36214E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.6734e-13 1.3922e-13 -1.6225e-17 -4.0872e-18 v Velocity[Y] -0.00018368 0.00018281 -9.0144e-10 -5.9634e-12 v Velocity[Z] -0.00018281 0.00018368 8.4008e-10 -1.7335e-12 v ǁVelocityǁ 1.1411e-10 0.00021245 1.2435e-05 6.472e-06 v Pressure -0.00041614 0.012675 0.00059932 -2.8019e-20 v k 1.2864e-08 0.0030883 0.0021594 0.0025979 v omega 32.321 1.0313e+05 2679.2 515.52 v TempK 288 341.43 292.23 289.68 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.5171e-13 0.00010828 7.3232e-05 9.1811e-05 v CourantNb 9.7433e-10 0.00033763 1.8592e-05 9.2046e-06 v FourierNb 0.1459 0.62811 0.22654 0.19255 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.8946 4.8947 0.00037847 -2.7369e-07 v volume_forces[Z] -4.8946 4.8947 -0.00037834 3.4017e-07 v ǁvolume_forcesǁ 4.153e-09 4.8966 0.38483 0.15225 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.46 289.83 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.020091 6.8568e-05 3.8916e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14591 0.62811 0.22656 0.19256 INSTANT 0.240750000E+00 TIME STEP NUMBER 250 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.23971E-05 0.30164E-02 Friction velocity uk : 0.25149E-05 0.30162E-02 Dimensionless distance yplus : 0.16748E-04 0.20067E-01 Friction thermal sca. tstar : -0.34014E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.11763E-04 0.14094E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.23971E-05 0.30164E-02 Friction velocity uk : 0.25149E-05 0.30162E-02 Dimensionless distance yplus : 0.16748E-04 0.20067E-01 Friction thermal sca. tstar : -0.34014E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.11763E-04 0.14094E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.42924E-08 4 0.60635E-06 0.32432E-11 0.27781E+01 c Velocity[X] 0.31571E-30 c Velocity[Y] 0.16216E-11 c Velocity[Z] 0.16216E-11 c Pressure 0.49933E-13 23 0.91577E-08 0.39462E-06 0.33131E+01 c k 0.89753E-06 2 0.17858E-06 0.72714E-07 0.32580E+01 c omega 0.13153E+02 1 0.87588E-08 0.63249E+01 0.13093E-01 c TempK 0.94372E+02 1 0.42084E-06 0.10543E+00 0.36109E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.6694e-13 1.3886e-13 -1.6192e-17 -4.0793e-18 v Velocity[Y] -0.00018331 0.00018242 -9.0368e-10 -5.9439e-12 v Velocity[Z] -0.00018242 0.00018332 8.4186e-10 -1.734e-12 v ǁVelocityǁ 1.1346e-10 0.00021192 1.2409e-05 6.4612e-06 v Pressure -0.00041785 0.012701 0.00060106 1.0394e-20 v k 1.2745e-08 0.0030775 0.0021521 0.0025898 v omega 32.238 1.0313e+05 2679.1 515.45 v TempK 288 341.43 292.24 289.69 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.5031e-13 0.00010818 7.3175e-05 9.1756e-05 v CourantNb 9.7841e-10 0.00033683 1.8549e-05 9.1848e-06 v FourierNb 0.14588 0.62811 0.22637 0.19242 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.8949 4.8949 0.00037897 -2.7474e-07 v volume_forces[Z] -4.8949 4.895 -0.00037884 3.414e-07 v ǁvolume_forcesǁ 4.1252e-09 4.8969 0.38533 0.15256 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.46 289.83 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.020067 6.8492e-05 3.8872e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14588 0.62811 0.22639 0.19243 INSTANT 0.241713000E+00 TIME STEP NUMBER 251 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.22891E-05 0.30127E-02 Friction velocity uk : 0.24104E-05 0.30125E-02 Dimensionless distance yplus : 0.16052E-04 0.20043E-01 Friction thermal sca. tstar : -0.38193E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.11274E-04 0.14077E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.22891E-05 0.30127E-02 Friction velocity uk : 0.24104E-05 0.30125E-02 Dimensionless distance yplus : 0.16052E-04 0.20043E-01 Friction thermal sca. tstar : -0.38193E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.11274E-04 0.14077E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.42824E-08 4 0.62136E-06 0.32113E-11 0.27707E+01 c Velocity[X] 0.31124E-30 c Velocity[Y] 0.16057E-11 c Velocity[Z] 0.16057E-11 c Pressure 0.49590E-13 23 0.91011E-08 0.39188E-06 0.32996E+01 c k 0.89484E-06 2 0.17733E-06 0.71890E-07 0.32494E+01 c omega 0.13153E+02 1 0.87056E-08 0.62609E+01 0.13026E-01 c TempK 0.94373E+02 1 0.41862E-06 0.10482E+00 0.36005E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.6653e-13 1.385e-13 -1.6159e-17 -4.0714e-18 v Velocity[Y] -0.00018295 0.00018204 -9.059e-10 -5.9246e-12 v Velocity[Z] -0.00018204 0.00018295 8.4362e-10 -1.7345e-12 v ǁVelocityǁ 1.1292e-10 0.00021139 1.2384e-05 6.4505e-06 v Pressure -0.00041957 0.012727 0.0006028 1.76e-20 v k 1.2628e-08 0.0030669 0.0021449 0.0025817 v omega 32.156 1.0313e+05 2679 515.37 v TempK 288 341.43 292.24 289.69 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.4892e-13 0.00010808 7.3119e-05 9.1701e-05 v CourantNb 9.8249e-10 0.00033604 1.8507e-05 9.1651e-06 v FourierNb 0.14585 0.62811 0.22621 0.1923 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.8952 4.8952 0.00037947 -2.7579e-07 v volume_forces[Z] -4.8952 4.8952 -0.00037934 3.4261e-07 v ǁvolume_forcesǁ 4.1017e-09 4.8971 0.38584 0.15287 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.47 289.84 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.020043 6.8417e-05 3.8827e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14585 0.62811 0.22622 0.19231 INSTANT 0.242676000E+00 TIME STEP NUMBER 252 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.21768E-05 0.30091E-02 Friction velocity uk : 0.23021E-05 0.30089E-02 Dimensionless distance yplus : 0.15331E-04 0.20018E-01 Friction thermal sca. tstar : -0.44427E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.10767E-04 0.14060E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.21768E-05 0.30091E-02 Friction velocity uk : 0.23021E-05 0.30089E-02 Dimensionless distance yplus : 0.15331E-04 0.20018E-01 Friction thermal sca. tstar : -0.44427E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.10767E-04 0.14060E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.42724E-08 4 0.70574E-06 0.31795E-11 0.27632E+01 c Velocity[X] 0.30682E-30 c Velocity[Y] 0.15898E-11 c Velocity[Z] 0.15898E-11 c Pressure 0.49322E-13 23 0.90461E-08 0.38974E-06 0.32863E+01 c k 0.89217E-06 2 0.17609E-06 0.71077E-07 0.32409E+01 c omega 0.13153E+02 1 0.86529E-08 0.61977E+01 0.12960E-01 c TempK 0.94373E+02 1 0.41642E-06 0.10423E+00 0.35902E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.6613e-13 1.3815e-13 -1.6126e-17 -4.0636e-18 v Velocity[Y] -0.00018259 0.00018166 -9.0811e-10 -5.9056e-12 v Velocity[Z] -0.00018166 0.00018259 8.4537e-10 -1.7353e-12 v ǁVelocityǁ 1.1249e-10 0.00021087 1.2359e-05 6.4399e-06 v Pressure -0.00042129 0.012753 0.00060453 -1.0509e-19 v k 1.2513e-08 0.0030563 0.0021378 0.0025737 v omega 32.075 1.0313e+05 2679 515.3 v TempK 288 341.43 292.25 289.69 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.4755e-13 0.00010799 7.3062e-05 9.1646e-05 v CourantNb 9.8657e-10 0.00033525 1.8464e-05 9.1456e-06 v FourierNb 0.14582 0.62811 0.22604 0.19217 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.8954 4.8955 0.00037997 -2.7683e-07 v volume_forces[Z] -4.8954 4.8955 -0.00037984 3.4383e-07 v ǁvolume_forcesǁ 4.0822e-09 4.8974 0.38634 0.15318 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.47 289.84 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.020018 6.8342e-05 3.8783e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14582 0.62811 0.22606 0.19218 INSTANT 0.243639000E+00 TIME STEP NUMBER 253 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.20591E-05 0.30055E-02 Friction velocity uk : 0.21891E-05 0.30053E-02 Dimensionless distance yplus : 0.14578E-04 0.19994E-01 Friction thermal sca. tstar : -0.55241E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.10239E-04 0.14043E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.20591E-05 0.30055E-02 Friction velocity uk : 0.21891E-05 0.30053E-02 Dimensionless distance yplus : 0.14578E-04 0.19994E-01 Friction thermal sca. tstar : -0.55241E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.10239E-04 0.14043E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.42625E-08 4 0.59720E-06 0.31478E-11 0.27556E+01 c Velocity[X] 0.30247E-30 c Velocity[Y] 0.15739E-11 c Velocity[Z] 0.15739E-11 c Pressure 0.48917E-13 23 0.89864E-08 0.38651E-06 0.32730E+01 c k 0.88951E-06 2 0.17486E-06 0.70276E-07 0.32324E+01 c omega 0.13153E+02 1 0.86007E-08 0.61354E+01 0.12895E-01 c TempK 0.94374E+02 1 0.41423E-06 0.10363E+00 0.35799E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.6574e-13 1.3779e-13 -1.6094e-17 -4.0558e-18 v Velocity[Y] -0.00018223 0.00018128 -9.1031e-10 -5.8862e-12 v Velocity[Z] -0.00018128 0.00018224 8.471e-10 -1.7359e-12 v ǁVelocityǁ 1.1216e-10 0.00021035 1.2334e-05 6.4295e-06 v Pressure -0.000423 0.012779 0.00060626 -8.0894e-21 v k 1.2399e-08 0.0030457 0.0021307 0.0025657 v omega 31.994 1.0313e+05 2678.9 515.22 v TempK 288 341.44 292.26 289.7 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.462e-13 0.00010789 7.3006e-05 9.1591e-05 v CourantNb 9.9065e-10 0.00033447 1.8422e-05 9.1263e-06 v FourierNb 0.14579 0.62811 0.22588 0.19205 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.8957 4.8957 0.00038046 -2.7787e-07 v volume_forces[Z] -4.8957 4.8957 -0.00038034 3.4503e-07 v ǁvolume_forcesǁ 4.0665e-09 4.8976 0.38684 0.15348 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.48 289.84 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.019994 6.8267e-05 3.8739e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.1458 0.62811 0.2259 0.19206 INSTANT 0.244602000E+00 TIME STEP NUMBER 254 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19344E-05 0.30019E-02 Friction velocity uk : 0.20700E-05 0.30017E-02 Dimensionless distance yplus : 0.13785E-04 0.19970E-01 Friction thermal sca. tstar : -0.82007E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.96819E-05 0.14026E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19344E-05 0.30019E-02 Friction velocity uk : 0.20700E-05 0.30017E-02 Dimensionless distance yplus : 0.13785E-04 0.19970E-01 Friction thermal sca. tstar : -0.82007E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.96819E-05 0.14026E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.42527E-08 4 0.59411E-06 0.31160E-11 0.27478E+01 c Velocity[X] 0.29817E-30 c Velocity[Y] 0.15580E-11 c Velocity[Z] 0.15580E-11 c Pressure 0.48538E-13 23 0.89304E-08 0.38349E-06 0.32599E+01 c k 0.88687E-06 2 0.17366E-06 0.69486E-07 0.32240E+01 c omega 0.13153E+02 1 0.85489E-08 0.60738E+01 0.12830E-01 c TempK 0.94375E+02 1 0.41207E-06 0.10304E+00 0.35697E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.6534e-13 1.3744e-13 -1.6062e-17 -4.0481e-18 v Velocity[Y] -0.00018188 0.00018091 -9.1249e-10 -5.867e-12 v Velocity[Z] -0.00018091 0.00018188 8.4881e-10 -1.7363e-12 v ǁVelocityǁ 1.1193e-10 0.00020983 1.231e-05 6.4191e-06 v Pressure -0.00042472 0.012805 0.00060799 -7.9913e-21 v k 1.2286e-08 0.0030353 0.0021236 0.0025578 v omega 31.913 1.0313e+05 2678.9 515.15 v TempK 288 341.44 292.26 289.7 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.4487e-13 0.00010779 7.295e-05 9.1536e-05 v CourantNb 9.9474e-10 0.00033369 1.8381e-05 9.107e-06 v FourierNb 0.14577 0.62811 0.22572 0.19192 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.8959 4.896 0.00038096 -2.789e-07 v volume_forces[Z] -4.8959 4.896 -0.00038083 3.4623e-07 v ǁvolume_forcesǁ 4.0545e-09 4.8979 0.38734 0.15379 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.49 289.85 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.01997 6.8193e-05 3.8695e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14577 0.62811 0.22573 0.19193 INSTANT 0.245565000E+00 TIME STEP NUMBER 255 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.18013E-05 0.29983E-02 Friction velocity uk : 0.19437E-05 0.29981E-02 Dimensionless distance yplus : 0.12944E-04 0.19947E-01 Friction thermal sca. tstar : -0.25999E+05 0.00000E+00 Dim-less thermal sca. tplus : 0.90914E-05 0.14009E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.18013E-05 0.29983E-02 Friction velocity uk : 0.19437E-05 0.29981E-02 Dimensionless distance yplus : 0.12944E-04 0.19947E-01 Friction thermal sca. tstar : -0.25999E+05 0.00000E+00 Dim-less thermal sca. tplus : 0.90914E-05 0.14009E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.42429E-08 4 0.59537E-06 0.30843E-11 0.27399E+01 c Velocity[X] 0.29392E-30 c Velocity[Y] 0.15422E-11 c Velocity[Z] 0.15421E-11 c Pressure 0.48193E-13 23 0.88720E-08 0.38074E-06 0.32468E+01 c k 0.88424E-06 2 0.17246E-06 0.68707E-07 0.32156E+01 c omega 0.13153E+02 1 0.84975E-08 0.60129E+01 0.12766E-01 c TempK 0.94376E+02 1 0.40992E-06 0.10246E+00 0.35595E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.6495e-13 1.3709e-13 -1.603e-17 -4.0404e-18 v Velocity[Y] -0.00018152 0.00018053 -9.1466e-10 -5.848e-12 v Velocity[Z] -0.00018054 0.00018153 8.5051e-10 -1.737e-12 v ǁVelocityǁ 1.118e-10 0.00020932 1.2285e-05 6.4088e-06 v Pressure -0.00042643 0.012831 0.00060971 1.2894e-20 v k 1.2174e-08 0.0030248 0.0021166 0.0025499 v omega 31.833 1.0313e+05 2678.8 515.07 v TempK 288 341.44 292.27 289.7 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.4355e-13 0.00010769 7.2894e-05 9.1482e-05 v CourantNb 9.9882e-10 0.00033292 1.8339e-05 9.0879e-06 v FourierNb 0.14574 0.62811 0.22555 0.1918 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.8962 4.8963 0.00038145 -2.7993e-07 v volume_forces[Z] -4.8962 4.8963 -0.00038132 3.4743e-07 v ǁvolume_forcesǁ 4.0463e-09 4.8982 0.38783 0.1541 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.49 289.85 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.019947 6.8118e-05 3.8651e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14574 0.62811 0.22557 0.19181 INSTANT 0.246528000E+00 TIME STEP NUMBER 256 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.16576E-05 0.29947E-02 Friction velocity uk : 0.18087E-05 0.29945E-02 Dimensionless distance yplus : 0.12045E-04 0.19923E-01 Friction thermal sca. tstar : -0.77905E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.84596E-05 0.13993E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.16576E-05 0.29947E-02 Friction velocity uk : 0.18087E-05 0.29945E-02 Dimensionless distance yplus : 0.12045E-04 0.19923E-01 Friction thermal sca. tstar : -0.77905E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.84596E-05 0.13993E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.42332E-08 4 0.58809E-06 0.30527E-11 0.27319E+01 c Velocity[X] 0.28974E-30 c Velocity[Y] 0.15264E-11 c Velocity[Z] 0.15263E-11 c Pressure 0.47842E-13 23 0.88214E-08 0.37794E-06 0.32339E+01 c k 0.88163E-06 2 0.17129E-06 0.67939E-07 0.32072E+01 c omega 0.13153E+02 1 0.84466E-08 0.59528E+01 0.12702E-01 c TempK 0.94376E+02 1 0.40780E-06 0.10188E+00 0.35495E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.6456e-13 1.3675e-13 -1.5998e-17 -4.0328e-18 v Velocity[Y] -0.00018117 0.00018016 -9.1682e-10 -5.8371e-12 v Velocity[Z] -0.00018017 0.00018118 8.5219e-10 -1.741e-12 v ǁVelocityǁ 1.1178e-10 0.00020881 1.2261e-05 6.3986e-06 v Pressure -0.00042815 0.012857 0.00061144 8.3835e-21 v k 1.2064e-08 0.0030145 0.0021096 0.0025421 v omega 31.753 1.0313e+05 2678.7 515 v TempK 288 341.45 292.27 289.71 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.4225e-13 0.0001076 7.2838e-05 9.1428e-05 v CourantNb 1.0029e-09 0.00033215 1.8298e-05 9.069e-06 v FourierNb 0.14571 0.62811 0.22539 0.19168 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.8965 4.8965 0.00038194 -2.8096e-07 v volume_forces[Z] -4.8965 4.8965 -0.00038181 3.4862e-07 v ǁvolume_forcesǁ 4.0417e-09 4.8984 0.38833 0.1544 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.5 289.85 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.019923 6.8048e-05 3.861e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14572 0.62811 0.22541 0.19169 INSTANT 0.247491000E+00 TIME STEP NUMBER 257 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15000E-05 0.29912E-02 Friction velocity uk : 0.16622E-05 0.29910E-02 Dimensionless distance yplus : 0.11069E-04 0.19899E-01 Friction thermal sca. tstar : -0.53890E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.77745E-05 0.13976E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15000E-05 0.29912E-02 Friction velocity uk : 0.16622E-05 0.29910E-02 Dimensionless distance yplus : 0.11069E-04 0.19899E-01 Friction thermal sca. tstar : -0.53890E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.77745E-05 0.13976E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.42236E-08 4 0.58512E-06 0.30211E-11 0.27238E+01 c Velocity[X] 0.28560E-30 c Velocity[Y] 0.15106E-11 c Velocity[Z] 0.15106E-11 c Pressure 0.47578E-13 23 0.87668E-08 0.37582E-06 0.32211E+01 c k 0.87903E-06 2 0.17012E-06 0.67181E-07 0.31989E+01 c omega 0.13153E+02 1 0.83961E-08 0.58935E+01 0.12638E-01 c TempK 0.94377E+02 1 0.40569E-06 0.10131E+00 0.35395E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.6417e-13 1.364e-13 -1.5967e-17 -4.0253e-18 v Velocity[Y] -0.00018083 0.00017979 -9.1896e-10 -5.8184e-12 v Velocity[Z] -0.0001798 0.00018083 8.5386e-10 -1.7418e-12 v ǁVelocityǁ 1.1186e-10 0.0002083 1.2237e-05 6.3886e-06 v Pressure -0.00042986 0.012882 0.00061316 -1.5934e-20 v k 1.1956e-08 0.0030041 0.0021027 0.0025343 v omega 31.673 1.0313e+05 2678.7 514.93 v TempK 288 341.45 292.28 289.71 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.4096e-13 0.0001075 7.2783e-05 9.1374e-05 v CourantNb 1.007e-09 0.00033138 1.8257e-05 9.0502e-06 v FourierNb 0.14569 0.62811 0.22523 0.19156 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.8967 4.8968 0.00038243 -2.8198e-07 v volume_forces[Z] -4.8967 4.8968 -0.0003823 3.4981e-07 v ǁvolume_forcesǁ 4.0407e-09 4.8987 0.38882 0.15471 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.5 289.86 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.019899 6.7978e-05 3.8568e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14569 0.62811 0.22525 0.19156 INSTANT 0.248454000E+00 TIME STEP NUMBER 258 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.13245E-05 0.29877E-02 Friction velocity uk : 0.15016E-05 0.29875E-02 Dimensionless distance yplus : 0.10000E-04 0.19876E-01 Friction thermal sca. tstar : -0.43734E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.70235E-05 0.13960E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.13245E-05 0.29877E-02 Friction velocity uk : 0.15016E-05 0.29875E-02 Dimensionless distance yplus : 0.10000E-04 0.19876E-01 Friction thermal sca. tstar : -0.43734E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.70235E-05 0.13960E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.42140E-08 4 0.58217E-06 0.29897E-11 0.27155E+01 c Velocity[X] 0.28154E-30 c Velocity[Y] 0.14949E-11 c Velocity[Z] 0.14948E-11 c Pressure 0.47165E-13 23 0.87083E-08 0.37253E-06 0.32083E+01 c k 0.87644E-06 2 0.16898E-06 0.66434E-07 0.31906E+01 c omega 0.13153E+02 1 0.83461E-08 0.58349E+01 0.12575E-01 c TempK 0.94378E+02 1 0.40360E-06 0.10075E+00 0.35295E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.6379e-13 1.3606e-13 -1.5936e-17 -4.0178e-18 v Velocity[Y] -0.00018048 0.00017943 -9.2108e-10 -5.7993e-12 v Velocity[Z] -0.00017943 0.00018048 8.5551e-10 -1.743e-12 v ǁVelocityǁ 1.1204e-10 0.0002078 1.2213e-05 6.3786e-06 v Pressure -0.00043158 0.012908 0.00061487 3.5446e-20 v k 1.1848e-08 0.0029939 0.0020958 0.0025266 v omega 31.594 1.0313e+05 2678.6 514.86 v TempK 288 341.45 292.28 289.71 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.3969e-13 0.0001074 7.2728e-05 9.132e-05 v CourantNb 1.0111e-09 0.00033062 1.8217e-05 9.0315e-06 v FourierNb 0.14566 0.62811 0.22507 0.19143 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.897 4.897 0.00038292 -2.83e-07 v volume_forces[Z] -4.897 4.897 -0.00038279 3.5099e-07 v ǁvolume_forcesǁ 4.0436e-09 4.8989 0.38931 0.15502 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.51 289.86 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.019876 6.7907e-05 3.8527e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14566 0.62811 0.22509 0.19144 INSTANT 0.249417000E+00 TIME STEP NUMBER 259 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11223E-05 0.29842E-02 Friction velocity uk : 0.13210E-05 0.29840E-02 Dimensionless distance yplus : 0.87973E-05 0.19853E-01 Friction thermal sca. tstar : -0.37744E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.61787E-05 0.13943E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11223E-05 0.29842E-02 Friction velocity uk : 0.13210E-05 0.29840E-02 Dimensionless distance yplus : 0.87973E-05 0.19853E-01 Friction thermal sca. tstar : -0.37744E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.61787E-05 0.13943E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.42045E-08 4 0.57922E-06 0.29583E-11 0.27072E+01 c Velocity[X] 0.27752E-30 c Velocity[Y] 0.14792E-11 c Velocity[Z] 0.14791E-11 c Pressure 0.46843E-13 23 0.86515E-08 0.36996E-06 0.31957E+01 c k 0.87387E-06 2 0.16784E-06 0.65697E-07 0.31824E+01 c omega 0.13153E+02 1 0.82964E-08 0.57769E+01 0.12513E-01 c TempK 0.94378E+02 1 0.40152E-06 0.10019E+00 0.35196E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.634e-13 1.3572e-13 -1.5905e-17 -4.0104e-18 v Velocity[Y] -0.00018014 0.00017907 -9.2319e-10 -5.7811e-12 v Velocity[Z] -0.00017907 0.00018014 8.5714e-10 -1.744e-12 v ǁVelocityǁ 1.1232e-10 0.0002073 1.2189e-05 6.3688e-06 v Pressure -0.00043329 0.012934 0.00061659 3.2946e-20 v k 1.1742e-08 0.0029837 0.0020889 0.0025189 v omega 31.515 1.0313e+05 2678.6 514.78 v TempK 288 341.45 292.29 289.72 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.3844e-13 0.0001073 7.2673e-05 9.1266e-05 v CourantNb 1.0152e-09 0.00032986 1.8177e-05 9.013e-06 v FourierNb 0.14563 0.62811 0.22492 0.19131 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.8972 4.8973 0.00038341 -2.8401e-07 v volume_forces[Z] -4.8972 4.8973 -0.00038328 3.5216e-07 v ǁvolume_forcesǁ 4.0501e-09 4.8992 0.38981 0.15532 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.51 289.86 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.019853 6.7837e-05 3.8485e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14563 0.62811 0.22493 0.19132 INSTANT 0.250380000E+00 TIME STEP NUMBER 260 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.87800E-06 0.29807E-02 Friction velocity uk : 0.11111E-05 0.29805E-02 Dimensionless distance yplus : 0.73993E-05 0.19830E-01 Friction thermal sca. tstar : -0.33684E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.51968E-05 0.13927E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.87800E-06 0.29807E-02 Friction velocity uk : 0.11111E-05 0.29805E-02 Dimensionless distance yplus : 0.73993E-05 0.19830E-01 Friction thermal sca. tstar : -0.33684E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.51968E-05 0.13927E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.41951E-08 4 0.57625E-06 0.29270E-11 0.26987E+01 c Velocity[X] 0.27355E-30 c Velocity[Y] 0.14635E-11 c Velocity[Z] 0.14635E-11 c Pressure 0.46505E-13 23 0.85995E-08 0.36727E-06 0.31831E+01 c k 0.87131E-06 2 0.16672E-06 0.64970E-07 0.31742E+01 c omega 0.13153E+02 1 0.82472E-08 0.57197E+01 0.12451E-01 c TempK 0.94379E+02 1 0.39947E-06 0.99630E-01 0.35098E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.6302e-13 1.3539e-13 -1.5874e-17 -4.003e-18 v Velocity[Y] -0.0001798 0.00017871 -9.2528e-10 -5.7622e-12 v Velocity[Z] -0.00017871 0.0001798 8.5876e-10 -1.7449e-12 v ǁVelocityǁ 1.1271e-10 0.0002068 1.2166e-05 6.359e-06 v Pressure -0.00043501 0.012959 0.0006183 -4.807e-20 v k 1.1637e-08 0.0029735 0.0020821 0.0025112 v omega 31.437 1.0313e+05 2678.5 514.71 v TempK 288 341.46 292.29 289.72 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.372e-13 0.00010721 7.2618e-05 9.1212e-05 v CourantNb 1.0193e-09 0.0003291 1.8137e-05 8.9947e-06 v FourierNb 0.1456 0.62811 0.22476 0.19119 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.8975 4.8975 0.00038389 -2.8502e-07 v volume_forces[Z] -4.8975 4.8975 -0.00038377 3.5333e-07 v ǁvolume_forcesǁ 4.0604e-09 4.8994 0.3903 0.15562 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.52 289.87 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.01983 6.7768e-05 3.8444e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14561 0.62811 0.22478 0.1912 INSTANT 0.251343000E+00 TIME STEP NUMBER 261 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.54924E-06 0.29772E-02 Friction velocity uk : 0.84994E-06 0.29770E-02 Dimensionless distance yplus : 0.56602E-05 0.19807E-01 Friction thermal sca. tstar : -0.30700E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.39754E-05 0.13911E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.54924E-06 0.29772E-02 Friction velocity uk : 0.84994E-06 0.29770E-02 Dimensionless distance yplus : 0.56602E-05 0.19807E-01 Friction thermal sca. tstar : -0.30700E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.39754E-05 0.13911E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.41858E-08 4 0.57331E-06 0.28958E-11 0.26901E+01 c Velocity[X] 0.26964E-30 c Velocity[Y] 0.14479E-11 c Velocity[Z] 0.14479E-11 c Pressure 0.46165E-13 23 0.85453E-08 0.36456E-06 0.31707E+01 c k 0.86877E-06 2 0.16562E-06 0.64252E-07 0.31661E+01 c omega 0.13153E+02 1 0.81984E-08 0.56632E+01 0.12389E-01 c TempK 0.94380E+02 1 0.39743E-06 0.99079E-01 0.35000E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.6265e-13 1.3505e-13 -1.5844e-17 -3.9957e-18 v Velocity[Y] -0.00017946 0.00017835 -9.2736e-10 -5.7436e-12 v Velocity[Z] -0.00017835 0.00017946 8.6037e-10 -1.746e-12 v ǁVelocityǁ 1.132e-10 0.0002063 1.2142e-05 6.3493e-06 v Pressure -0.00043672 0.012985 0.00062001 -1.2526e-20 v k 1.1534e-08 0.0029634 0.0020753 0.0025036 v omega 31.359 1.0313e+05 2678.4 514.64 v TempK 288 341.46 292.3 289.72 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.3597e-13 0.00010711 7.2563e-05 9.1159e-05 v CourantNb 1.0234e-09 0.00032835 1.8097e-05 8.9764e-06 v FourierNb 0.14558 0.62811 0.2246 0.19107 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.8977 4.8978 0.00038438 -2.8602e-07 v volume_forces[Z] -4.8977 4.8978 -0.00038425 3.545e-07 v ǁvolume_forcesǁ 4.0744e-09 4.8997 0.39078 0.15593 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.52 289.87 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.019807 6.7698e-05 3.8403e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14558 0.62811 0.22462 0.19108 INSTANT 0.252306000E+00 TIME STEP NUMBER 262 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.23672E-06 0.29738E-02 Friction velocity uk : 0.63433E-06 0.29736E-02 Dimensionless distance yplus : 0.42244E-05 0.19784E-01 Friction thermal sca. tstar : -0.28389E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.29669E-05 0.13895E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.23672E-06 0.29738E-02 Friction velocity uk : 0.63433E-06 0.29736E-02 Dimensionless distance yplus : 0.42244E-05 0.19784E-01 Friction thermal sca. tstar : -0.28389E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.29669E-05 0.13895E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.41766E-08 4 0.57040E-06 0.28648E-11 0.26814E+01 c Velocity[X] 0.26579E-30 c Velocity[Y] 0.14324E-11 c Velocity[Z] 0.14324E-11 c Pressure 0.45834E-13 23 0.84911E-08 0.36192E-06 0.31583E+01 c k 0.86623E-06 2 0.16453E-06 0.63545E-07 0.31580E+01 c omega 0.13153E+02 1 0.81500E-08 0.56074E+01 0.12328E-01 c TempK 0.94381E+02 1 0.39541E-06 0.98534E-01 0.34904E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.6227e-13 1.3472e-13 -1.5814e-17 -3.9885e-18 v Velocity[Y] -0.00017912 0.00017799 -9.2942e-10 -5.7251e-12 v Velocity[Z] -0.000178 0.00017913 8.6196e-10 -1.7472e-12 v ǁVelocityǁ 1.1379e-10 0.00020581 1.2119e-05 6.3398e-06 v Pressure -0.00043844 0.01301 0.00062171 1.0001e-20 v k 1.1431e-08 0.0029534 0.0020686 0.002496 v omega 31.282 1.0313e+05 2678.4 514.57 v TempK 288 341.46 292.3 289.73 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.3476e-13 0.00010701 7.2509e-05 9.1106e-05 v CourantNb 1.0275e-09 0.00032761 1.8058e-05 8.9584e-06 v FourierNb 0.14555 0.62811 0.22445 0.19095 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.898 4.898 0.00038486 -2.8702e-07 v volume_forces[Z] -4.898 4.898 -0.00038473 3.5566e-07 v ǁvolume_forcesǁ 4.0921e-09 4.8999 0.39127 0.15623 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.53 289.87 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.019784 6.7629e-05 3.8363e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14555 0.62811 0.22446 0.19096 INSTANT 0.253269000E+00 TIME STEP NUMBER 263 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.61957E-06 0.29704E-02 Friction velocity uk : 0.89701E-06 0.29702E-02 Dimensionless distance yplus : 0.59737E-05 0.19761E-01 Friction thermal sca. tstar : -0.26531E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.41955E-05 0.13879E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.61957E-06 0.29704E-02 Friction velocity uk : 0.89701E-06 0.29702E-02 Dimensionless distance yplus : 0.59737E-05 0.19761E-01 Friction thermal sca. tstar : -0.26531E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.41955E-05 0.13879E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.41674E-08 4 0.56752E-06 0.28338E-11 0.26726E+01 c Velocity[X] 0.26199E-30 c Velocity[Y] 0.14169E-11 c Velocity[Z] 0.14169E-11 c Pressure 0.45520E-13 23 0.84368E-08 0.35942E-06 0.31460E+01 c k 0.86372E-06 2 0.16345E-06 0.62847E-07 0.31500E+01 c omega 0.13153E+02 1 0.81019E-08 0.55523E+01 0.12267E-01 c TempK 0.94381E+02 1 0.39341E-06 0.97993E-01 0.34807E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.619e-13 1.3439e-13 -1.5784e-17 -3.9813e-18 v Velocity[Y] -0.00017879 0.00017764 -9.3147e-10 -5.7067e-12 v Velocity[Z] -0.00017764 0.00017879 8.6353e-10 -1.7484e-12 v ǁVelocityǁ 1.1448e-10 0.00020532 1.2096e-05 6.3304e-06 v Pressure -0.00044016 0.013036 0.00062341 5.2262e-20 v k 1.133e-08 0.0029434 0.0020619 0.0024885 v omega 31.205 1.0313e+05 2678.3 514.5 v TempK 288 341.46 292.31 289.73 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.3357e-13 0.00010692 7.2455e-05 9.1053e-05 v CourantNb 1.0316e-09 0.00032687 1.8019e-05 8.9404e-06 v FourierNb 0.14552 0.62811 0.22429 0.19083 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.8982 4.8983 0.00038534 -2.8801e-07 v volume_forces[Z] -4.8982 4.8983 -0.00038522 3.5681e-07 v ǁvolume_forcesǁ 4.1135e-09 4.9001 0.39176 0.15653 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.53 289.88 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.019761 6.7561e-05 3.8322e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14552 0.62811 0.22431 0.19084 INSTANT 0.254232000E+00 TIME STEP NUMBER 264 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.93275E-06 0.29670E-02 Friction velocity uk : 0.11469E-05 0.29668E-02 Dimensionless distance yplus : 0.76376E-05 0.19738E-01 Friction thermal sca. tstar : -0.24995E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.53642E-05 0.13863E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.93275E-06 0.29670E-02 Friction velocity uk : 0.11469E-05 0.29668E-02 Dimensionless distance yplus : 0.76376E-05 0.19738E-01 Friction thermal sca. tstar : -0.24995E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.53642E-05 0.13863E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.41583E-08 4 0.56594E-06 0.28030E-11 0.26637E+01 c Velocity[X] 0.25824E-30 c Velocity[Y] 0.14015E-11 c Velocity[Z] 0.14015E-11 c Pressure 0.45195E-13 23 0.83844E-08 0.35683E-06 0.31339E+01 c k 0.86121E-06 2 0.16238E-06 0.62159E-07 0.31420E+01 c omega 0.13153E+02 1 0.80543E-08 0.54978E+01 0.12207E-01 c TempK 0.94382E+02 1 0.39142E-06 0.97457E-01 0.34712E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.6153e-13 1.3406e-13 -1.5754e-17 -3.9741e-18 v Velocity[Y] -0.00017846 0.00017729 -9.3351e-10 -5.6883e-12 v Velocity[Z] -0.00017729 0.00017846 8.6509e-10 -1.7496e-12 v ǁVelocityǁ 1.1528e-10 0.00020484 1.2073e-05 6.321e-06 v Pressure -0.00044187 0.013061 0.00062511 2.5788e-20 v k 1.123e-08 0.0029334 0.0020552 0.002481 v omega 31.128 1.0313e+05 2678.3 514.43 v TempK 288 341.47 292.32 289.73 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.3239e-13 0.00010685 7.2401e-05 9.1e-05 v CourantNb 1.0356e-09 0.00032613 1.798e-05 8.9227e-06 v FourierNb 0.14549 0.62811 0.22414 0.19071 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.8985 4.8985 0.00038583 -2.8901e-07 v volume_forces[Z] -4.8985 4.8985 -0.0003857 3.5796e-07 v ǁvolume_forcesǁ 4.1386e-09 4.9004 0.39224 0.15683 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.54 289.88 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.019738 6.7493e-05 3.8282e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.1455 0.62811 0.22415 0.19072 INSTANT 0.255195000E+00 TIME STEP NUMBER 265 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11728E-05 0.29636E-02 Friction velocity uk : 0.13520E-05 0.29634E-02 Dimensionless distance yplus : 0.90035E-05 0.19716E-01 Friction thermal sca. tstar : -0.23697E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.63235E-05 0.13847E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11728E-05 0.29636E-02 Friction velocity uk : 0.13520E-05 0.29634E-02 Dimensionless distance yplus : 0.90035E-05 0.19716E-01 Friction thermal sca. tstar : -0.23697E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.63235E-05 0.13847E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.41492E-08 4 0.56178E-06 0.27724E-11 0.26548E+01 c Velocity[X] 0.25455E-30 c Velocity[Y] 0.13862E-11 c Velocity[Z] 0.13862E-11 c Pressure 0.44863E-13 23 0.83318E-08 0.35419E-06 0.31218E+01 c k 0.85872E-06 2 0.16133E-06 0.61479E-07 0.31340E+01 c omega 0.13153E+02 1 0.80071E-08 0.54440E+01 0.12147E-01 c TempK 0.94383E+02 1 0.38945E-06 0.96926E-01 0.34616E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.6116e-13 1.3374e-13 -1.5724e-17 -3.967e-18 v Velocity[Y] -0.00017813 0.00017694 -9.3553e-10 -5.6699e-12 v Velocity[Z] -0.00017694 0.00017813 8.6663e-10 -1.7509e-12 v ǁVelocityǁ 1.1617e-10 0.00020435 1.2051e-05 6.3118e-06 v Pressure -0.00044359 0.013086 0.00062681 -4.4099e-20 v k 1.1132e-08 0.0029235 0.0020486 0.0024735 v omega 31.051 1.0313e+05 2678.2 514.36 v TempK 288 341.47 292.32 289.74 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.3122e-13 0.00010677 7.2347e-05 9.0947e-05 v CourantNb 1.0397e-09 0.0003254 1.7941e-05 8.905e-06 v FourierNb 0.14547 0.62811 0.22398 0.19059 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.8987 4.8988 0.0003863 -2.8999e-07 v volume_forces[Z] -4.8987 4.8988 -0.00038618 3.5911e-07 v ǁvolume_forcesǁ 4.1673e-09 4.9006 0.39272 0.15713 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.54 289.88 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.019716 6.7425e-05 3.8242e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14547 0.62811 0.224 0.1906 INSTANT 0.256158000E+00 TIME STEP NUMBER 266 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12712E-05 0.29602E-02 Friction velocity uk : 0.14375E-05 0.29601E-02 Dimensionless distance yplus : 0.95732E-05 0.19693E-01 Friction thermal sca. tstar : -0.22583E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.67236E-05 0.13831E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12712E-05 0.29602E-02 Friction velocity uk : 0.14375E-05 0.29601E-02 Dimensionless distance yplus : 0.95732E-05 0.19693E-01 Friction thermal sca. tstar : -0.22583E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.67236E-05 0.13831E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.41403E-08 4 0.55894E-06 0.27419E-11 0.26457E+01 c Velocity[X] 0.25090E-30 c Velocity[Y] 0.13709E-11 c Velocity[Z] 0.13709E-11 c Pressure 0.44544E-13 23 0.82796E-08 0.35164E-06 0.31098E+01 c k 0.85624E-06 2 0.16029E-06 0.60809E-07 0.31261E+01 c omega 0.13153E+02 1 0.79603E-08 0.53909E+01 0.12087E-01 c TempK 0.94383E+02 1 0.38750E-06 0.96400E-01 0.34522E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.608e-13 1.3342e-13 -1.5695e-17 -3.96e-18 v Velocity[Y] -0.0001778 0.00017659 -9.3753e-10 -5.6516e-12 v Velocity[Z] -0.0001766 0.00017781 8.6815e-10 -1.7522e-12 v ǁVelocityǁ 1.1675e-10 0.00020387 1.2029e-05 6.3027e-06 v Pressure -0.00044531 0.013111 0.00062851 3.6819e-20 v k 1.1034e-08 0.0029137 0.002042 0.0024661 v omega 30.975 1.0313e+05 2678.2 514.29 v TempK 288 341.47 292.33 289.74 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.3007e-13 0.0001067 7.2293e-05 9.0894e-05 v CourantNb 1.0438e-09 0.00032467 1.7903e-05 8.8876e-06 v FourierNb 0.14544 0.62811 0.22383 0.19047 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.8989 4.899 0.00038678 -2.9098e-07 v volume_forces[Z] -4.8989 4.899 -0.00038665 3.6025e-07 v ǁvolume_forcesǁ 4.1997e-09 4.9009 0.3932 0.15744 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.55 289.89 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.019693 6.7357e-05 3.8202e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14544 0.62811 0.22385 0.19048 INSTANT 0.257121000E+00 TIME STEP NUMBER 267 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10575E-05 0.29569E-02 Friction velocity uk : 0.12468E-05 0.29567E-02 Dimensionless distance yplus : 0.83033E-05 0.19671E-01 Friction thermal sca. tstar : -0.21611E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.58317E-05 0.13816E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10575E-05 0.29569E-02 Friction velocity uk : 0.12468E-05 0.29567E-02 Dimensionless distance yplus : 0.83033E-05 0.19671E-01 Friction thermal sca. tstar : -0.21611E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.58317E-05 0.13816E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.41314E-08 4 0.55611E-06 0.27115E-11 0.26365E+01 c Velocity[X] 0.24731E-30 c Velocity[Y] 0.13558E-11 c Velocity[Z] 0.13558E-11 c Pressure 0.44228E-13 23 0.82277E-08 0.34912E-06 0.30979E+01 c k 0.85378E-06 2 0.15927E-06 0.60148E-07 0.31182E+01 c omega 0.13153E+02 1 0.79138E-08 0.53384E+01 0.12028E-01 c TempK 0.94384E+02 1 0.38556E-06 0.95879E-01 0.34428E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.6044e-13 1.331e-13 -1.5666e-17 -3.953e-18 v Velocity[Y] -0.00017748 0.00017625 -9.3952e-10 -5.6334e-12 v Velocity[Z] -0.00017625 0.00017748 8.6966e-10 -1.7535e-12 v ǁVelocityǁ 1.1707e-10 0.0002034 1.2006e-05 6.2936e-06 v Pressure -0.00044702 0.013137 0.0006302 5.3145e-20 v k 1.0938e-08 0.0029039 0.0020355 0.0024587 v omega 30.9 1.0313e+05 2678.1 514.22 v TempK 288 341.48 292.33 289.74 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.2893e-13 0.00010662 7.224e-05 9.0842e-05 v CourantNb 1.0479e-09 0.00032394 1.7865e-05 8.8702e-06 v FourierNb 0.14541 0.62811 0.22368 0.19036 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.8992 4.8992 0.00038726 -2.9195e-07 v volume_forces[Z] -4.8992 4.8992 -0.00038713 3.6138e-07 v ǁvolume_forcesǁ 4.2204e-09 4.9011 0.39368 0.15773 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.56 289.89 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.019671 6.729e-05 3.8163e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14541 0.62811 0.22369 0.19037 INSTANT 0.258084000E+00 TIME STEP NUMBER 268 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.79161E-06 0.29536E-02 Friction velocity uk : 0.10200E-05 0.29534E-02 Dimensionless distance yplus : 0.67930E-05 0.19649E-01 Friction thermal sca. tstar : -0.20755E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.47710E-05 0.13800E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.79161E-06 0.29536E-02 Friction velocity uk : 0.10200E-05 0.29534E-02 Dimensionless distance yplus : 0.67930E-05 0.19649E-01 Friction thermal sca. tstar : -0.20755E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.47710E-05 0.13800E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.41226E-08 4 0.55329E-06 0.26813E-11 0.26273E+01 c Velocity[X] 0.24377E-30 c Velocity[Y] 0.13407E-11 c Velocity[Z] 0.13407E-11 c Pressure 0.43914E-13 23 0.81749E-08 0.34662E-06 0.30860E+01 c k 0.85133E-06 2 0.15826E-06 0.59496E-07 0.31104E+01 c omega 0.13153E+02 1 0.78678E-08 0.52865E+01 0.11970E-01 c TempK 0.94385E+02 1 0.38364E-06 0.95362E-01 0.34335E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.6008e-13 1.3278e-13 -1.5637e-17 -3.9461e-18 v Velocity[Y] -0.00017716 0.00017591 -9.415e-10 -5.6162e-12 v Velocity[Z] -0.00017591 0.00017716 8.7116e-10 -1.7499e-12 v ǁVelocityǁ 1.175e-10 0.00020292 1.1984e-05 6.2847e-06 v Pressure -0.00044874 0.013162 0.00063189 1.4757e-20 v k 1.0843e-08 0.0028942 0.002029 0.0024514 v omega 30.824 1.0313e+05 2678 514.15 v TempK 288 341.48 292.34 289.75 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.278e-13 0.00010655 7.2186e-05 9.0789e-05 v CourantNb 1.052e-09 0.00032322 1.7828e-05 8.8531e-06 v FourierNb 0.14538 0.62811 0.22353 0.19024 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.8994 4.8995 0.00038773 -2.9293e-07 v volume_forces[Z] -4.8994 4.8995 -0.0003876 3.6252e-07 v ǁvolume_forcesǁ 4.2322e-09 4.9013 0.39416 0.15803 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.56 289.89 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.019649 6.7224e-05 3.8123e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14539 0.62811 0.22354 0.19025 INSTANT 0.259047000E+00 TIME STEP NUMBER 269 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.40665E-06 0.29503E-02 Friction velocity uk : 0.72425E-06 0.29501E-02 Dimensionless distance yplus : 0.48232E-05 0.19627E-01 Friction thermal sca. tstar : -0.19993E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.33875E-05 0.13785E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.40665E-06 0.29503E-02 Friction velocity uk : 0.72425E-06 0.29501E-02 Dimensionless distance yplus : 0.48232E-05 0.19627E-01 Friction thermal sca. tstar : -0.19993E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.33875E-05 0.13785E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.41138E-08 4 0.55058E-06 0.26513E-11 0.26180E+01 c Velocity[X] 0.24029E-30 c Velocity[Y] 0.13257E-11 c Velocity[Z] 0.13257E-11 c Pressure 0.43609E-13 23 0.81275E-08 0.34419E-06 0.30743E+01 c k 0.84889E-06 2 0.15725E-06 0.58853E-07 0.31025E+01 c omega 0.13153E+02 1 0.78221E-08 0.52352E+01 0.11912E-01 c TempK 0.94386E+02 1 0.38174E-06 0.94850E-01 0.34242E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.5972e-13 1.3246e-13 -1.5608e-17 -3.9392e-18 v Velocity[Y] -0.00017684 0.00017557 -9.4346e-10 -5.5982e-12 v Velocity[Z] -0.00017557 0.00017684 8.7264e-10 -1.7513e-12 v ǁVelocityǁ 1.1803e-10 0.00020245 1.1963e-05 6.2759e-06 v Pressure -0.00045046 0.013187 0.00063358 2.0885e-20 v k 1.0748e-08 0.0028845 0.0020225 0.0024441 v omega 30.75 1.0313e+05 2678 514.08 v TempK 288 341.48 292.34 289.75 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.2669e-13 0.00010648 7.2133e-05 9.0737e-05 v CourantNb 1.0561e-09 0.00032251 1.779e-05 8.8361e-06 v FourierNb 0.14536 0.62811 0.22337 0.19012 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.8997 4.8997 0.00038821 -2.939e-07 v volume_forces[Z] -4.8997 4.8997 -0.00038808 3.6364e-07 v ǁvolume_forcesǁ 4.2476e-09 4.9016 0.39464 0.15833 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.57 289.9 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.019627 6.7158e-05 3.8084e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14536 0.62811 0.22339 0.19013 INSTANT 0.260010000E+00 TIME STEP NUMBER 270 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.32923E-06 0.29470E-02 Friction velocity uk : 0.66875E-06 0.29468E-02 Dimensionless distance yplus : 0.44536E-05 0.19605E-01 Friction thermal sca. tstar : -0.19309E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.31279E-05 0.13770E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.32923E-06 0.29470E-02 Friction velocity uk : 0.66875E-06 0.29468E-02 Dimensionless distance yplus : 0.44536E-05 0.19605E-01 Friction thermal sca. tstar : -0.19309E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.31279E-05 0.13770E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.41051E-08 4 0.54774E-06 0.26215E-11 0.26086E+01 c Velocity[X] 0.23685E-30 c Velocity[Y] 0.13108E-11 c Velocity[Z] 0.13107E-11 c Pressure 0.43294E-13 23 0.80742E-08 0.34168E-06 0.30627E+01 c k 0.84646E-06 2 0.15626E-06 0.58218E-07 0.30948E+01 c omega 0.13153E+02 1 0.77768E-08 0.51846E+01 0.11854E-01 c TempK 0.94386E+02 1 0.37985E-06 0.94342E-01 0.34150E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.5937e-13 1.3215e-13 -1.558e-17 -3.9324e-18 v Velocity[Y] -0.00017652 0.00017523 -9.454e-10 -5.5801e-12 v Velocity[Z] -0.00017524 0.00017652 8.7411e-10 -1.7529e-12 v ǁVelocityǁ 1.1865e-10 0.00020198 1.1941e-05 6.2672e-06 v Pressure -0.00045217 0.013212 0.00063526 1.1497e-20 v k 1.0655e-08 0.0028749 0.0020161 0.0024368 v omega 30.675 1.0313e+05 2677.9 514.01 v TempK 288 341.48 292.35 289.75 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.2559e-13 0.0001064 7.2081e-05 9.0685e-05 v CourantNb 1.0602e-09 0.00032179 1.7753e-05 8.8192e-06 v FourierNb 0.14533 0.62811 0.22322 0.19001 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.8999 4.9 0.00038868 -2.9487e-07 v volume_forces[Z] -4.8999 4.9 -0.00038855 3.6476e-07 v ǁvolume_forcesǁ 4.2667e-09 4.9018 0.39511 0.15863 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.57 289.9 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.019605 6.7092e-05 3.8045e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14533 0.62811 0.22324 0.19002 INSTANT 0.260973000E+00 TIME STEP NUMBER 271 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.75211E-06 0.29437E-02 Friction velocity uk : 0.98063E-06 0.29435E-02 Dimensionless distance yplus : 0.65306E-05 0.19584E-01 Friction thermal sca. tstar : -0.18690E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.45867E-05 0.13754E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.75211E-06 0.29437E-02 Friction velocity uk : 0.98063E-06 0.29435E-02 Dimensionless distance yplus : 0.65306E-05 0.19584E-01 Friction thermal sca. tstar : -0.18690E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.45867E-05 0.13754E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.40965E-08 4 0.56508E-06 0.25918E-11 0.25991E+01 c Velocity[X] 0.23346E-30 c Velocity[Y] 0.12959E-11 c Velocity[Z] 0.12959E-11 c Pressure 0.42996E-13 23 0.80228E-08 0.33931E-06 0.30511E+01 c k 0.84405E-06 2 0.15529E-06 0.57591E-07 0.30871E+01 c omega 0.13153E+02 1 0.77319E-08 0.51345E+01 0.11797E-01 c TempK 0.94387E+02 1 0.37798E-06 0.93839E-01 0.34058E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.5901e-13 1.3184e-13 -1.5552e-17 -3.9256e-18 v Velocity[Y] -0.00017621 0.0001749 -9.4733e-10 -5.5622e-12 v Velocity[Z] -0.0001749 0.00017621 8.7556e-10 -1.7544e-12 v ǁVelocityǁ 1.1938e-10 0.00020152 1.192e-05 6.2586e-06 v Pressure -0.00045389 0.013237 0.00063694 4.2163e-21 v k 1.0563e-08 0.0028653 0.0020097 0.0024296 v omega 30.601 1.0313e+05 2677.9 513.94 v TempK 288 341.49 292.35 289.76 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.245e-13 0.00010633 7.2028e-05 9.0633e-05 v CourantNb 1.0643e-09 0.00032109 1.7716e-05 8.8025e-06 v FourierNb 0.1453 0.62811 0.22308 0.18989 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9001 4.9002 0.00038915 -2.9583e-07 v volume_forces[Z] -4.9001 4.9002 -0.00038902 3.6588e-07 v ǁvolume_forcesǁ 4.2893e-09 4.902 0.39559 0.15893 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.58 289.9 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.019584 6.7026e-05 3.8006e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.1453 0.62811 0.22309 0.1899 INSTANT 0.261936000E+00 TIME STEP NUMBER 272 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10340E-05 0.29405E-02 Friction velocity uk : 0.12159E-05 0.29403E-02 Dimensionless distance yplus : 0.80974E-05 0.19562E-01 Friction thermal sca. tstar : -0.18127E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.56871E-05 0.13739E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10340E-05 0.29405E-02 Friction velocity uk : 0.12159E-05 0.29403E-02 Dimensionless distance yplus : 0.80974E-05 0.19562E-01 Friction thermal sca. tstar : -0.18127E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.56871E-05 0.13739E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.40880E-08 4 0.54223E-06 0.25624E-11 0.25896E+01 c Velocity[X] 0.23011E-30 c Velocity[Y] 0.12812E-11 c Velocity[Z] 0.12812E-11 c Pressure 0.42691E-13 23 0.79734E-08 0.33688E-06 0.30396E+01 c k 0.84165E-06 2 0.15432E-06 0.56973E-07 0.30794E+01 c omega 0.13153E+02 1 0.76873E-08 0.50851E+01 0.11740E-01 c TempK 0.94388E+02 1 0.37612E-06 0.93341E-01 0.33967E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.5866e-13 1.3153e-13 -1.5523e-17 -3.9188e-18 v Velocity[Y] -0.00017589 0.00017456 -9.4925e-10 -5.5443e-12 v Velocity[Z] -0.00017457 0.0001759 8.7699e-10 -1.7559e-12 v ǁVelocityǁ 1.2021e-10 0.00020106 1.1898e-05 6.2501e-06 v Pressure -0.0004556 0.013262 0.00063862 -7.6971e-21 v k 1.0473e-08 0.0028557 0.0020033 0.0024225 v omega 30.527 1.0313e+05 2677.8 513.88 v TempK 288 341.49 292.36 289.76 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.2343e-13 0.00010625 7.1975e-05 9.0582e-05 v CourantNb 1.0684e-09 0.00032038 1.768e-05 8.7859e-06 v FourierNb 0.14527 0.62811 0.22293 0.18978 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9004 4.9004 0.00038962 -2.9679e-07 v volume_forces[Z] -4.9004 4.9004 -0.00038949 3.6699e-07 v ǁvolume_forcesǁ 4.3156e-09 4.9023 0.39606 0.15923 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.58 289.91 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.019562 6.6961e-05 3.7968e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14528 0.62811 0.22294 0.18978 INSTANT 0.262899000E+00 TIME STEP NUMBER 273 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12589E-05 0.29373E-02 Friction velocity uk : 0.14134E-05 0.29371E-02 Dimensionless distance yplus : 0.94125E-05 0.19541E-01 Friction thermal sca. tstar : -0.17612E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.66108E-05 0.13724E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12589E-05 0.29373E-02 Friction velocity uk : 0.14134E-05 0.29371E-02 Dimensionless distance yplus : 0.94125E-05 0.19541E-01 Friction thermal sca. tstar : -0.17612E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.66108E-05 0.13724E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.40796E-08 4 0.53950E-06 0.25331E-11 0.25800E+01 c Velocity[X] 0.22682E-30 c Velocity[Y] 0.12666E-11 c Velocity[Z] 0.12665E-11 c Pressure 0.42378E-13 23 0.79247E-08 0.33439E-06 0.30282E+01 c k 0.83926E-06 2 0.15337E-06 0.56363E-07 0.30717E+01 c omega 0.13153E+02 1 0.76431E-08 0.50362E+01 0.11683E-01 c TempK 0.94388E+02 1 0.37428E-06 0.92846E-01 0.33877E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.5832e-13 1.3123e-13 -1.5496e-17 -3.9121e-18 v Velocity[Y] -0.00017558 0.00017423 -9.5115e-10 -5.5264e-12 v Velocity[Z] -0.00017424 0.00017559 8.7841e-10 -1.7575e-12 v ǁVelocityǁ 1.2113e-10 0.0002006 1.1877e-05 6.2417e-06 v Pressure -0.00045732 0.013287 0.0006403 6.1773e-21 v k 1.0383e-08 0.0028463 0.001997 0.0024153 v omega 30.453 1.0313e+05 2677.8 513.81 v TempK 288 341.49 292.36 289.76 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.2236e-13 0.00010618 7.1923e-05 9.053e-05 v CourantNb 1.0725e-09 0.00031968 1.7644e-05 8.7695e-06 v FourierNb 0.14525 0.62811 0.22278 0.18966 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9006 4.9007 0.00039009 -2.9775e-07 v volume_forces[Z] -4.9006 4.9007 -0.00038996 3.681e-07 v ǁvolume_forcesǁ 4.3455e-09 4.9025 0.39653 0.15952 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.59 289.91 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.019541 6.6897e-05 3.793e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14525 0.62811 0.2228 0.18967 INSTANT 0.263862000E+00 TIME STEP NUMBER 274 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.14514E-05 0.29340E-02 Friction velocity uk : 0.15872E-05 0.29339E-02 Dimensionless distance yplus : 0.10570E-04 0.19519E-01 Friction thermal sca. tstar : -0.17138E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.74237E-05 0.13709E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.14514E-05 0.29340E-02 Friction velocity uk : 0.15872E-05 0.29339E-02 Dimensionless distance yplus : 0.10570E-04 0.19519E-01 Friction thermal sca. tstar : -0.17138E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.74237E-05 0.13709E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.40712E-08 4 0.53679E-06 0.25040E-11 0.25703E+01 c Velocity[X] 0.22358E-30 c Velocity[Y] 0.12520E-11 c Velocity[Z] 0.12520E-11 c Pressure 0.42080E-13 23 0.78751E-08 0.33201E-06 0.30169E+01 c k 0.83689E-06 2 0.15242E-06 0.55761E-07 0.30641E+01 c omega 0.13153E+02 1 0.75992E-08 0.49879E+01 0.11627E-01 c TempK 0.94389E+02 1 0.37245E-06 0.92356E-01 0.33787E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.5797e-13 1.3092e-13 -1.5468e-17 -3.9055e-18 v Velocity[Y] -0.00017527 0.00017391 -9.5304e-10 -5.5087e-12 v Velocity[Z] -0.00017391 0.00017528 8.7981e-10 -1.7592e-12 v ǁVelocityǁ 1.2215e-10 0.00020014 1.1857e-05 6.2334e-06 v Pressure -0.00045904 0.013312 0.00064197 -2.1596e-20 v k 1.0294e-08 0.0028368 0.0019907 0.0024082 v omega 30.38 1.0313e+05 2677.7 513.74 v TempK 288 341.49 292.37 289.77 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.2131e-13 0.0001061 7.1871e-05 9.0479e-05 v CourantNb 1.0766e-09 0.00031899 1.7608e-05 8.7532e-06 v FourierNb 0.14522 0.62811 0.22263 0.18955 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9008 4.9009 0.00039056 -2.987e-07 v volume_forces[Z] -4.9008 4.9009 -0.00039043 3.692e-07 v ǁvolume_forcesǁ 4.3789e-09 4.9027 0.39701 0.15982 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.59 289.91 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.019519 6.6832e-05 3.7892e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14522 0.62811 0.22265 0.18955 INSTANT 0.264825000E+00 TIME STEP NUMBER 275 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.16225E-05 0.29309E-02 Friction velocity uk : 0.17444E-05 0.29307E-02 Dimensionless distance yplus : 0.11617E-04 0.19498E-01 Friction thermal sca. tstar : -0.16700E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.81591E-05 0.13694E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.16225E-05 0.29309E-02 Friction velocity uk : 0.17444E-05 0.29307E-02 Dimensionless distance yplus : 0.11617E-04 0.19498E-01 Friction thermal sca. tstar : -0.16700E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.81591E-05 0.13694E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.40629E-08 4 0.53419E-06 0.24752E-11 0.25605E+01 c Velocity[X] 0.22038E-30 c Velocity[Y] 0.12376E-11 c Velocity[Z] 0.12376E-11 c Pressure 0.41922E-13 23 0.78341E-08 0.33075E-06 0.30057E+01 c k 0.83452E-06 2 0.15149E-06 0.55167E-07 0.30566E+01 c omega 0.13153E+02 1 0.75557E-08 0.49402E+01 0.11571E-01 c TempK 0.94390E+02 1 0.37064E-06 0.91871E-01 0.33698E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.5763e-13 1.3062e-13 -1.544e-17 -3.8989e-18 v Velocity[Y] -0.00017497 0.00017358 -9.5491e-10 -5.4913e-12 v Velocity[Z] -0.00017359 0.00017497 8.812e-10 -1.7608e-12 v ǁVelocityǁ 1.2327e-10 0.00019969 1.1836e-05 6.2253e-06 v Pressure -0.00046075 0.013337 0.00064364 -4.6575e-20 v k 1.0206e-08 0.0028274 0.0019845 0.0024012 v omega 30.308 1.0313e+05 2677.6 513.67 v TempK 288 341.5 292.37 289.77 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.2028e-13 0.00010603 7.1819e-05 9.0427e-05 v CourantNb 1.0807e-09 0.0003183 1.7572e-05 8.7371e-06 v FourierNb 0.14519 0.62811 0.22249 0.18943 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9011 4.9011 0.00039103 -2.9965e-07 v volume_forces[Z] -4.9011 4.9011 -0.00039089 3.703e-07 v ǁvolume_forcesǁ 4.4159e-09 4.903 0.39747 0.16011 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.6 289.92 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.019498 6.6768e-05 3.7854e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14519 0.62811 0.2225 0.18944 INSTANT 0.265788000E+00 TIME STEP NUMBER 276 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.17780E-05 0.29277E-02 Friction velocity uk : 0.18892E-05 0.29275E-02 Dimensionless distance yplus : 0.12581E-04 0.19477E-01 Friction thermal sca. tstar : -0.16294E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.88360E-05 0.13679E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.17780E-05 0.29277E-02 Friction velocity uk : 0.18892E-05 0.29275E-02 Dimensionless distance yplus : 0.12581E-04 0.19477E-01 Friction thermal sca. tstar : -0.16294E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.88360E-05 0.13679E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.40547E-08 4 0.53142E-06 0.24465E-11 0.25507E+01 c Velocity[X] 0.21723E-30 c Velocity[Y] 0.12233E-11 c Velocity[Z] 0.12233E-11 c Pressure 0.41488E-13 23 0.77783E-08 0.32730E-06 0.29945E+01 c k 0.83217E-06 2 0.15057E-06 0.54580E-07 0.30490E+01 c omega 0.13153E+02 1 0.75126E-08 0.48930E+01 0.11516E-01 c TempK 0.94391E+02 1 0.36884E-06 0.91389E-01 0.33609E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.5729e-13 1.3032e-13 -1.5413e-17 -3.8924e-18 v Velocity[Y] -0.00017467 0.00017326 -9.5677e-10 -5.4737e-12 v Velocity[Z] -0.00017326 0.00017467 8.8257e-10 -1.7626e-12 v ǁVelocityǁ 1.2449e-10 0.00019924 1.1815e-05 6.2172e-06 v Pressure -0.00046247 0.013361 0.00064531 4.9026e-23 v k 1.0119e-08 0.0028181 0.0019782 0.0023941 v omega 30.235 1.0313e+05 2677.6 513.61 v TempK 288 341.5 292.38 289.77 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.1925e-13 0.00010595 7.1767e-05 9.0376e-05 v CourantNb 1.0848e-09 0.00031761 1.7537e-05 8.7211e-06 v FourierNb 0.14508 0.62811 0.22234 0.18932 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9013 4.9014 0.00039149 -3.0059e-07 v volume_forces[Z] -4.9013 4.9014 -0.00039136 3.7139e-07 v ǁvolume_forcesǁ 4.4563e-09 4.9032 0.39794 0.16041 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.6 289.92 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.019477 6.6705e-05 3.7816e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14508 0.62811 0.22236 0.18933 INSTANT 0.266751000E+00 TIME STEP NUMBER 277 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19218E-05 0.29245E-02 Friction velocity uk : 0.20242E-05 0.29243E-02 Dimensionless distance yplus : 0.13480E-04 0.19456E-01 Friction thermal sca. tstar : -0.15916E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.94678E-05 0.13665E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19218E-05 0.29245E-02 Friction velocity uk : 0.20242E-05 0.29243E-02 Dimensionless distance yplus : 0.13480E-04 0.19456E-01 Friction thermal sca. tstar : -0.15916E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.94678E-05 0.13665E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.40465E-08 4 0.52875E-06 0.24181E-11 0.25409E+01 c Velocity[X] 0.21413E-30 c Velocity[Y] 0.12091E-11 c Velocity[Z] 0.12090E-11 c Pressure 0.41198E-13 23 0.77329E-08 0.32500E-06 0.29835E+01 c k 0.82983E-06 2 0.14966E-06 0.54002E-07 0.30415E+01 c omega 0.13153E+02 1 0.74698E-08 0.48464E+01 0.11461E-01 c TempK 0.94391E+02 1 0.36706E-06 0.90912E-01 0.33520E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.5695e-13 1.3002e-13 -1.5386e-17 -3.8859e-18 v Velocity[Y] -0.00017436 0.00017294 -9.5862e-10 -5.4563e-12 v Velocity[Z] -0.00017294 0.00017437 8.8393e-10 -1.7644e-12 v ǁVelocityǁ 1.258e-10 0.00019879 1.1795e-05 6.2092e-06 v Pressure -0.00046418 0.013386 0.00064698 2.444e-20 v k 1.0034e-08 0.0028088 0.0019721 0.0023871 v omega 30.163 1.0313e+05 2677.5 513.54 v TempK 288 341.5 292.38 289.78 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.1824e-13 0.00010588 7.1716e-05 9.0325e-05 v CourantNb 1.0889e-09 0.00031693 1.7502e-05 8.7053e-06 v FourierNb 0.14496 0.62811 0.2222 0.1892 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9015 4.9016 0.00039195 -3.0153e-07 v volume_forces[Z] -4.9015 4.9016 -0.00039182 3.7248e-07 v ǁvolume_forcesǁ 4.5003e-09 4.9034 0.39841 0.1607 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.61 289.92 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.019456 6.6642e-05 3.7779e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14497 0.62811 0.22221 0.18921 INSTANT 0.267714000E+00 TIME STEP NUMBER 278 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.20562E-05 0.29214E-02 Friction velocity uk : 0.21513E-05 0.29212E-02 Dimensionless distance yplus : 0.14327E-04 0.19435E-01 Friction thermal sca. tstar : -0.15563E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.10062E-04 0.13650E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.20562E-05 0.29214E-02 Friction velocity uk : 0.21513E-05 0.29212E-02 Dimensionless distance yplus : 0.14327E-04 0.19435E-01 Friction thermal sca. tstar : -0.15563E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.10062E-04 0.13650E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.40384E-08 4 0.52613E-06 0.23899E-11 0.25310E+01 c Velocity[X] 0.21107E-30 c Velocity[Y] 0.11949E-11 c Velocity[Z] 0.11949E-11 c Pressure 0.41001E-13 23 0.76862E-08 0.32342E-06 0.29725E+01 c k 0.82750E-06 2 0.14876E-06 0.53430E-07 0.30341E+01 c omega 0.13153E+02 1 0.74273E-08 0.48004E+01 0.11406E-01 c TempK 0.94392E+02 1 0.36529E-06 0.90439E-01 0.33433E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.5661e-13 1.2973e-13 -1.5359e-17 -3.8794e-18 v Velocity[Y] -0.00017406 0.00017262 -9.6045e-10 -5.4392e-12 v Velocity[Z] -0.00017262 0.00017407 8.8528e-10 -1.7661e-12 v ǁVelocityǁ 1.272e-10 0.00019835 1.1775e-05 6.2014e-06 v Pressure -0.0004659 0.013411 0.00064864 -3.5838e-20 v k 9.9487e-09 0.0027996 0.0019659 0.0023802 v omega 30.091 1.0313e+05 2677.5 513.48 v TempK 288 341.5 292.39 289.78 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.1723e-13 0.0001058 7.1664e-05 9.0274e-05 v CourantNb 1.093e-09 0.00031625 1.7467e-05 8.6897e-06 v FourierNb 0.14485 0.6281 0.22205 0.18909 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9018 4.9018 0.00039242 -3.0247e-07 v volume_forces[Z] -4.9018 4.9018 -0.00039228 3.7357e-07 v ǁvolume_forcesǁ 4.5475e-09 4.9036 0.39887 0.161 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.61 289.93 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.019435 6.6579e-05 3.7742e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14485 0.62811 0.22207 0.1891 INSTANT 0.268677000E+00 TIME STEP NUMBER 279 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.21829E-05 0.29183E-02 Friction velocity uk : 0.22718E-05 0.29181E-02 Dimensionless distance yplus : 0.15129E-04 0.19414E-01 Friction thermal sca. tstar : -0.15472E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.10626E-04 0.13635E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.21829E-05 0.29183E-02 Friction velocity uk : 0.22718E-05 0.29181E-02 Dimensionless distance yplus : 0.15129E-04 0.19414E-01 Friction thermal sca. tstar : -0.15472E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.10626E-04 0.13635E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.40304E-08 4 0.52348E-06 0.23619E-11 0.25210E+01 c Velocity[X] 0.20806E-30 c Velocity[Y] 0.11809E-11 c Velocity[Z] 0.11809E-11 c Pressure 0.40618E-13 23 0.76345E-08 0.32038E-06 0.29615E+01 c k 0.82519E-06 2 0.14787E-06 0.52867E-07 0.30267E+01 c omega 0.13153E+02 1 0.73852E-08 0.47549E+01 0.11352E-01 c TempK 0.94393E+02 1 0.36354E-06 0.89970E-01 0.33346E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.5628e-13 1.2943e-13 -1.5332e-17 -3.873e-18 v Velocity[Y] -0.00017377 0.0001723 -9.6245e-10 -5.6006e-12 v Velocity[Z] -0.00017231 0.00017377 8.8663e-10 -1.7447e-12 v ǁVelocityǁ 1.2889e-10 0.00019791 1.1755e-05 6.1936e-06 v Pressure -0.00046762 0.013435 0.0006503 1.4561e-20 v k 9.8648e-09 0.0027905 0.0019598 0.0023733 v omega 30.02 1.0313e+05 2677.4 513.41 v TempK 288 341.51 292.39 289.78 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.1624e-13 0.00010573 7.1613e-05 9.0224e-05 v CourantNb 1.0971e-09 0.00031558 1.7432e-05 8.6741e-06 v FourierNb 0.14474 0.6281 0.22191 0.18898 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.902 4.902 0.00039288 -3.0341e-07 v volume_forces[Z] -4.902 4.902 -0.00039275 3.7465e-07 v ǁvolume_forcesǁ 4.5982e-09 4.9039 0.39934 0.16129 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.62 289.93 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.019414 6.6516e-05 3.7705e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14474 0.62811 0.22192 0.18899 INSTANT 0.269640000E+00 TIME STEP NUMBER 280 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.23242E-05 0.29152E-02 Friction velocity uk : 0.24071E-05 0.29150E-02 Dimensionless distance yplus : 0.16030E-04 0.19394E-01 Friction thermal sca. tstar : -0.15744E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.11259E-04 0.13621E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.23242E-05 0.29152E-02 Friction velocity uk : 0.24071E-05 0.29150E-02 Dimensionless distance yplus : 0.16030E-04 0.19394E-01 Friction thermal sca. tstar : -0.15744E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.11259E-04 0.13621E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.40225E-08 4 0.52082E-06 0.23341E-11 0.25110E+01 c Velocity[X] 0.20508E-30 c Velocity[Y] 0.11671E-11 c Velocity[Z] 0.11670E-11 c Pressure 0.40335E-13 22 0.76490E-08 0.31813E-06 0.29507E+01 c k 0.82289E-06 2 0.14699E-06 0.52310E-07 0.30193E+01 c omega 0.13153E+02 1 0.73434E-08 0.47099E+01 0.11298E-01 c TempK 0.94393E+02 1 0.36180E-06 0.89505E-01 0.33259E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.5595e-13 1.2914e-13 -1.5306e-17 -3.8666e-18 v Velocity[Y] -0.00017347 0.00017199 -9.6439e-10 -5.7122e-12 v Velocity[Z] -0.00017199 0.00017347 8.8801e-10 -1.689e-12 v ǁVelocityǁ 1.3042e-10 0.00019747 1.1735e-05 6.186e-06 v Pressure -0.00046933 0.01346 0.00065196 -2.9759e-20 v k 9.782e-09 0.0027819 0.0019537 0.0023664 v omega 29.949 1.0313e+05 2677.4 513.35 v TempK 288 341.51 292.4 289.79 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.1526e-13 0.00010566 7.1562e-05 9.0173e-05 v CourantNb 1.1012e-09 0.00031491 1.7398e-05 8.6587e-06 v FourierNb 0.14462 0.6281 0.22176 0.18887 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9022 4.9023 0.00039334 -3.0433e-07 v volume_forces[Z] -4.9022 4.9023 -0.00039321 3.7573e-07 v ǁvolume_forcesǁ 4.6593e-09 4.9041 0.3998 0.16159 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.62 289.93 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.019394 6.6454e-05 3.7668e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14462 0.62811 0.22178 0.18888 INSTANT 0.270603000E+00 TIME STEP NUMBER 281 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.24331E-05 0.29121E-02 Friction velocity uk : 0.25115E-05 0.29119E-02 Dimensionless distance yplus : 0.16725E-04 0.19373E-01 Friction thermal sca. tstar : -0.16032E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.11747E-04 0.13606E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.24331E-05 0.29121E-02 Friction velocity uk : 0.25115E-05 0.29119E-02 Dimensionless distance yplus : 0.16725E-04 0.19373E-01 Friction thermal sca. tstar : -0.16032E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.11747E-04 0.13606E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.40146E-08 4 0.51822E-06 0.23065E-11 0.25010E+01 c Velocity[X] 0.20216E-30 c Velocity[Y] 0.11533E-11 c Velocity[Z] 0.11533E-11 c Pressure 0.40052E-13 22 0.76033E-08 0.31588E-06 0.29399E+01 c k 0.82059E-06 2 0.14612E-06 0.51761E-07 0.30119E+01 c omega 0.13153E+02 1 0.73020E-08 0.46654E+01 0.11245E-01 c TempK 0.94394E+02 1 0.36007E-06 0.89044E-01 0.33173E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.5562e-13 1.2886e-13 -1.5279e-17 -3.8603e-18 v Velocity[Y] -0.00017318 0.00017168 -9.6617e-10 -5.6941e-12 v Velocity[Z] -0.00017168 0.00017318 8.893e-10 -1.6915e-12 v ǁVelocityǁ 1.3199e-10 0.00019703 1.1716e-05 6.1784e-06 v Pressure -0.00047105 0.013485 0.00065362 -2.1057e-20 v k 9.7e-09 0.0027733 0.0019477 0.0023595 v omega 29.878 1.0313e+05 2677.3 513.28 v TempK 288 341.51 292.4 289.79 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.143e-13 0.00010558 7.1511e-05 9.0123e-05 v CourantNb 1.1053e-09 0.00031424 1.7364e-05 8.6435e-06 v FourierNb 0.14451 0.6281 0.22162 0.18876 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9024 4.9025 0.0003938 -3.0526e-07 v volume_forces[Z] -4.9024 4.9025 -0.00039366 3.7681e-07 v ǁvolume_forcesǁ 4.7146e-09 4.9043 0.40026 0.16188 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.63 289.94 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.019373 6.6393e-05 3.7632e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14451 0.6281 0.22164 0.18876 INSTANT 0.271566000E+00 TIME STEP NUMBER 282 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.25347E-05 0.29090E-02 Friction velocity uk : 0.26092E-05 0.29089E-02 Dimensionless distance yplus : 0.17376E-04 0.19353E-01 Friction thermal sca. tstar : -0.16339E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.12204E-04 0.13592E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.25347E-05 0.29090E-02 Friction velocity uk : 0.26092E-05 0.29089E-02 Dimensionless distance yplus : 0.17376E-04 0.19353E-01 Friction thermal sca. tstar : -0.16339E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.12204E-04 0.13592E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.40068E-08 4 0.51563E-06 0.22792E-11 0.24909E+01 c Velocity[X] 0.19929E-30 c Velocity[Y] 0.11396E-11 c Velocity[Z] 0.11396E-11 c Pressure 0.39772E-13 22 0.75583E-08 0.31365E-06 0.29293E+01 c k 0.81831E-06 2 0.14526E-06 0.51219E-07 0.30046E+01 c omega 0.13153E+02 1 0.72609E-08 0.46215E+01 0.11192E-01 c TempK 0.94395E+02 1 0.35836E-06 0.88587E-01 0.33087E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.5529e-13 1.2857e-13 -1.5253e-17 -3.854e-18 v Velocity[Y] -0.00017289 0.00017137 -9.6795e-10 -5.676e-12 v Velocity[Z] -0.00017137 0.00017289 8.9059e-10 -1.6941e-12 v ǁVelocityǁ 1.3369e-10 0.0001966 1.1697e-05 6.171e-06 v Pressure -0.00047276 0.013509 0.00065527 7.2069e-21 v k 9.619e-09 0.0027648 0.0019417 0.0023527 v omega 29.808 1.0313e+05 2677.3 513.22 v TempK 288 341.51 292.41 289.79 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.1334e-13 0.00010551 7.1461e-05 9.0072e-05 v CourantNb 1.1094e-09 0.00031358 1.733e-05 8.6284e-06 v FourierNb 0.14439 0.6281 0.22148 0.18865 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9027 4.9027 0.00039426 -3.0618e-07 v volume_forces[Z] -4.9027 4.9027 -0.00039412 3.7788e-07 v ǁvolume_forcesǁ 4.7715e-09 4.9045 0.40072 0.16217 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.63 289.94 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.019353 6.6331e-05 3.7596e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.1444 0.6281 0.2215 0.18865 INSTANT 0.272529000E+00 TIME STEP NUMBER 283 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.26360E-05 0.29060E-02 Friction velocity uk : 0.27069E-05 0.29058E-02 Dimensionless distance yplus : 0.18027E-04 0.19333E-01 Friction thermal sca. tstar : -0.16665E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.12661E-04 0.13578E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.26360E-05 0.29060E-02 Friction velocity uk : 0.27069E-05 0.29058E-02 Dimensionless distance yplus : 0.18027E-04 0.19333E-01 Friction thermal sca. tstar : -0.16665E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.12661E-04 0.13578E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.39991E-08 4 0.51306E-06 0.22521E-11 0.24807E+01 c Velocity[X] 0.19645E-30 c Velocity[Y] 0.11261E-11 c Velocity[Z] 0.11261E-11 c Pressure 0.39495E-13 22 0.75131E-08 0.31145E-06 0.29186E+01 c k 0.81605E-06 2 0.14441E-06 0.50684E-07 0.29974E+01 c omega 0.13153E+02 1 0.72201E-08 0.45781E+01 0.11139E-01 c TempK 0.94396E+02 1 0.35666E-06 0.88133E-01 0.33002E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.5497e-13 1.2829e-13 -1.5227e-17 -3.8478e-18 v Velocity[Y] -0.0001726 0.00017106 -9.697e-10 -5.6581e-12 v Velocity[Z] -0.00017106 0.0001726 8.9186e-10 -1.6963e-12 v ǁVelocityǁ 1.3548e-10 0.00019617 1.1677e-05 6.1636e-06 v Pressure -0.00047448 0.013534 0.00065692 -1.6669e-21 v k 9.5388e-09 0.0027563 0.0019357 0.002346 v omega 29.738 1.0313e+05 2677.2 513.15 v TempK 288 341.52 292.41 289.8 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.1239e-13 0.00010543 7.141e-05 9.0022e-05 v CourantNb 1.1136e-09 0.00031292 1.7297e-05 8.6134e-06 v FourierNb 0.14428 0.6281 0.22134 0.18853 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9029 4.9029 0.00039471 -3.071e-07 v volume_forces[Z] -4.9029 4.9029 -0.00039458 3.7894e-07 v ǁvolume_forcesǁ 4.8328e-09 4.9048 0.40118 0.16246 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.64 289.94 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.019333 6.627e-05 3.7559e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14428 0.6281 0.22136 0.18854 INSTANT 0.273492000E+00 TIME STEP NUMBER 284 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.27355E-05 0.29030E-02 Friction velocity uk : 0.28032E-05 0.29028E-02 Dimensionless distance yplus : 0.18668E-04 0.19312E-01 Friction thermal sca. tstar : -0.17015E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.13111E-04 0.13564E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.27355E-05 0.29030E-02 Friction velocity uk : 0.28032E-05 0.29028E-02 Dimensionless distance yplus : 0.18668E-04 0.19312E-01 Friction thermal sca. tstar : -0.17015E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.13111E-04 0.13564E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.39915E-08 4 0.51053E-06 0.22253E-11 0.24706E+01 c Velocity[X] 0.19366E-30 c Velocity[Y] 0.11127E-11 c Velocity[Z] 0.11126E-11 c Pressure 0.39238E-13 22 0.74704E-08 0.30940E-06 0.29081E+01 c k 0.81379E-06 2 0.14357E-06 0.50156E-07 0.29901E+01 c omega 0.13153E+02 1 0.71796E-08 0.45352E+01 0.11087E-01 c TempK 0.94396E+02 1 0.35497E-06 0.87684E-01 0.32917E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.5465e-13 1.28e-13 -1.5201e-17 -3.8416e-18 v Velocity[Y] -0.00017231 0.00017075 -9.7145e-10 -5.6403e-12 v Velocity[Z] -0.00017076 0.00017232 8.9311e-10 -1.6988e-12 v ǁVelocityǁ 1.3737e-10 0.00019574 1.1658e-05 6.1564e-06 v Pressure -0.00047619 0.013558 0.00065857 1.4659e-20 v k 9.4596e-09 0.0027478 0.0019298 0.0023392 v omega 29.668 1.0313e+05 2677.2 513.09 v TempK 288 341.52 292.42 289.8 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.1145e-13 0.00010536 7.136e-05 8.9972e-05 v CourantNb 1.1177e-09 0.00031227 1.7264e-05 8.5986e-06 v FourierNb 0.14417 0.6281 0.2212 0.18842 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9031 4.9032 0.00039517 -3.0802e-07 v volume_forces[Z] -4.9031 4.9032 -0.00039503 3.8e-07 v ǁvolume_forcesǁ 4.8977e-09 4.905 0.40164 0.16275 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.64 289.95 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.019312 6.621e-05 3.7524e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14417 0.6281 0.22122 0.18843 INSTANT 0.274455000E+00 TIME STEP NUMBER 285 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.28328E-05 0.28999E-02 Friction velocity uk : 0.28974E-05 0.28998E-02 Dimensionless distance yplus : 0.19296E-04 0.19292E-01 Friction thermal sca. tstar : -0.17389E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.13552E-04 0.13550E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.28328E-05 0.28999E-02 Friction velocity uk : 0.28974E-05 0.28998E-02 Dimensionless distance yplus : 0.19296E-04 0.19292E-01 Friction thermal sca. tstar : -0.17389E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.13552E-04 0.13550E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.39839E-08 4 0.50797E-06 0.21987E-11 0.24604E+01 c Velocity[X] 0.19091E-30 c Velocity[Y] 0.10994E-11 c Velocity[Z] 0.10993E-11 c Pressure 0.38944E-13 22 0.74254E-08 0.30706E-06 0.28976E+01 c k 0.81154E-06 2 0.14274E-06 0.49634E-07 0.29829E+01 c omega 0.13153E+02 1 0.71395E-08 0.44927E+01 0.11035E-01 c TempK 0.94397E+02 1 0.35330E-06 0.87238E-01 0.32833E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.5433e-13 1.2772e-13 -1.5176e-17 -3.8354e-18 v Velocity[Y] -0.00017203 0.00017045 -9.7318e-10 -5.6227e-12 v Velocity[Z] -0.00017045 0.00017203 8.9435e-10 -1.7009e-12 v ǁVelocityǁ 1.3934e-10 0.00019532 1.164e-05 6.1493e-06 v Pressure -0.00047791 0.013582 0.00066022 8.6777e-20 v k 9.3812e-09 0.0027394 0.0019238 0.0023325 v omega 29.598 1.0313e+05 2677.1 513.02 v TempK 288 341.52 292.42 289.8 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.1053e-13 0.00010528 7.131e-05 8.9923e-05 v CourantNb 1.1218e-09 0.00031162 1.7231e-05 8.5839e-06 v FourierNb 0.14405 0.6281 0.22106 0.18831 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9033 4.9034 0.00039562 -3.0893e-07 v volume_forces[Z] -4.9033 4.9034 -0.00039549 3.8105e-07 v ǁvolume_forcesǁ 4.9659e-09 4.9052 0.4021 0.16304 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.65 289.95 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.019292 6.6149e-05 3.7488e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14406 0.6281 0.22108 0.18832 INSTANT 0.275418000E+00 TIME STEP NUMBER 286 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.29277E-05 0.28970E-02 Friction velocity uk : 0.29895E-05 0.28968E-02 Dimensionless distance yplus : 0.19909E-04 0.19272E-01 Friction thermal sca. tstar : -0.17791E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.13983E-04 0.13536E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.29277E-05 0.28970E-02 Friction velocity uk : 0.29895E-05 0.28968E-02 Dimensionless distance yplus : 0.19909E-04 0.19272E-01 Friction thermal sca. tstar : -0.17791E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.13983E-04 0.13536E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.39764E-08 4 0.50550E-06 0.21723E-11 0.24502E+01 c Velocity[X] 0.18820E-30 c Velocity[Y] 0.10862E-11 c Velocity[Z] 0.10862E-11 c Pressure 0.38758E-13 22 0.73826E-08 0.30558E-06 0.28873E+01 c k 0.80931E-06 2 0.14192E-06 0.49120E-07 0.29758E+01 c omega 0.13153E+02 1 0.70996E-08 0.44508E+01 0.10983E-01 c TempK 0.94398E+02 1 0.35164E-06 0.86796E-01 0.32749E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.5401e-13 1.2745e-13 -1.515e-17 -3.8293e-18 v Velocity[Y] -0.00017175 0.00017015 -9.749e-10 -5.605e-12 v Velocity[Z] -0.00017015 0.00017175 8.9558e-10 -1.7033e-12 v ǁVelocityǁ 1.4139e-10 0.0001949 1.1621e-05 6.1423e-06 v Pressure -0.00047963 0.013607 0.00066186 -3.5299e-20 v k 9.3038e-09 0.002731 0.001918 0.0023259 v omega 29.529 1.0313e+05 2677.1 512.96 v TempK 288 341.52 292.43 289.81 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.0961e-13 0.00010521 7.126e-05 8.9873e-05 v CourantNb 1.1259e-09 0.00031098 1.7198e-05 8.5694e-06 v FourierNb 0.14394 0.6281 0.22092 0.1882 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9035 4.9036 0.00039607 -3.0984e-07 v volume_forces[Z] -4.9035 4.9036 -0.00039594 3.821e-07 v ǁvolume_forcesǁ 5.037e-09 4.9054 0.40255 0.16333 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.65 289.95 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.019272 6.6089e-05 3.7452e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14394 0.6281 0.22094 0.18821 INSTANT 0.276381000E+00 TIME STEP NUMBER 287 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.30202E-05 0.28940E-02 Friction velocity uk : 0.30795E-05 0.28938E-02 Dimensionless distance yplus : 0.20508E-04 0.19253E-01 Friction thermal sca. tstar : -0.18226E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.14404E-04 0.13522E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.30202E-05 0.28940E-02 Friction velocity uk : 0.30795E-05 0.28938E-02 Dimensionless distance yplus : 0.20508E-04 0.19253E-01 Friction thermal sca. tstar : -0.18226E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.14404E-04 0.13522E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.39690E-08 4 0.50301E-06 0.21462E-11 0.24399E+01 c Velocity[X] 0.18554E-30 c Velocity[Y] 0.10731E-11 c Velocity[Z] 0.10731E-11 c Pressure 0.38498E-13 22 0.73431E-08 0.30351E-06 0.28769E+01 c k 0.80709E-06 2 0.14111E-06 0.48611E-07 0.29686E+01 c omega 0.13153E+02 1 0.70601E-08 0.44094E+01 0.10932E-01 c TempK 0.94398E+02 1 0.35000E-06 0.86358E-01 0.32666E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.5369e-13 1.2717e-13 -1.5125e-17 -3.8232e-18 v Velocity[Y] -0.00017147 0.00016985 -9.766e-10 -5.5876e-12 v Velocity[Z] -0.00016985 0.00017147 8.9679e-10 -1.7059e-12 v ǁVelocityǁ 1.4351e-10 0.00019448 1.1603e-05 6.1353e-06 v Pressure -0.00048134 0.013631 0.00066351 6.2264e-21 v k 9.2272e-09 0.0027227 0.0019121 0.0023192 v omega 29.461 1.0313e+05 2677 512.9 v TempK 288 341.52 292.43 289.81 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.0871e-13 0.00010514 7.121e-05 8.9823e-05 v CourantNb 1.13e-09 0.00031034 1.7166e-05 8.555e-06 v FourierNb 0.14383 0.6281 0.22078 0.1881 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9038 4.9038 0.00039653 -3.1074e-07 v volume_forces[Z] -4.9038 4.9038 -0.00039639 3.8315e-07 v ǁvolume_forcesǁ 5.1111e-09 4.9056 0.40301 0.16362 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.66 289.96 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.019253 6.603e-05 3.7417e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14383 0.6281 0.2208 0.1881 INSTANT 0.277344000E+00 TIME STEP NUMBER 288 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.31105E-05 0.28910E-02 Friction velocity uk : 0.31674E-05 0.28908E-02 Dimensionless distance yplus : 0.21094E-04 0.19233E-01 Friction thermal sca. tstar : -0.18697E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.14815E-04 0.13508E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.31105E-05 0.28910E-02 Friction velocity uk : 0.31674E-05 0.28908E-02 Dimensionless distance yplus : 0.21094E-04 0.19233E-01 Friction thermal sca. tstar : -0.18697E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.14815E-04 0.13508E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.39616E-08 4 0.50331E-06 0.21204E-11 0.24296E+01 c Velocity[X] 0.18291E-30 c Velocity[Y] 0.10602E-11 c Velocity[Z] 0.10602E-11 c Pressure 0.38139E-13 22 0.72967E-08 0.30066E-06 0.28667E+01 c k 0.80488E-06 2 0.14030E-06 0.48110E-07 0.29615E+01 c omega 0.13153E+02 1 0.70209E-08 0.43684E+01 0.10881E-01 c TempK 0.94399E+02 1 0.34836E-06 0.85924E-01 0.32584E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.5338e-13 1.269e-13 -1.51e-17 -3.8172e-18 v Velocity[Y] -0.00017119 0.00016955 -9.7829e-10 -5.5701e-12 v Velocity[Z] -0.00016956 0.00017119 8.9798e-10 -1.7081e-12 v ǁVelocityǁ 1.4571e-10 0.00019406 1.1584e-05 6.1285e-06 v Pressure -0.00048306 0.013655 0.00066514 -1.4316e-20 v k 9.1514e-09 0.0027144 0.0019063 0.0023126 v omega 29.392 1.0313e+05 2677 512.84 v TempK 288 341.53 292.44 289.81 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.0781e-13 0.00010506 7.1161e-05 8.9774e-05 v CourantNb 1.1341e-09 0.0003097 1.7134e-05 8.5408e-06 v FourierNb 0.14371 0.6281 0.22064 0.18799 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.904 4.904 0.00039698 -3.1164e-07 v volume_forces[Z] -4.904 4.904 -0.00039684 3.8419e-07 v ǁvolume_forcesǁ 5.1879e-09 4.9058 0.40346 0.16391 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.66 289.96 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.019233 6.5971e-05 3.7382e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14372 0.6281 0.22066 0.188 INSTANT 0.278307000E+00 TIME STEP NUMBER 289 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.31988E-05 0.28881E-02 Friction velocity uk : 0.32535E-05 0.28879E-02 Dimensionless distance yplus : 0.21667E-04 0.19213E-01 Friction thermal sca. tstar : -0.19209E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.15217E-04 0.13494E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.31988E-05 0.28881E-02 Friction velocity uk : 0.32535E-05 0.28879E-02 Dimensionless distance yplus : 0.21667E-04 0.19213E-01 Friction thermal sca. tstar : -0.19209E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.15217E-04 0.13494E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.39543E-08 4 0.49798E-06 0.20948E-11 0.24193E+01 c Velocity[X] 0.18032E-30 c Velocity[Y] 0.10474E-11 c Velocity[Z] 0.10474E-11 c Pressure 0.37873E-13 22 0.72542E-08 0.29855E-06 0.28565E+01 c k 0.80268E-06 2 0.13951E-06 0.47614E-07 0.29545E+01 c omega 0.13153E+02 1 0.69820E-08 0.43279E+01 0.10830E-01 c TempK 0.94400E+02 1 0.34674E-06 0.85493E-01 0.32501E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.5307e-13 1.2662e-13 -1.5075e-17 -3.8112e-18 v Velocity[Y] -0.00017091 0.00016926 -9.7996e-10 -5.5526e-12 v Velocity[Z] -0.00016926 0.00017091 8.9916e-10 -1.7105e-12 v ǁVelocityǁ 1.4798e-10 0.00019365 1.1566e-05 6.1218e-06 v Pressure -0.00048477 0.013679 0.00066678 4.4295e-20 v k 9.0765e-09 0.0027061 0.0019005 0.0023061 v omega 29.324 1.0313e+05 2676.9 512.77 v TempK 288 341.53 292.44 289.82 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.0693e-13 0.00010499 7.1111e-05 8.9724e-05 v CourantNb 1.1382e-09 0.00030907 1.7102e-05 8.5267e-06 v FourierNb 0.1436 0.6281 0.22051 0.18788 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9042 4.9043 0.00039743 -3.1254e-07 v volume_forces[Z] -4.9042 4.9043 -0.00039729 3.8523e-07 v ǁvolume_forcesǁ 5.2674e-09 4.906 0.40391 0.1642 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.67 289.96 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.019213 6.5912e-05 3.7347e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.1436 0.6281 0.22052 0.18789 INSTANT 0.279270000E+00 TIME STEP NUMBER 290 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.32850E-05 0.28852E-02 Friction velocity uk : 0.33377E-05 0.28850E-02 Dimensionless distance yplus : 0.22228E-04 0.19194E-01 Friction thermal sca. tstar : -0.19769E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.15611E-04 0.13481E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.32850E-05 0.28852E-02 Friction velocity uk : 0.33377E-05 0.28850E-02 Dimensionless distance yplus : 0.22228E-04 0.19194E-01 Friction thermal sca. tstar : -0.19769E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.15611E-04 0.13481E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.39471E-08 4 0.49553E-06 0.20694E-11 0.24090E+01 c Velocity[X] 0.17720E-30 c Velocity[Y] 0.10347E-11 c Velocity[Z] 0.10347E-11 c Pressure 0.37616E-13 21 0.10447E-07 0.29650E-06 0.28464E+01 c k 0.80049E-06 2 0.13872E-06 0.47125E-07 0.29474E+01 c omega 0.13153E+02 1 0.69434E-08 0.42878E+01 0.10780E-01 c TempK 0.94401E+02 1 0.34513E-06 0.85065E-01 0.32420E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.5276e-13 1.2635e-13 -1.5051e-17 -3.8055e-18 v Velocity[Y] -0.00017064 0.00016897 -9.8165e-10 -5.5595e-12 v Velocity[Z] -0.00016897 0.00017064 9.0033e-10 -1.7122e-12 v ǁVelocityǁ 1.5024e-10 0.00019324 1.1549e-05 6.1152e-06 v Pressure -0.00048649 0.013704 0.00066841 -1.4806e-20 v k 9.0024e-09 0.0026979 0.0018948 0.0022995 v omega 29.256 1.0313e+05 2676.9 512.71 v TempK 288 341.53 292.45 289.82 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.0605e-13 0.00010491 7.1062e-05 8.9675e-05 v CourantNb 1.1425e-09 0.00030844 1.707e-05 8.5128e-06 v FourierNb 0.14349 0.6281 0.22037 0.18777 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9044 4.9045 0.00039787 -3.1344e-07 v volume_forces[Z] -4.9044 4.9045 -0.00039774 3.8626e-07 v ǁvolume_forcesǁ 5.3494e-09 4.9063 0.40436 0.16449 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.67 289.97 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.019194 6.5853e-05 3.7313e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14349 0.6281 0.22039 0.18778 INSTANT 0.280233000E+00 TIME STEP NUMBER 291 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+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-05 0.28822E-02 Friction velocity uk : 0.34157E-05 0.28821E-02 Dimensionless distance yplus : 0.22747E-04 0.19175E-01 Friction thermal sca. tstar : -0.20384E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.15976E-04 0.13467E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+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-05 0.28822E-02 Friction velocity uk : 0.34157E-05 0.28821E-02 Dimensionless distance yplus : 0.22747E-04 0.19175E-01 Friction thermal sca. tstar : -0.20384E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.15976E-04 0.13467E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.39400E-08 4 0.49484E-06 0.20443E-11 0.23986E+01 c Velocity[X] 0.17513E-30 c Velocity[Y] 0.10221E-11 c Velocity[Z] 0.10221E-11 c Pressure 0.37463E-13 21 0.10401E-07 0.29528E-06 0.28364E+01 c k 0.79831E-06 2 0.13795E-06 0.46642E-07 0.29405E+01 c omega 0.13153E+02 1 0.69051E-08 0.42482E+01 0.10730E-01 c TempK 0.94401E+02 1 0.34354E-06 0.84642E-01 0.32339E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.5245e-13 1.2609e-13 -1.5027e-17 -3.7997e-18 v Velocity[Y] -0.00017037 0.00016867 -9.8329e-10 -5.5425e-12 v Velocity[Z] -0.00016868 0.00017037 9.0148e-10 -1.7144e-12 v ǁVelocityǁ 1.5265e-10 0.00019283 1.1531e-05 6.1087e-06 v Pressure -0.0004882 0.013728 0.00067005 2.618e-20 v k 8.9291e-09 0.0026897 0.0018891 0.002293 v omega 29.189 1.0313e+05 2676.8 512.65 v TempK 288 341.53 292.45 289.82 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.0519e-13 0.00010484 7.1013e-05 8.9626e-05 v CourantNb 1.1466e-09 0.00030781 1.7039e-05 8.499e-06 v FourierNb 0.14338 0.6281 0.22024 0.18766 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9046 4.9047 0.00039832 -3.1433e-07 v volume_forces[Z] -4.9046 4.9047 -0.00039819 3.8729e-07 v ǁvolume_forcesǁ 5.4311e-09 4.9065 0.40481 0.16477 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.68 289.97 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.019175 6.5795e-05 3.7278e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14338 0.6281 0.22025 0.18767 INSTANT 0.281196000E+00 TIME STEP NUMBER 292 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.34477E-05 0.28794E-02 Friction velocity uk : 0.34967E-05 0.28792E-02 Dimensionless distance yplus : 0.23287E-04 0.19155E-01 Friction thermal sca. tstar : -0.21066E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.16355E-04 0.13454E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.34477E-05 0.28794E-02 Friction velocity uk : 0.34967E-05 0.28792E-02 Dimensionless distance yplus : 0.23287E-04 0.19155E-01 Friction thermal sca. tstar : -0.21066E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.16355E-04 0.13454E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.39329E-08 4 0.49183E-06 0.20194E-11 0.23883E+01 c Velocity[X] 0.17274E-30 c Velocity[Y] 0.10097E-11 c Velocity[Z] 0.10097E-11 c Pressure 0.37171E-13 21 0.10346E-07 0.29296E-06 0.28264E+01 c k 0.79614E-06 2 0.13718E-06 0.46165E-07 0.29335E+01 c omega 0.13153E+02 1 0.68671E-08 0.42091E+01 0.10681E-01 c TempK 0.94402E+02 1 0.34196E-06 0.84221E-01 0.32258E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.5214e-13 1.2582e-13 -1.5002e-17 -3.7938e-18 v Velocity[Y] -0.0001701 0.00016839 -9.8493e-10 -5.5251e-12 v Velocity[Z] -0.00016839 0.0001701 9.0262e-10 -1.717e-12 v ǁVelocityǁ 1.5512e-10 0.00019242 1.1513e-05 6.1023e-06 v Pressure -0.00048992 0.013752 0.00067168 2.2405e-20 v k 8.8566e-09 0.0026816 0.0018834 0.0022866 v omega 29.122 1.0313e+05 2676.8 512.59 v TempK 288 341.54 292.46 289.83 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.0433e-13 0.00010477 7.0964e-05 8.9577e-05 v CourantNb 1.1507e-09 0.00030719 1.7008e-05 8.4853e-06 v FourierNb 0.14326 0.6281 0.2201 0.18756 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9048 4.9049 0.00039877 -3.1522e-07 v volume_forces[Z] -4.9048 4.9049 -0.00039863 3.8832e-07 v ǁvolume_forcesǁ 5.5183e-09 4.9067 0.40526 0.16506 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.68 289.97 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.019155 6.5737e-05 3.7244e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14327 0.6281 0.22012 0.18757 INSTANT 0.282159000E+00 TIME STEP NUMBER 293 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.35290E-05 0.28765E-02 Friction velocity uk : 0.35763E-05 0.28763E-02 Dimensionless distance yplus : 0.23817E-04 0.19136E-01 Friction thermal sca. tstar : -0.21825E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.16727E-04 0.13440E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.35290E-05 0.28765E-02 Friction velocity uk : 0.35763E-05 0.28763E-02 Dimensionless distance yplus : 0.23817E-04 0.19136E-01 Friction thermal sca. tstar : -0.21825E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.16727E-04 0.13440E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.39259E-08 4 0.48929E-06 0.19948E-11 0.23779E+01 c Velocity[X] 0.17034E-30 c Velocity[Y] 0.99742E-12 c Velocity[Z] 0.99742E-12 c Pressure 0.36911E-13 21 0.10294E-07 0.29089E-06 0.28165E+01 c k 0.79398E-06 2 0.13642E-06 0.45695E-07 0.29266E+01 c omega 0.13153E+02 1 0.68294E-08 0.41704E+01 0.10632E-01 c TempK 0.94403E+02 1 0.34038E-06 0.83804E-01 0.32177E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.5184e-13 1.2556e-13 -1.4978e-17 -3.788e-18 v Velocity[Y] -0.00016983 0.0001681 -9.8655e-10 -5.5078e-12 v Velocity[Z] -0.0001681 0.00016983 9.0374e-10 -1.7194e-12 v ǁVelocityǁ 1.5765e-10 0.00019202 1.1496e-05 6.096e-06 v Pressure -0.00049163 0.013776 0.0006733 9.315e-22 v k 8.7849e-09 0.0026735 0.0018777 0.0022801 v omega 29.055 1.0313e+05 2676.7 512.53 v TempK 288 341.54 292.46 289.83 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.0348e-13 0.00010469 7.0915e-05 8.9529e-05 v CourantNb 1.1548e-09 0.00030658 1.6977e-05 8.4718e-06 v FourierNb 0.14315 0.6281 0.21997 0.18745 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9051 4.9051 0.00039921 -3.161e-07 v volume_forces[Z] -4.9051 4.9051 -0.00039908 3.8934e-07 v ǁvolume_forcesǁ 5.6075e-09 4.9069 0.40571 0.16535 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.69 289.97 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.019136 6.5679e-05 3.721e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14315 0.6281 0.21998 0.18746 INSTANT 0.283122000E+00 TIME STEP NUMBER 294 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.36088E-05 0.28736E-02 Friction velocity uk : 0.36546E-05 0.28735E-02 Dimensionless distance yplus : 0.24338E-04 0.19117E-01 Friction thermal sca. tstar : -0.22677E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.17093E-04 0.13427E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.36088E-05 0.28736E-02 Friction velocity uk : 0.36546E-05 0.28735E-02 Dimensionless distance yplus : 0.24338E-04 0.19117E-01 Friction thermal sca. tstar : -0.22677E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.17093E-04 0.13427E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.39189E-08 4 0.48684E-06 0.19705E-11 0.23675E+01 c Velocity[X] 0.16796E-30 c Velocity[Y] 0.98526E-12 c Velocity[Z] 0.98525E-12 c Pressure 0.36647E-13 21 0.10242E-07 0.28880E-06 0.28066E+01 c k 0.79184E-06 2 0.13566E-06 0.45230E-07 0.29197E+01 c omega 0.13153E+02 1 0.67920E-08 0.41322E+01 0.10583E-01 c TempK 0.94403E+02 1 0.33883E-06 0.83391E-01 0.32098E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.5154e-13 1.253e-13 -1.4954e-17 -3.7822e-18 v Velocity[Y] -0.00016956 0.00016781 -9.8815e-10 -5.4906e-12 v Velocity[Z] -0.00016782 0.00016956 9.0485e-10 -1.7219e-12 v ǁVelocityǁ 1.6024e-10 0.00019162 1.1479e-05 6.0898e-06 v Pressure -0.00049335 0.0138 0.00067493 -2.4709e-20 v k 8.714e-09 0.0026654 0.0018721 0.0022737 v omega 28.988 1.0313e+05 2676.7 512.47 v TempK 288 341.54 292.47 289.83 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.0265e-13 0.00010462 7.0866e-05 8.948e-05 v CourantNb 1.1589e-09 0.00030596 1.6947e-05 8.4584e-06 v FourierNb 0.14304 0.6281 0.21983 0.18734 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9053 4.9053 0.00039966 -3.1698e-07 v volume_forces[Z] -4.9053 4.9053 -0.00039952 3.9036e-07 v ǁvolume_forcesǁ 5.699e-09 4.9071 0.40616 0.16563 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.69 289.98 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.019117 6.5622e-05 3.7176e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14304 0.6281 0.21985 0.18735 INSTANT 0.284085000E+00 TIME STEP NUMBER 295 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.36872E-05 0.28708E-02 Friction velocity uk : 0.37315E-05 0.28706E-02 Dimensionless distance yplus : 0.24850E-04 0.19098E-01 Friction thermal sca. tstar : -0.23644E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.17453E-04 0.13414E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.36872E-05 0.28708E-02 Friction velocity uk : 0.37315E-05 0.28706E-02 Dimensionless distance yplus : 0.24850E-04 0.19098E-01 Friction thermal sca. tstar : -0.23644E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.17453E-04 0.13414E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.39121E-08 4 0.48447E-06 0.19464E-11 0.23571E+01 c Velocity[X] 0.16561E-30 c Velocity[Y] 0.97322E-12 c Velocity[Z] 0.97321E-12 c Pressure 0.36432E-13 21 0.10194E-07 0.28709E-06 0.27969E+01 c k 0.78970E-06 2 0.13492E-06 0.44770E-07 0.29128E+01 c omega 0.13153E+02 1 0.67549E-08 0.40944E+01 0.10534E-01 c TempK 0.94404E+02 1 0.33728E-06 0.82981E-01 0.32018E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.5124e-13 1.2504e-13 -1.493e-17 -3.7765e-18 v Velocity[Y] -0.0001693 0.00016753 -9.8975e-10 -5.4736e-12 v Velocity[Z] -0.00016753 0.0001693 9.0595e-10 -1.7245e-12 v ǁVelocityǁ 1.6195e-10 0.00019122 1.1462e-05 6.0837e-06 v Pressure -0.00049506 0.013824 0.00067655 -2.8337e-20 v k 8.6438e-09 0.0026574 0.0018665 0.0022674 v omega 28.922 1.0313e+05 2676.6 512.4 v TempK 288 341.54 292.47 289.84 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.0182e-13 0.00010454 7.0818e-05 8.9431e-05 v CourantNb 1.163e-09 0.00030535 1.6916e-05 8.4452e-06 v FourierNb 0.14293 0.6281 0.2197 0.18724 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9055 4.9055 0.0004001 -3.1786e-07 v volume_forces[Z] -4.9055 4.9055 -0.00039996 3.9137e-07 v ǁvolume_forcesǁ 5.7926e-09 4.9073 0.4066 0.16592 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.7 289.98 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.019098 6.5565e-05 3.7142e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14293 0.6281 0.21972 0.18725 INSTANT 0.285048000E+00 TIME STEP NUMBER 296 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.37642E-05 0.28680E-02 Friction velocity uk : 0.38071E-05 0.28678E-02 Dimensionless distance yplus : 0.25354E-04 0.19080E-01 Friction thermal sca. tstar : -0.24753E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.17807E-04 0.13400E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.37642E-05 0.28680E-02 Friction velocity uk : 0.38071E-05 0.28678E-02 Dimensionless distance yplus : 0.25354E-04 0.19080E-01 Friction thermal sca. tstar : -0.24753E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.17807E-04 0.13400E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.39053E-08 4 0.48209E-06 0.19226E-11 0.23467E+01 c Velocity[X] 0.16329E-30 c Velocity[Y] 0.96131E-12 c Velocity[Z] 0.96130E-12 c Pressure 0.36147E-13 21 0.10138E-07 0.28482E-06 0.27872E+01 c k 0.78758E-06 2 0.13418E-06 0.44317E-07 0.29060E+01 c omega 0.13153E+02 1 0.67180E-08 0.40570E+01 0.10486E-01 c TempK 0.94405E+02 1 0.33574E-06 0.82574E-01 0.31939E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.5094e-13 1.2478e-13 -1.4906e-17 -3.7707e-18 v Velocity[Y] -0.00016903 0.00016725 -9.9132e-10 -5.4564e-12 v Velocity[Z] -0.00016725 0.00016904 9.0703e-10 -1.727e-12 v ǁVelocityǁ 1.6018e-10 0.00019083 1.1445e-05 6.0777e-06 v Pressure -0.00049678 0.013848 0.00067817 -6.9372e-21 v k 8.5744e-09 0.0026494 0.0018609 0.002261 v omega 28.856 1.0313e+05 2676.6 512.34 v TempK 288 341.55 292.48 289.84 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.01e-13 0.00010447 7.077e-05 8.9383e-05 v CourantNb 1.1671e-09 0.00030475 1.6886e-05 8.4321e-06 v FourierNb 0.14282 0.6281 0.21957 0.18713 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9057 4.9057 0.00040054 -3.1874e-07 v volume_forces[Z] -4.9057 4.9057 -0.0004004 3.9238e-07 v ǁvolume_forcesǁ 5.8546e-09 4.9075 0.40705 0.16621 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.7 289.98 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.01908 6.5508e-05 3.7108e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14282 0.6281 0.21958 0.18714 INSTANT 0.286011000E+00 TIME STEP NUMBER 297 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.38401E-05 0.28651E-02 Friction velocity uk : 0.38816E-05 0.28650E-02 Dimensionless distance yplus : 0.25850E-04 0.19061E-01 Friction thermal sca. tstar : -0.26042E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.18155E-04 0.13387E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.38401E-05 0.28651E-02 Friction velocity uk : 0.38816E-05 0.28650E-02 Dimensionless distance yplus : 0.25850E-04 0.19061E-01 Friction thermal sca. tstar : -0.26042E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.18155E-04 0.13387E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.38985E-08 4 0.47974E-06 0.18991E-11 0.23363E+01 c Velocity[X] 0.16101E-30 c Velocity[Y] 0.94953E-12 c Velocity[Z] 0.94952E-12 c Pressure 0.35907E-13 21 0.10086E-07 0.28291E-06 0.27775E+01 c k 0.78546E-06 2 0.13345E-06 0.43869E-07 0.28992E+01 c omega 0.13153E+02 1 0.66815E-08 0.40200E+01 0.10438E-01 c TempK 0.94406E+02 1 0.33422E-06 0.82171E-01 0.31861E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.5064e-13 1.2452e-13 -1.4882e-17 -3.7651e-18 v Velocity[Y] -0.00016877 0.00016697 -9.9289e-10 -5.4394e-12 v Velocity[Z] -0.00016698 0.00016878 9.0809e-10 -1.7297e-12 v ǁVelocityǁ 1.5842e-10 0.00019044 1.1428e-05 6.0718e-06 v Pressure -0.00049849 0.013872 0.00067979 4.1697e-20 v k 8.5058e-09 0.0026414 0.0018554 0.0022547 v omega 28.79 1.0313e+05 2676.5 512.28 v TempK 288 341.55 292.48 289.84 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.0019e-13 0.0001044 7.0721e-05 8.9335e-05 v CourantNb 1.1712e-09 0.00030415 1.6857e-05 8.4192e-06 v FourierNb 0.1427 0.6281 0.21943 0.18703 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9059 4.9059 0.00040098 -3.1961e-07 v volume_forces[Z] -4.9059 4.9059 -0.00040084 3.9339e-07 v ǁvolume_forcesǁ 5.7905e-09 4.9077 0.40749 0.16649 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.71 289.99 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.019061 6.5452e-05 3.7075e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14271 0.6281 0.21945 0.18704 INSTANT 0.286974000E+00 TIME STEP NUMBER 298 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.39147E-05 0.28624E-02 Friction velocity uk : 0.39550E-05 0.28622E-02 Dimensionless distance yplus : 0.26339E-04 0.19042E-01 Friction thermal sca. tstar : -0.27566E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.18499E-04 0.13374E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.39147E-05 0.28624E-02 Friction velocity uk : 0.39550E-05 0.28622E-02 Dimensionless distance yplus : 0.26339E-04 0.19042E-01 Friction thermal sca. tstar : -0.27566E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.18499E-04 0.13374E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.38919E-08 4 0.47740E-06 0.18758E-11 0.23259E+01 c Velocity[X] 0.15877E-30 c Velocity[Y] 0.93788E-12 c Velocity[Z] 0.93787E-12 c Pressure 0.35655E-13 21 0.10036E-07 0.28092E-06 0.27679E+01 c k 0.78336E-06 2 0.13273E-06 0.43427E-07 0.28924E+01 c omega 0.13153E+02 1 0.66452E-08 0.39834E+01 0.10390E-01 c TempK 0.94406E+02 1 0.33271E-06 0.81770E-01 0.31783E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.5035e-13 1.2427e-13 -1.4859e-17 -3.7594e-18 v Velocity[Y] -0.00016852 0.0001667 -9.9444e-10 -5.4223e-12 v Velocity[Z] -0.0001667 0.00016852 9.0915e-10 -1.7322e-12 v ǁVelocityǁ 1.5667e-10 0.00019005 1.1412e-05 6.066e-06 v Pressure -0.0005002 0.013895 0.0006814 3.0396e-20 v k 8.4379e-09 0.0026335 0.0018499 0.0022485 v omega 28.725 1.0313e+05 2676.5 512.22 v TempK 288 341.55 292.49 289.85 v Density 1.205 1.205 1.205 1.205 v TurbVisc 9.9384e-14 0.00010432 7.0673e-05 8.9287e-05 v CourantNb 1.1753e-09 0.00030355 1.6827e-05 8.4064e-06 v FourierNb 0.14259 0.6281 0.2193 0.18692 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9061 4.9061 0.00040142 -3.2048e-07 v volume_forces[Z] -4.9061 4.9061 -0.00040128 3.9439e-07 v ǁvolume_forcesǁ 5.7268e-09 4.9079 0.40793 0.16677 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.71 289.99 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.019042 6.5396e-05 3.7041e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14259 0.6281 0.21932 0.18693 INSTANT 0.287937000E+00 TIME STEP NUMBER 299 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.39882E-05 0.28596E-02 Friction velocity uk : 0.40273E-05 0.28594E-02 Dimensionless distance yplus : 0.26820E-04 0.19024E-01 Friction thermal sca. tstar : -0.29404E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.18837E-04 0.13361E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.39882E-05 0.28596E-02 Friction velocity uk : 0.40273E-05 0.28594E-02 Dimensionless distance yplus : 0.26820E-04 0.19024E-01 Friction thermal sca. tstar : -0.29404E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.18837E-04 0.13361E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.38853E-08 4 0.47514E-06 0.18527E-11 0.23155E+01 c Velocity[X] 0.15656E-30 c Velocity[Y] 0.92636E-12 c Velocity[Z] 0.92636E-12 c Pressure 0.35417E-13 21 0.99862E-08 0.27902E-06 0.27584E+01 c k 0.78126E-06 2 0.13202E-06 0.42991E-07 0.28857E+01 c omega 0.13153E+02 1 0.66092E-08 0.39473E+01 0.10343E-01 c TempK 0.94407E+02 1 0.33121E-06 0.81373E-01 0.31705E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.5006e-13 1.2402e-13 -1.4835e-17 -3.7538e-18 v Velocity[Y] -0.00016826 0.00016642 -9.9598e-10 -5.4055e-12 v Velocity[Z] -0.00016642 0.00016826 9.1018e-10 -1.7348e-12 v ǁVelocityǁ 1.5493e-10 0.00018966 1.1396e-05 6.0603e-06 v Pressure -0.00050192 0.013919 0.00068301 7.6726e-21 v k 8.3707e-09 0.0026257 0.0018444 0.0022422 v omega 28.66 1.0313e+05 2676.4 512.16 v TempK 288 341.55 292.49 289.85 v Density 1.205 1.205 1.205 1.205 v TurbVisc 9.8591e-14 0.00010425 7.0626e-05 8.9239e-05 v CourantNb 1.1795e-09 0.00030296 1.6798e-05 8.3937e-06 v FourierNb 0.14248 0.6281 0.21917 0.18682 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9063 4.9064 0.00040186 -3.2134e-07 v volume_forces[Z] -4.9063 4.9064 -0.00040172 3.9539e-07 v ǁvolume_forcesǁ 5.6636e-09 4.9081 0.40837 0.16706 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.72 289.99 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.019024 6.534e-05 3.7008e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14248 0.6281 0.21919 0.18683 INSTANT 0.288900000E+00 TIME STEP NUMBER 300 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.40607E-05 0.28568E-02 Friction velocity uk : 0.40987E-05 0.28567E-02 Dimensionless distance yplus : 0.27295E-04 0.19006E-01 Friction thermal sca. tstar : -0.31681E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.19170E-04 0.13348E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.40607E-05 0.28568E-02 Friction velocity uk : 0.40987E-05 0.28567E-02 Dimensionless distance yplus : 0.27295E-04 0.19006E-01 Friction thermal sca. tstar : -0.31681E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.19170E-04 0.13348E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.38788E-08 4 0.47280E-06 0.18299E-11 0.23051E+01 c Velocity[X] 0.15438E-30 c Velocity[Y] 0.91498E-12 c Velocity[Z] 0.91497E-12 c Pressure 0.35194E-13 21 0.99367E-08 0.27725E-06 0.27490E+01 c k 0.77918E-06 2 0.13131E-06 0.42559E-07 0.28790E+01 c omega 0.13153E+02 1 0.65735E-08 0.39116E+01 0.10296E-01 c TempK 0.94408E+02 1 0.32972E-06 0.80980E-01 0.31628E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.4977e-13 1.2377e-13 -1.4812e-17 -3.7482e-18 v Velocity[Y] -0.000168 0.00016615 -9.975e-10 -5.3887e-12 v Velocity[Z] -0.00016615 0.00016801 9.1121e-10 -1.7374e-12 v ǁVelocityǁ 1.5321e-10 0.00018928 1.138e-05 6.0547e-06 v Pressure -0.00050364 0.013943 0.00068462 -4.4786e-20 v k 8.3043e-09 0.0026178 0.001839 0.002236 v omega 28.595 1.0313e+05 2676.4 512.1 v TempK 288 341.55 292.5 289.85 v Density 1.205 1.205 1.205 1.205 v TurbVisc 9.7806e-14 0.00010417 7.0578e-05 8.9191e-05 v CourantNb 1.1836e-09 0.00030237 1.6769e-05 8.3812e-06 v FourierNb 0.14237 0.6281 0.21904 0.18671 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9065 4.9066 0.00040229 -3.222e-07 v volume_forces[Z] -4.9065 4.9066 -0.00040216 3.9638e-07 v ǁvolume_forcesǁ 5.6009e-09 4.9083 0.40881 0.16734 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.72 290 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.019006 6.5284e-05 3.6975e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14237 0.6281 0.21906 0.18672 INSTANT 0.289863000E+00 TIME STEP NUMBER 301 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.41260E-05 0.28541E-02 Friction velocity uk : 0.41629E-05 0.28539E-02 Dimensionless distance yplus : 0.27723E-04 0.18987E-01 Friction thermal sca. tstar : -0.34605E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.19471E-04 0.13335E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.41260E-05 0.28541E-02 Friction velocity uk : 0.41629E-05 0.28539E-02 Dimensionless distance yplus : 0.27723E-04 0.18987E-01 Friction thermal sca. tstar : -0.34605E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.19471E-04 0.13335E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.38723E-08 4 0.47047E-06 0.18074E-11 0.22947E+01 c Velocity[X] 0.15223E-30 c Velocity[Y] 0.90372E-12 c Velocity[Z] 0.90371E-12 c Pressure 0.34942E-13 21 0.98843E-08 0.27525E-06 0.27396E+01 c k 0.77711E-06 2 0.13061E-06 0.42133E-07 0.28724E+01 c omega 0.13153E+02 1 0.65380E-08 0.38762E+01 0.10250E-01 c TempK 0.94408E+02 1 0.32824E-06 0.80589E-01 0.31551E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.4948e-13 1.2352e-13 -1.4789e-17 -3.7427e-18 v Velocity[Y] -0.00016775 0.00016588 -9.9901e-10 -5.3717e-12 v Velocity[Z] -0.00016588 0.00016775 9.1222e-10 -1.74e-12 v ǁVelocityǁ 1.515e-10 0.0001889 1.1364e-05 6.0492e-06 v Pressure -0.00050535 0.013967 0.00068623 -4.2653e-21 v k 8.2385e-09 0.00261 0.0018335 0.0022298 v omega 28.531 1.0313e+05 2676.3 512.05 v TempK 288 341.56 292.5 289.85 v Density 1.205 1.205 1.205 1.205 v TurbVisc 9.7029e-14 0.0001041 7.053e-05 8.9143e-05 v CourantNb 1.1877e-09 0.00030179 1.6741e-05 8.3688e-06 v FourierNb 0.14226 0.6281 0.21891 0.18661 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9067 4.9068 0.00040273 -3.2306e-07 v volume_forces[Z] -4.9067 4.9068 -0.00040259 3.9738e-07 v ǁvolume_forcesǁ 5.5386e-09 4.9085 0.40925 0.16762 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.73 290 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.018987 6.5229e-05 3.6943e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14226 0.6281 0.21893 0.18662 INSTANT 0.290826000E+00 TIME STEP NUMBER 302 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.40507E-05 0.28513E-02 Friction velocity uk : 0.40878E-05 0.28512E-02 Dimensionless distance yplus : 0.27223E-04 0.18969E-01 Friction thermal sca. tstar : -0.38549E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.19120E-04 0.13323E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.40507E-05 0.28513E-02 Friction velocity uk : 0.40878E-05 0.28512E-02 Dimensionless distance yplus : 0.27223E-04 0.18969E-01 Friction thermal sca. tstar : -0.38549E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.19120E-04 0.13323E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.38659E-08 4 0.46824E-06 0.17852E-11 0.22843E+01 c Velocity[X] 0.15012E-30 c Velocity[Y] 0.89259E-12 c Velocity[Z] 0.89259E-12 c Pressure 0.34710E-13 21 0.98361E-08 0.27340E-06 0.27303E+01 c k 0.77504E-06 2 0.12992E-06 0.41713E-07 0.28657E+01 c omega 0.13153E+02 1 0.65029E-08 0.38413E+01 0.10203E-01 c TempK 0.94409E+02 1 0.32677E-06 0.80201E-01 0.31475E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.492e-13 1.2327e-13 -1.4766e-17 -3.7372e-18 v Velocity[Y] -0.0001675 0.00016561 -1.0005e-09 -5.3551e-12 v Velocity[Z] -0.00016561 0.0001675 9.1322e-10 -1.7426e-12 v ǁVelocityǁ 1.4981e-10 0.00018852 1.1348e-05 6.0438e-06 v Pressure -0.00050707 0.01399 0.00068784 -2.7798e-20 v k 8.1735e-09 0.0026023 0.0018281 0.0022237 v omega 28.466 1.0313e+05 2676.3 511.99 v TempK 288 341.56 292.51 289.86 v Density 1.205 1.205 1.205 1.205 v TurbVisc 9.6261e-14 0.00010403 7.0483e-05 8.9096e-05 v CourantNb 1.1918e-09 0.0003012 1.6712e-05 8.3565e-06 v FourierNb 0.14215 0.6281 0.21878 0.18651 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9069 4.907 0.00040316 -3.2392e-07 v volume_forces[Z] -4.9069 4.907 -0.00040303 3.9836e-07 v ǁvolume_forcesǁ 5.4769e-09 4.9087 0.40969 0.16791 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.73 290 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.018969 6.5173e-05 3.691e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14215 0.6281 0.2188 0.18652 INSTANT 0.291789000E+00 TIME STEP NUMBER 303 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.39736E-05 0.28486E-02 Friction velocity uk : 0.40110E-05 0.28485E-02 Dimensionless distance yplus : 0.26712E-04 0.18951E-01 Friction thermal sca. tstar : -0.44286E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.18761E-04 0.13310E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.39736E-05 0.28486E-02 Friction velocity uk : 0.40110E-05 0.28485E-02 Dimensionless distance yplus : 0.26712E-04 0.18951E-01 Friction thermal sca. tstar : -0.44286E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.18761E-04 0.13310E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.38596E-08 4 0.46599E-06 0.17632E-11 0.22740E+01 c Velocity[X] 0.14804E-30 c Velocity[Y] 0.88160E-12 c Velocity[Z] 0.88160E-12 c Pressure 0.34565E-13 21 0.97995E-08 0.27225E-06 0.27210E+01 c k 0.77299E-06 2 0.12924E-06 0.41297E-07 0.28591E+01 c omega 0.13153E+02 1 0.64679E-08 0.38067E+01 0.10157E-01 c TempK 0.94410E+02 1 0.32532E-06 0.79817E-01 0.31399E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.4891e-13 1.2303e-13 -1.4743e-17 -3.7317e-18 v Velocity[Y] -0.00016725 0.00016534 -1.002e-09 -5.3388e-12 v Velocity[Z] -0.00016534 0.00016725 9.142e-10 -1.7453e-12 v ǁVelocityǁ 1.4814e-10 0.00018814 1.1332e-05 6.0385e-06 v Pressure -0.00050878 0.014014 0.00068944 -3.9932e-20 v k 8.1091e-09 0.0025945 0.0018228 0.0022176 v omega 28.402 1.0313e+05 2676.2 511.93 v TempK 288 341.56 292.51 289.86 v Density 1.205 1.205 1.205 1.205 v TurbVisc 9.5501e-14 0.00010395 7.0436e-05 8.9048e-05 v CourantNb 1.1959e-09 0.00030063 1.6684e-05 8.3444e-06 v FourierNb 0.14204 0.6281 0.21865 0.1864 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9071 4.9072 0.0004036 -3.2477e-07 v volume_forces[Z] -4.9071 4.9072 -0.00040346 3.9935e-07 v ǁvolume_forcesǁ 5.4157e-09 4.9089 0.41012 0.16819 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.74 290.01 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.018951 6.5118e-05 3.6877e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14204 0.6281 0.21867 0.18641 INSTANT 0.292752000E+00 TIME STEP NUMBER 304 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.38947E-05 0.28459E-02 Friction velocity uk : 0.39324E-05 0.28458E-02 Dimensionless distance yplus : 0.26188E-04 0.18933E-01 Friction thermal sca. tstar : -0.53771E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.18393E-04 0.13297E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.38947E-05 0.28459E-02 Friction velocity uk : 0.39324E-05 0.28458E-02 Dimensionless distance yplus : 0.26188E-04 0.18933E-01 Friction thermal sca. tstar : -0.53771E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.18393E-04 0.13297E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.38533E-08 4 0.46376E-06 0.17415E-11 0.22636E+01 c Velocity[X] 0.14600E-30 c Velocity[Y] 0.87074E-12 c Velocity[Z] 0.87073E-12 c Pressure 0.34360E-13 21 0.97476E-08 0.27062E-06 0.27118E+01 c k 0.77095E-06 2 0.12856E-06 0.40887E-07 0.28526E+01 c omega 0.13153E+02 1 0.64333E-08 0.37725E+01 0.10112E-01 c TempK 0.94410E+02 1 0.32387E-06 0.79436E-01 0.31324E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.4863e-13 1.2278e-13 -1.472e-17 -3.7262e-18 v Velocity[Y] -0.000167 0.00016508 -1.0035e-09 -5.3221e-12 v Velocity[Z] -0.00016508 0.00016701 9.1517e-10 -1.7479e-12 v ǁVelocityǁ 1.4648e-10 0.00018777 1.1317e-05 6.0333e-06 v Pressure -0.0005105 0.014037 0.00069104 -2.9759e-20 v k 8.0454e-09 0.0025868 0.0018174 0.0022115 v omega 28.339 1.0313e+05 2676.2 511.87 v TempK 288 341.56 292.52 289.86 v Density 1.205 1.205 1.205 1.205 v TurbVisc 9.4749e-14 0.00010388 7.0389e-05 8.9001e-05 v CourantNb 1.2e-09 0.00030005 1.6656e-05 8.3324e-06 v FourierNb 0.14192 0.6281 0.21852 0.1863 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9073 4.9074 0.00040403 -3.2562e-07 v volume_forces[Z] -4.9073 4.9074 -0.00040389 4.0033e-07 v ǁvolume_forcesǁ 5.3552e-09 4.9091 0.41056 0.16847 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.74 290.01 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.018933 6.5064e-05 3.6845e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14193 0.6281 0.21854 0.18631 INSTANT 0.293715000E+00 TIME STEP NUMBER 305 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.38137E-05 0.28433E-02 Friction velocity uk : 0.38518E-05 0.28431E-02 Dimensionless distance yplus : 0.25651E-04 0.18915E-01 Friction thermal sca. tstar : -0.74343E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.18016E-04 0.13285E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.38137E-05 0.28433E-02 Friction velocity uk : 0.38518E-05 0.28431E-02 Dimensionless distance yplus : 0.25651E-04 0.18915E-01 Friction thermal sca. tstar : -0.74343E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.18016E-04 0.13285E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.38471E-08 4 0.46150E-06 0.17200E-11 0.22533E+01 c Velocity[X] 0.14399E-30 c Velocity[Y] 0.86000E-12 c Velocity[Z] 0.86000E-12 c Pressure 0.34048E-13 21 0.96875E-08 0.26815E-06 0.27027E+01 c k 0.76891E-06 2 0.12789E-06 0.40481E-07 0.28460E+01 c omega 0.13153E+02 1 0.63989E-08 0.37387E+01 0.10066E-01 c TempK 0.94411E+02 1 0.32244E-06 0.79057E-01 0.31249E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.4835e-13 1.2254e-13 -1.4698e-17 -3.7208e-18 v Velocity[Y] -0.00016676 0.00016481 -1.0049e-09 -5.305e-12 v Velocity[Z] -0.00016482 0.00016676 9.1612e-10 -1.7507e-12 v ǁVelocityǁ 1.4485e-10 0.0001874 1.1302e-05 6.0282e-06 v Pressure -0.00051221 0.014061 0.00069264 -4.3683e-20 v k 7.9824e-09 0.0025792 0.0018121 0.0022054 v omega 28.275 1.0313e+05 2676.1 511.81 v TempK 288 341.57 292.52 289.87 v Density 1.205 1.205 1.205 1.205 v TurbVisc 9.4005e-14 0.0001038 7.0342e-05 8.8953e-05 v CourantNb 1.2041e-09 0.00029948 1.6628e-05 8.3205e-06 v FourierNb 0.14181 0.6281 0.2184 0.1862 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9075 4.9076 0.00040446 -3.2647e-07 v volume_forces[Z] -4.9075 4.9076 -0.00040433 4.013e-07 v ǁvolume_forcesǁ 5.2954e-09 4.9093 0.41099 0.16875 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.75 290.01 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.018915 6.5009e-05 3.6812e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14182 0.6281 0.21841 0.18621 INSTANT 0.294678000E+00 TIME STEP NUMBER 306 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.37305E-05 0.28406E-02 Friction velocity uk : 0.37690E-05 0.28404E-02 Dimensionless distance yplus : 0.25100E-04 0.18898E-01 Friction thermal sca. tstar : -0.25765E+05 0.00000E+00 Dim-less thermal sca. tplus : 0.17629E-04 0.13272E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.37305E-05 0.28406E-02 Friction velocity uk : 0.37690E-05 0.28404E-02 Dimensionless distance yplus : 0.25100E-04 0.18898E-01 Friction thermal sca. tstar : -0.25765E+05 0.00000E+00 Dim-less thermal sca. tplus : 0.17629E-04 0.13272E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.38410E-08 4 0.45927E-06 0.16988E-11 0.22430E+01 c Velocity[X] 0.14201E-30 c Velocity[Y] 0.84940E-12 c Velocity[Z] 0.84940E-12 c Pressure 0.33787E-13 21 0.96412E-08 0.26608E-06 0.26936E+01 c k 0.76689E-06 2 0.12723E-06 0.40081E-07 0.28395E+01 c omega 0.13153E+02 1 0.63648E-08 0.37053E+01 0.10021E-01 c TempK 0.94412E+02 1 0.32101E-06 0.78682E-01 0.31174E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.4807e-13 1.223e-13 -1.4675e-17 -3.7155e-18 v Velocity[Y] -0.00016652 0.00016455 -1.0064e-09 -5.2886e-12 v Velocity[Z] -0.00016456 0.00016652 9.1706e-10 -1.7534e-12 v ǁVelocityǁ 1.4323e-10 0.00018703 1.1287e-05 6.0232e-06 v Pressure -0.00051393 0.014084 0.00069424 6.0302e-21 v k 7.9201e-09 0.0025716 0.0018069 0.0021994 v omega 28.212 1.0313e+05 2676.1 511.75 v TempK 288 341.57 292.53 289.87 v Density 1.205 1.205 1.205 1.205 v TurbVisc 9.3269e-14 0.00010373 7.0295e-05 8.8906e-05 v CourantNb 1.2082e-09 0.00029892 1.6601e-05 8.3088e-06 v FourierNb 0.1417 0.6281 0.21827 0.1861 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9077 4.9078 0.00040489 -3.2731e-07 v volume_forces[Z] -4.9077 4.9078 -0.00040476 4.0227e-07 v ǁvolume_forcesǁ 5.2361e-09 4.9095 0.41142 0.16903 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.75 290.02 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.018898 6.4953e-05 3.6779e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.1417 0.6281 0.21829 0.18611 INSTANT 0.295641000E+00 TIME STEP NUMBER 307 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.36452E-05 0.28379E-02 Friction velocity uk : 0.36841E-05 0.28378E-02 Dimensionless distance yplus : 0.24534E-04 0.18880E-01 Friction thermal sca. tstar : -0.11659E+05 0.00000E+00 Dim-less thermal sca. tplus : 0.17231E-04 0.13260E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.36452E-05 0.28379E-02 Friction velocity uk : 0.36841E-05 0.28378E-02 Dimensionless distance yplus : 0.24534E-04 0.18880E-01 Friction thermal sca. tstar : -0.11659E+05 0.00000E+00 Dim-less thermal sca. tplus : 0.17231E-04 0.13260E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.38350E-08 4 0.45708E-06 0.16779E-11 0.22326E+01 c Velocity[X] 0.14006E-30 c Velocity[Y] 0.83893E-12 c Velocity[Z] 0.83892E-12 c Pressure 0.33570E-13 21 0.95923E-08 0.26435E-06 0.26845E+01 c k 0.76488E-06 2 0.12657E-06 0.39685E-07 0.28330E+01 c omega 0.13153E+02 1 0.63309E-08 0.36723E+01 0.99764E-02 c TempK 0.94413E+02 1 0.31960E-06 0.78309E-01 0.31100E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.478e-13 1.2207e-13 -1.4653e-17 -3.7101e-18 v Velocity[Y] -0.00016627 0.00016429 -1.0078e-09 -5.2721e-12 v Velocity[Z] -0.0001643 0.00016628 9.1799e-10 -1.7559e-12 v ǁVelocityǁ 1.4164e-10 0.00018666 1.1272e-05 6.0183e-06 v Pressure -0.00051565 0.014108 0.00069583 -4.709e-20 v k 7.8584e-09 0.002564 0.0018016 0.0021934 v omega 28.15 1.0313e+05 2676 511.7 v TempK 288 341.57 292.53 289.87 v Density 1.205 1.205 1.205 1.205 v TurbVisc 9.2541e-14 0.00010367 7.0248e-05 8.8859e-05 v CourantNb 1.2123e-09 0.00029836 1.6574e-05 8.2972e-06 v FourierNb 0.14159 0.6281 0.21814 0.186 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9079 4.908 0.00040532 -3.2815e-07 v volume_forces[Z] -4.9079 4.908 -0.00040519 4.0324e-07 v ǁvolume_forcesǁ 5.1778e-09 4.9097 0.41186 0.16931 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.75 290.02 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.01888 6.4901e-05 3.6748e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14159 0.6281 0.21816 0.186 INSTANT 0.296604000E+00 TIME STEP NUMBER 308 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.35574E-05 0.28353E-02 Friction velocity uk : 0.35968E-05 0.28351E-02 Dimensionless distance yplus : 0.23953E-04 0.18862E-01 Friction thermal sca. tstar : -0.64345E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.16823E-04 0.13248E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.35574E-05 0.28353E-02 Friction velocity uk : 0.35968E-05 0.28351E-02 Dimensionless distance yplus : 0.23953E-04 0.18862E-01 Friction thermal sca. tstar : -0.64345E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.16823E-04 0.13248E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.38290E-08 4 0.45489E-06 0.16572E-11 0.22224E+01 c Velocity[X] 0.13814E-30 c Velocity[Y] 0.82858E-12 c Velocity[Z] 0.82858E-12 c Pressure 0.33341E-13 21 0.95458E-08 0.26254E-06 0.26756E+01 c k 0.76287E-06 2 0.12592E-06 0.39294E-07 0.28266E+01 c omega 0.13153E+02 1 0.62973E-08 0.36396E+01 0.99319E-02 c TempK 0.94413E+02 1 0.31820E-06 0.77940E-01 0.31026E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.4752e-13 1.2183e-13 -1.4631e-17 -3.7048e-18 v Velocity[Y] -0.00016603 0.00016404 -1.0092e-09 -5.2557e-12 v Velocity[Z] -0.00016404 0.00016604 9.1891e-10 -1.7586e-12 v ǁVelocityǁ 1.4007e-10 0.0001863 1.1257e-05 6.0134e-06 v Pressure -0.00051736 0.014131 0.00069742 1.0688e-20 v k 7.7974e-09 0.0025564 0.0017964 0.0021875 v omega 28.087 1.0313e+05 2676 511.64 v TempK 288 341.57 292.54 289.88 v Density 1.205 1.205 1.205 1.205 v TurbVisc 9.182e-14 0.00010361 7.0202e-05 8.8812e-05 v CourantNb 1.2164e-09 0.0002978 1.6547e-05 8.2857e-06 v FourierNb 0.14148 0.6281 0.21802 0.1859 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9081 4.9082 0.00040575 -3.2899e-07 v volume_forces[Z] -4.9081 4.9082 -0.00040561 4.0421e-07 v ǁvolume_forcesǁ 5.1202e-09 4.9099 0.41229 0.16959 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.76 290.02 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.018862 6.4849e-05 3.6717e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14148 0.6281 0.21803 0.1859 INSTANT 0.297567000E+00 TIME STEP NUMBER 309 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.34669E-05 0.28327E-02 Friction velocity uk : 0.35069E-05 0.28325E-02 Dimensionless distance yplus : 0.23354E-04 0.18845E-01 Friction thermal sca. tstar : -0.12386E+05 0.00000E+00 Dim-less thermal sca. tplus : 0.16403E-04 0.13235E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.34669E-05 0.28327E-02 Friction velocity uk : 0.35069E-05 0.28325E-02 Dimensionless distance yplus : 0.23354E-04 0.18845E-01 Friction thermal sca. tstar : -0.12386E+05 0.00000E+00 Dim-less thermal sca. tplus : 0.16403E-04 0.13235E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.38230E-08 4 0.45271E-06 0.16367E-11 0.22121E+01 c Velocity[X] 0.13625E-30 c Velocity[Y] 0.81837E-12 c Velocity[Z] 0.81837E-12 c Pressure 0.33118E-13 21 0.95002E-08 0.26077E-06 0.26667E+01 c k 0.76088E-06 2 0.12528E-06 0.38908E-07 0.28202E+01 c omega 0.13153E+02 1 0.62639E-08 0.36073E+01 0.98877E-02 c TempK 0.94414E+02 1 0.31680E-06 0.77573E-01 0.30952E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.4725e-13 1.216e-13 -1.4609e-17 -3.6995e-18 v Velocity[Y] -0.0001658 0.00016378 -1.0106e-09 -5.2394e-12 v Velocity[Z] -0.00016378 0.0001658 9.1981e-10 -1.7615e-12 v ǁVelocityǁ 1.3852e-10 0.00018593 1.1242e-05 6.0087e-06 v Pressure -0.00051908 0.014155 0.00069901 -3.8437e-20 v k 7.737e-09 0.0025489 0.0017912 0.0021815 v omega 28.025 1.0313e+05 2675.9 511.58 v TempK 288 341.57 292.54 289.88 v Density 1.205 1.205 1.205 1.205 v TurbVisc 9.1107e-14 0.00010355 7.0156e-05 8.8766e-05 v CourantNb 1.2205e-09 0.00029724 1.652e-05 8.2744e-06 v FourierNb 0.14137 0.6281 0.21789 0.18579 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9083 4.9084 0.00040618 -3.2982e-07 v volume_forces[Z] -4.9083 4.9084 -0.00040604 4.0517e-07 v ǁvolume_forcesǁ 5.0634e-09 4.9101 0.41272 0.16987 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.76 290.02 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.018845 6.4796e-05 3.6686e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14137 0.6281 0.21791 0.1858 INSTANT 0.298530000E+00 TIME STEP NUMBER 310 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.33737E-05 0.28301E-02 Friction velocity uk : 0.34142E-05 0.28299E-02 Dimensionless distance yplus : 0.22737E-04 0.18828E-01 Friction thermal sca. tstar : -0.82808E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.15969E-04 0.13223E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.33737E-05 0.28301E-02 Friction velocity uk : 0.34142E-05 0.28299E-02 Dimensionless distance yplus : 0.22737E-04 0.18828E-01 Friction thermal sca. tstar : -0.82808E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.15969E-04 0.13223E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.38172E-08 4 0.45057E-06 0.16166E-11 0.22018E+01 c Velocity[X] 0.13440E-30 c Velocity[Y] 0.80828E-12 c Velocity[Z] 0.80828E-12 c Pressure 0.32902E-13 21 0.94537E-08 0.25905E-06 0.26578E+01 c k 0.75889E-06 2 0.12464E-06 0.38527E-07 0.28138E+01 c omega 0.13153E+02 1 0.62308E-08 0.35753E+01 0.98437E-02 c TempK 0.94415E+02 1 0.31542E-06 0.77209E-01 0.30879E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.4698e-13 1.2136e-13 -1.4587e-17 -3.6943e-18 v Velocity[Y] -0.00016556 0.00016353 -1.012e-09 -5.223e-12 v Velocity[Z] -0.00016353 0.00016556 9.2069e-10 -1.7643e-12 v ǁVelocityǁ 1.37e-10 0.00018558 1.1228e-05 6.0041e-06 v Pressure -0.00052079 0.014178 0.0007006 -1.6473e-20 v k 7.6772e-09 0.0025415 0.001786 0.0021756 v omega 27.963 1.0313e+05 2675.9 511.53 v TempK 288 341.58 292.55 289.88 v Density 1.205 1.205 1.205 1.205 v TurbVisc 9.0401e-14 0.0001035 7.011e-05 8.8719e-05 v CourantNb 1.2246e-09 0.00029669 1.6493e-05 8.2632e-06 v FourierNb 0.14126 0.6281 0.21777 0.18569 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9085 4.9085 0.0004066 -3.3066e-07 v volume_forces[Z] -4.9085 4.9085 -0.00040647 4.0613e-07 v ǁvolume_forcesǁ 5.0075e-09 4.9103 0.41314 0.17015 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.77 290.03 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.018828 6.4746e-05 3.6656e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14126 0.6281 0.21778 0.1857 INSTANT 0.299493000E+00 TIME STEP NUMBER 311 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.32773E-05 0.28275E-02 Friction velocity uk : 0.33186E-05 0.28273E-02 Dimensionless distance yplus : 0.22100E-04 0.18810E-01 Friction thermal sca. tstar : -0.52507E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.15522E-04 0.13211E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.32773E-05 0.28275E-02 Friction velocity uk : 0.33186E-05 0.28273E-02 Dimensionless distance yplus : 0.22100E-04 0.18810E-01 Friction thermal sca. tstar : -0.52507E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.15522E-04 0.13211E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.38114E-08 4 0.46723E-06 0.15967E-11 0.21916E+01 c Velocity[X] 0.13257E-30 c Velocity[Y] 0.79833E-12 c Velocity[Z] 0.79833E-12 c Pressure 0.32681E-13 21 0.94080E-08 0.25730E-06 0.26490E+01 c k 0.75692E-06 2 0.12401E-06 0.38150E-07 0.28074E+01 c omega 0.13153E+02 1 0.61979E-08 0.35437E+01 0.98001E-02 c TempK 0.94415E+02 1 0.31405E-06 0.76848E-01 0.30807E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.4671e-13 1.2113e-13 -1.4565e-17 -3.689e-18 v Velocity[Y] -0.00016532 0.00016327 -1.0134e-09 -5.2069e-12 v Velocity[Z] -0.00016328 0.00016533 9.2157e-10 -1.7669e-12 v ǁVelocityǁ 1.3551e-10 0.00018522 1.1214e-05 5.9996e-06 v Pressure -0.00052251 0.014201 0.00070218 3.2701e-20 v k 7.6181e-09 0.002534 0.0017809 0.0021697 v omega 27.901 1.0313e+05 2675.8 511.47 v TempK 288 341.58 292.55 289.89 v Density 1.205 1.205 1.205 1.205 v TurbVisc 8.9703e-14 0.00010344 7.0064e-05 8.8673e-05 v CourantNb 1.2287e-09 0.00029615 1.6467e-05 8.2521e-06 v FourierNb 0.14115 0.6281 0.21764 0.18559 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9087 4.9087 0.00040703 -3.3148e-07 v volume_forces[Z] -4.9087 4.9087 -0.00040689 4.0708e-07 v ǁvolume_forcesǁ 4.9526e-09 4.9105 0.41357 0.17043 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.77 290.03 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.01881 6.4697e-05 3.6627e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14115 0.6281 0.21766 0.1856 INSTANT 0.300456000E+00 TIME STEP NUMBER 312 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.31776E-05 0.28249E-02 Friction velocity uk : 0.32197E-05 0.28247E-02 Dimensionless distance yplus : 0.21442E-04 0.18793E-01 Friction thermal sca. tstar : -0.41526E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.15059E-04 0.13199E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.31776E-05 0.28249E-02 Friction velocity uk : 0.32197E-05 0.28247E-02 Dimensionless distance yplus : 0.21442E-04 0.18793E-01 Friction thermal sca. tstar : -0.41526E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.15059E-04 0.13199E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.38056E-08 4 0.44630E-06 0.15770E-11 0.21814E+01 c Velocity[X] 0.13077E-30 c Velocity[Y] 0.78850E-12 c Velocity[Z] 0.78850E-12 c Pressure 0.32464E-13 21 0.93607E-08 0.25558E-06 0.26403E+01 c k 0.75495E-06 2 0.12338E-06 0.37778E-07 0.28011E+01 c omega 0.13153E+02 1 0.61653E-08 0.35124E+01 0.97568E-02 c TempK 0.94416E+02 1 0.31269E-06 0.76490E-01 0.30735E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.4644e-13 1.209e-13 -1.4544e-17 -3.6839e-18 v Velocity[Y] -0.00016509 0.00016302 -1.0148e-09 -5.1908e-12 v Velocity[Z] -0.00016303 0.00016509 9.2243e-10 -1.7697e-12 v ǁVelocityǁ 1.3405e-10 0.00018486 1.1199e-05 5.9951e-06 v Pressure -0.00052422 0.014225 0.00070377 1.5223e-20 v k 7.5595e-09 0.0025266 0.0017758 0.0021639 v omega 27.84 1.0313e+05 2675.8 511.41 v TempK 288 341.58 292.56 289.89 v Density 1.205 1.205 1.205 1.205 v TurbVisc 8.9012e-14 0.00010338 7.0018e-05 8.8626e-05 v CourantNb 1.2329e-09 0.0002956 1.6441e-05 8.2412e-06 v FourierNb 0.14104 0.6281 0.21752 0.18549 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9089 4.9089 0.00040745 -3.3231e-07 v volume_forces[Z] -4.9089 4.9089 -0.00040732 4.0803e-07 v ǁvolume_forcesǁ 4.8988e-09 4.9107 0.414 0.1707 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.78 290.03 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.018793 6.4648e-05 3.6598e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14104 0.6281 0.21753 0.1855 INSTANT 0.301419000E+00 TIME STEP NUMBER 313 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.30742E-05 0.28223E-02 Friction velocity uk : 0.31172E-05 0.28222E-02 Dimensionless distance yplus : 0.20759E-04 0.18776E-01 Friction thermal sca. tstar : -0.35413E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.14580E-04 0.13187E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.30742E-05 0.28223E-02 Friction velocity uk : 0.31172E-05 0.28222E-02 Dimensionless distance yplus : 0.20759E-04 0.18776E-01 Friction thermal sca. tstar : -0.35413E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.14580E-04 0.13187E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.37999E-08 4 0.44419E-06 0.15576E-11 0.21713E+01 c Velocity[X] 0.12900E-30 c Velocity[Y] 0.77880E-12 c Velocity[Z] 0.77880E-12 c Pressure 0.32252E-13 21 0.93154E-08 0.25389E-06 0.26316E+01 c k 0.75299E-06 2 0.12276E-06 0.37410E-07 0.27948E+01 c omega 0.13153E+02 1 0.61329E-08 0.34814E+01 0.97137E-02 c TempK 0.94417E+02 1 0.31133E-06 0.76135E-01 0.30663E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.4617e-13 1.2068e-13 -1.4522e-17 -3.6787e-18 v Velocity[Y] -0.00016486 0.00016277 -1.0161e-09 -5.1747e-12 v Velocity[Z] -0.00016278 0.00016486 9.2327e-10 -1.7725e-12 v ǁVelocityǁ 1.3262e-10 0.00018451 1.1186e-05 5.9908e-06 v Pressure -0.00052594 0.014248 0.00070535 -7.0598e-21 v k 7.5016e-09 0.0025193 0.0017707 0.0021581 v omega 27.779 1.0313e+05 2675.7 511.36 v TempK 288 341.58 292.56 289.89 v Density 1.205 1.205 1.205 1.205 v TurbVisc 8.8328e-14 0.00010332 6.9972e-05 8.858e-05 v CourantNb 1.237e-09 0.00029506 1.6416e-05 8.2304e-06 v FourierNb 0.14093 0.6281 0.21739 0.18539 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9091 4.9091 0.00040788 -3.3313e-07 v volume_forces[Z] -4.9091 4.9091 -0.00040774 4.0898e-07 v ǁvolume_forcesǁ 4.8459e-09 4.9109 0.41442 0.17098 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.78 290.04 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.018776 6.4599e-05 3.6569e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14093 0.6281 0.21741 0.1854 INSTANT 0.302382000E+00 TIME STEP NUMBER 314 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.29668E-05 0.28198E-02 Friction velocity uk : 0.30108E-05 0.28196E-02 Dimensionless distance yplus : 0.20051E-04 0.18759E-01 Friction thermal sca. tstar : -0.37378E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.14082E-04 0.13175E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.29668E-05 0.28198E-02 Friction velocity uk : 0.30108E-05 0.28196E-02 Dimensionless distance yplus : 0.20051E-04 0.18759E-01 Friction thermal sca. tstar : -0.37378E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.14082E-04 0.13175E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.37943E-08 4 0.44210E-06 0.15385E-11 0.21612E+01 c Velocity[X] 0.12726E-30 c Velocity[Y] 0.76923E-12 c Velocity[Z] 0.76923E-12 c Pressure 0.32042E-13 21 0.92698E-08 0.25223E-06 0.26230E+01 c k 0.75105E-06 2 0.12215E-06 0.37046E-07 0.27885E+01 c omega 0.13153E+02 1 0.61008E-08 0.34508E+01 0.96709E-02 c TempK 0.94417E+02 1 0.30999E-06 0.75782E-01 0.30591E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.4591e-13 1.2045e-13 -1.4501e-17 -3.6736e-18 v Velocity[Y] -0.00016463 0.00016253 -1.0175e-09 -5.1586e-12 v Velocity[Z] -0.00016253 0.00016463 9.2411e-10 -1.7753e-12 v ǁVelocityǁ 1.3123e-10 0.00018416 1.1172e-05 5.9865e-06 v Pressure -0.00052765 0.014271 0.00070693 -1.461e-20 v k 7.4442e-09 0.0025119 0.0017656 0.0021523 v omega 27.718 1.0313e+05 2675.7 511.3 v TempK 288 341.58 292.57 289.9 v Density 1.205 1.205 1.205 1.205 v TurbVisc 8.7651e-14 0.00010326 6.9926e-05 8.8534e-05 v CourantNb 1.2411e-09 0.00029453 1.639e-05 8.2197e-06 v FourierNb 0.14082 0.6281 0.21727 0.1853 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9093 4.9093 0.0004083 -3.3395e-07 v volume_forces[Z] -4.9093 4.9093 -0.00040816 4.0992e-07 v ǁvolume_forcesǁ 4.7943e-09 4.911 0.41485 0.17126 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.79 290.04 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.018759 6.455e-05 3.654e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14082 0.6281 0.21729 0.1853 INSTANT 0.303345000E+00 TIME STEP NUMBER 315 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.28549E-05 0.28173E-02 Friction velocity uk : 0.29000E-05 0.28171E-02 Dimensionless distance yplus : 0.19313E-04 0.18742E-01 Friction thermal sca. tstar : -0.43505E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.13564E-04 0.13163E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.28549E-05 0.28173E-02 Friction velocity uk : 0.29000E-05 0.28171E-02 Dimensionless distance yplus : 0.19313E-04 0.18742E-01 Friction thermal sca. tstar : -0.43505E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.13564E-04 0.13163E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.37888E-08 4 0.44001E-06 0.15196E-11 0.21511E+01 c Velocity[X] 0.12555E-30 c Velocity[Y] 0.75978E-12 c Velocity[Z] 0.75978E-12 c Pressure 0.31832E-13 21 0.92260E-08 0.25056E-06 0.26144E+01 c k 0.74911E-06 2 0.12154E-06 0.36687E-07 0.27823E+01 c omega 0.13153E+02 1 0.60689E-08 0.34206E+01 0.96284E-02 c TempK 0.94418E+02 1 0.30866E-06 0.75432E-01 0.30520E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.4565e-13 1.2023e-13 -1.4479e-17 -3.6685e-18 v Velocity[Y] -0.0001644 0.00016228 -1.0188e-09 -5.1427e-12 v Velocity[Z] -0.00016228 0.0001644 9.2493e-10 -1.7781e-12 v ǁVelocityǁ 1.2986e-10 0.00018381 1.1158e-05 5.9824e-06 v Pressure -0.00052937 0.014294 0.0007085 -5.1576e-20 v k 7.3875e-09 0.0025046 0.0017606 0.0021465 v omega 27.657 1.0313e+05 2675.7 511.25 v TempK 288 341.59 292.57 289.9 v Density 1.205 1.205 1.205 1.205 v TurbVisc 8.6981e-14 0.00010321 6.9881e-05 8.8488e-05 v CourantNb 1.2452e-09 0.00029399 1.6365e-05 8.2092e-06 v FourierNb 0.14071 0.6281 0.21715 0.1852 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9095 4.9095 0.00040872 -3.3477e-07 v volume_forces[Z] -4.9095 4.9095 -0.00040858 4.1086e-07 v ǁvolume_forcesǁ 4.7438e-09 4.9112 0.41527 0.17153 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.79 290.04 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.018742 6.4501e-05 3.6511e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14072 0.6281 0.21717 0.18521 INSTANT 0.304308000E+00 TIME STEP NUMBER 316 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.27379E-05 0.28147E-02 Friction velocity uk : 0.27844E-05 0.28146E-02 Dimensionless distance yplus : 0.18543E-04 0.18726E-01 Friction thermal sca. tstar : -0.54171E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.13023E-04 0.13152E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.27379E-05 0.28147E-02 Friction velocity uk : 0.27844E-05 0.28146E-02 Dimensionless distance yplus : 0.18543E-04 0.18726E-01 Friction thermal sca. tstar : -0.54171E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.13023E-04 0.13152E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.37833E-08 4 0.43796E-06 0.15009E-11 0.21410E+01 c Velocity[X] 0.12386E-30 c Velocity[Y] 0.75045E-12 c Velocity[Z] 0.75045E-12 c Pressure 0.31632E-13 21 0.91824E-08 0.24898E-06 0.26059E+01 c k 0.74718E-06 2 0.12094E-06 0.36333E-07 0.27760E+01 c omega 0.13153E+02 1 0.60372E-08 0.33906E+01 0.95862E-02 c TempK 0.94419E+02 1 0.30734E-06 0.75085E-01 0.30450E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.4539e-13 1.2001e-13 -1.4458e-17 -3.6634e-18 v Velocity[Y] -0.00016417 0.00016204 -1.0201e-09 -5.1269e-12 v Velocity[Z] -0.00016204 0.00016418 9.2573e-10 -1.7811e-12 v ǁVelocityǁ 1.2854e-10 0.00018347 1.1145e-05 5.9783e-06 v Pressure -0.00053108 0.014317 0.00071007 2.3263e-20 v k 7.3313e-09 0.0024974 0.0017556 0.0021408 v omega 27.597 1.0313e+05 2675.6 511.19 v TempK 288 341.59 292.58 289.9 v Density 1.205 1.205 1.205 1.205 v TurbVisc 8.6318e-14 0.00010315 6.9836e-05 8.8442e-05 v CourantNb 1.2493e-09 0.00029346 1.634e-05 8.1988e-06 v FourierNb 0.1406 0.6281 0.21703 0.1851 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9097 4.9097 0.00040914 -3.3558e-07 v volume_forces[Z] -4.9097 4.9097 -0.000409 4.118e-07 v ǁvolume_forcesǁ 4.6946e-09 4.9114 0.41569 0.17181 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.8 290.05 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.018726 6.4452e-05 3.6481e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14061 0.6281 0.21704 0.18511 INSTANT 0.305271000E+00 TIME STEP NUMBER 317 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.26152E-05 0.28122E-02 Friction velocity uk : 0.26633E-05 0.28121E-02 Dimensionless distance yplus : 0.17736E-04 0.18709E-01 Friction thermal sca. tstar : -0.80839E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.12457E-04 0.13140E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.26152E-05 0.28122E-02 Friction velocity uk : 0.26633E-05 0.28121E-02 Dimensionless distance yplus : 0.17736E-04 0.18709E-01 Friction thermal sca. tstar : -0.80839E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.12457E-04 0.13140E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.37779E-08 4 0.43597E-06 0.14825E-11 0.21310E+01 c Velocity[X] 0.12220E-30 c Velocity[Y] 0.74126E-12 c Velocity[Z] 0.74126E-12 c Pressure 0.31530E-13 21 0.91522E-08 0.24816E-06 0.25974E+01 c k 0.74526E-06 2 0.12035E-06 0.35982E-07 0.27699E+01 c omega 0.13153E+02 1 0.60057E-08 0.33610E+01 0.95442E-02 c TempK 0.94420E+02 1 0.30602E-06 0.74740E-01 0.30379E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.4513e-13 1.1979e-13 -1.4437e-17 -3.6584e-18 v Velocity[Y] -0.00016395 0.0001618 -1.0214e-09 -5.1116e-12 v Velocity[Z] -0.0001618 0.00016395 9.2653e-10 -1.7836e-12 v ǁVelocityǁ 1.2725e-10 0.00018313 1.1131e-05 5.9743e-06 v Pressure -0.00053279 0.01434 0.00071165 -3.1622e-21 v k 7.2757e-09 0.0024901 0.0017506 0.0021351 v omega 27.537 1.0313e+05 2675.6 511.14 v TempK 288 341.59 292.58 289.9 v Density 1.205 1.205 1.205 1.205 v TurbVisc 8.5661e-14 0.00010309 6.979e-05 8.8396e-05 v CourantNb 1.2534e-09 0.00029294 1.6315e-05 8.1885e-06 v FourierNb 0.1405 0.6281 0.21691 0.185 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9098 4.9099 0.00040956 -3.3639e-07 v volume_forces[Z] -4.9098 4.9099 -0.00040942 4.1274e-07 v ǁvolume_forcesǁ 4.6467e-09 4.9116 0.41612 0.17208 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.8 290.05 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.018709 6.4402e-05 3.6452e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.1405 0.6281 0.21692 0.18501 INSTANT 0.306234000E+00 TIME STEP NUMBER 318 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.24859E-05 0.28097E-02 Friction velocity uk : 0.25359E-05 0.28096E-02 Dimensionless distance yplus : 0.16888E-04 0.18692E-01 Friction thermal sca. tstar : -0.17232E+05 0.00000E+00 Dim-less thermal sca. tplus : 0.11861E-04 0.13128E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.24859E-05 0.28097E-02 Friction velocity uk : 0.25359E-05 0.28096E-02 Dimensionless distance yplus : 0.16888E-04 0.18692E-01 Friction thermal sca. tstar : -0.17232E+05 0.00000E+00 Dim-less thermal sca. tplus : 0.11861E-04 0.13128E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.37725E-08 4 0.43396E-06 0.14644E-11 0.21210E+01 c Velocity[X] 0.12057E-30 c Velocity[Y] 0.73219E-12 c Velocity[Z] 0.73219E-12 c Pressure 0.31355E-13 21 0.91100E-08 0.24677E-06 0.25890E+01 c k 0.74335E-06 2 0.11976E-06 0.35636E-07 0.27637E+01 c omega 0.13153E+02 1 0.59745E-08 0.33317E+01 0.95025E-02 c TempK 0.94420E+02 1 0.30472E-06 0.74398E-01 0.30309E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.4487e-13 1.1957e-13 -1.4416e-17 -3.6533e-18 v Velocity[Y] -0.00016373 0.00016156 -1.0227e-09 -5.0958e-12 v Velocity[Z] -0.00016156 0.00016373 9.2731e-10 -1.7866e-12 v ǁVelocityǁ 1.2601e-10 0.00018279 1.1118e-05 5.9705e-06 v Pressure -0.00053451 0.014363 0.00071322 -2.1008e-20 v k 7.2207e-09 0.0024829 0.0017456 0.0021294 v omega 27.477 1.0313e+05 2675.5 511.08 v TempK 288 341.59 292.58 289.91 v Density 1.205 1.205 1.205 1.205 v TurbVisc 8.5012e-14 0.00010303 6.9745e-05 8.835e-05 v CourantNb 1.2575e-09 0.00029242 1.629e-05 8.1784e-06 v FourierNb 0.14039 0.6281 0.21679 0.1849 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.91 4.9101 0.00040998 -3.372e-07 v volume_forces[Z] -4.91 4.9101 -0.00040984 4.1367e-07 v ǁvolume_forcesǁ 4.6002e-09 4.9118 0.41654 0.17236 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.81 290.05 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.018692 6.4353e-05 3.6423e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14039 0.6281 0.2168 0.18491 INSTANT 0.307197000E+00 TIME STEP NUMBER 319 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.23490E-05 0.28073E-02 Friction velocity uk : 0.24011E-05 0.28071E-02 Dimensionless distance yplus : 0.15990E-04 0.18676E-01 Friction thermal sca. tstar : -0.67102E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.11231E-04 0.13117E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.23490E-05 0.28073E-02 Friction velocity uk : 0.24011E-05 0.28071E-02 Dimensionless distance yplus : 0.15990E-04 0.18676E-01 Friction thermal sca. tstar : -0.67102E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.11231E-04 0.13117E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.37672E-08 4 0.43209E-06 0.14465E-11 0.21111E+01 c Velocity[X] 0.11896E-30 c Velocity[Y] 0.72324E-12 c Velocity[Z] 0.72324E-12 c Pressure 0.31046E-13 20 0.92430E-08 0.24432E-06 0.25806E+01 c k 0.74144E-06 2 0.11918E-06 0.35293E-07 0.27576E+01 c omega 0.13153E+02 1 0.59435E-08 0.33027E+01 0.94611E-02 c TempK 0.94421E+02 1 0.30342E-06 0.74058E-01 0.30240E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.4461e-13 1.1935e-13 -1.4395e-17 -3.6484e-18 v Velocity[Y] -0.0001635 0.00016132 -1.0242e-09 -5.2767e-12 v Velocity[Z] -0.00016132 0.00016351 9.2815e-10 -1.7245e-12 v ǁVelocityǁ 1.2507e-10 0.00018245 1.1105e-05 5.9667e-06 v Pressure -0.00053622 0.014386 0.00071478 -9.364e-21 v k 7.1662e-09 0.0024758 0.0017407 0.0021237 v omega 27.418 1.0313e+05 2675.5 511.03 v TempK 288 341.59 292.59 289.91 v Density 1.205 1.205 1.205 1.205 v TurbVisc 8.4369e-14 0.00010297 6.9701e-05 8.8305e-05 v CourantNb 1.2616e-09 0.0002919 1.6266e-05 8.1683e-06 v FourierNb 0.14028 0.6281 0.21667 0.18481 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9102 4.9103 0.0004104 -3.3801e-07 v volume_forces[Z] -4.9102 4.9103 -0.00041026 4.1459e-07 v ǁvolume_forcesǁ 4.5552e-09 4.912 0.41696 0.17263 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.81 290.06 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.018676 6.4308e-05 3.6396e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14028 0.6281 0.21668 0.18481 INSTANT 0.308160000E+00 TIME STEP NUMBER 320 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.22119E-05 0.28048E-02 Friction velocity uk : 0.22666E-05 0.28046E-02 Dimensionless distance yplus : 0.15094E-04 0.18659E-01 Friction thermal sca. tstar : -0.49347E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.10601E-04 0.13105E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.22119E-05 0.28048E-02 Friction velocity uk : 0.22666E-05 0.28046E-02 Dimensionless distance yplus : 0.15094E-04 0.18659E-01 Friction thermal sca. tstar : -0.49347E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.10601E-04 0.13105E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.37619E-08 4 0.43007E-06 0.14288E-11 0.21011E+01 c Velocity[X] 0.11739E-30 c Velocity[Y] 0.71441E-12 c Velocity[Z] 0.71441E-12 c Pressure 0.30837E-13 20 0.92009E-08 0.24267E-06 0.25723E+01 c k 0.73955E-06 2 0.11860E-06 0.34955E-07 0.27515E+01 c omega 0.13153E+02 1 0.59128E-08 0.32741E+01 0.94200E-02 c TempK 0.94422E+02 1 0.30213E-06 0.73721E-01 0.30171E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.4436e-13 1.1913e-13 -1.4375e-17 -3.6434e-18 v Velocity[Y] -0.00016328 0.00016108 -1.0254e-09 -5.261e-12 v Velocity[Z] -0.00016108 0.00016329 9.289e-10 -1.727e-12 v ǁVelocityǁ 1.2386e-10 0.00018211 1.1092e-05 5.963e-06 v Pressure -0.00053794 0.014409 0.00071635 -4.8266e-20 v k 7.1123e-09 0.0024686 0.0017358 0.0021181 v omega 27.358 1.0313e+05 2675.4 510.97 v TempK 288 341.6 292.59 289.91 v Density 1.205 1.205 1.205 1.205 v TurbVisc 8.3732e-14 0.00010292 6.9656e-05 8.8259e-05 v CourantNb 1.2658e-09 0.00029138 1.6242e-05 8.1584e-06 v FourierNb 0.14017 0.6281 0.21655 0.18471 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9104 4.9105 0.00041081 -3.3881e-07 v volume_forces[Z] -4.9104 4.9105 -0.00041067 4.1552e-07 v ǁvolume_forcesǁ 4.5212e-09 4.9122 0.41737 0.17291 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.82 290.06 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.018659 6.4262e-05 3.6369e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14017 0.6281 0.21656 0.18472 INSTANT 0.309123000E+00 TIME STEP NUMBER 321 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.20585E-05 0.28023E-02 Friction velocity uk : 0.21164E-05 0.28022E-02 Dimensionless distance yplus : 0.14094E-04 0.18643E-01 Friction thermal sca. tstar : -0.40846E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.98989E-05 0.13094E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.20585E-05 0.28023E-02 Friction velocity uk : 0.21164E-05 0.28022E-02 Dimensionless distance yplus : 0.14094E-04 0.18643E-01 Friction thermal sca. tstar : -0.40846E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.98989E-05 0.13094E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.37567E-08 4 0.42804E-06 0.14114E-11 0.20913E+01 c Velocity[X] 0.11583E-30 c Velocity[Y] 0.70571E-12 c Velocity[Z] 0.70571E-12 c Pressure 0.30637E-13 20 0.91573E-08 0.24108E-06 0.25641E+01 c k 0.73767E-06 2 0.11803E-06 0.34621E-07 0.27454E+01 c omega 0.13153E+02 1 0.58823E-08 0.32457E+01 0.93791E-02 c TempK 0.94422E+02 1 0.30086E-06 0.73387E-01 0.30102E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.4411e-13 1.1892e-13 -1.4354e-17 -3.6385e-18 v Velocity[Y] -0.00016307 0.00016085 -1.0267e-09 -5.244e-12 v Velocity[Z] -0.00016085 0.00016307 9.2964e-10 -1.7306e-12 v ǁVelocityǁ 1.2272e-10 0.00018178 1.108e-05 5.9594e-06 v Pressure -0.00053965 0.014432 0.00071791 -4.3486e-20 v k 7.059e-09 0.0024615 0.0017309 0.0021125 v omega 27.299 1.0313e+05 2675.4 510.92 v TempK 288 341.6 292.6 289.92 v Density 1.205 1.205 1.205 1.205 v TurbVisc 8.3103e-14 0.00010286 6.9611e-05 8.8214e-05 v CourantNb 1.2699e-09 0.00029087 1.6218e-05 8.1487e-06 v FourierNb 0.14006 0.6281 0.21643 0.18461 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9106 4.9106 0.00041123 -3.3961e-07 v volume_forces[Z] -4.9106 4.9106 -0.00041109 4.1644e-07 v ǁvolume_forcesǁ 4.4775e-09 4.9123 0.41779 0.17318 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.82 290.06 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.018643 6.4216e-05 3.6341e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.14006 0.6281 0.21644 0.18462 INSTANT 0.310086000E+00 TIME STEP NUMBER 322 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.18904E-05 0.27999E-02 Friction velocity uk : 0.19525E-05 0.27998E-02 Dimensionless distance yplus : 0.13003E-04 0.18627E-01 Friction thermal sca. tstar : -0.35620E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.91321E-05 0.13082E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.18904E-05 0.27999E-02 Friction velocity uk : 0.19525E-05 0.27998E-02 Dimensionless distance yplus : 0.13003E-04 0.18627E-01 Friction thermal sca. tstar : -0.35620E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.91321E-05 0.13082E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.37516E-08 4 0.42604E-06 0.13942E-11 0.20815E+01 c Velocity[X] 0.11430E-30 c Velocity[Y] 0.69712E-12 c Velocity[Z] 0.69713E-12 c Pressure 0.30445E-13 20 0.91140E-08 0.23956E-06 0.25558E+01 c k 0.73579E-06 2 0.11746E-06 0.34291E-07 0.27393E+01 c omega 0.13153E+02 1 0.58519E-08 0.32176E+01 0.93384E-02 c TempK 0.94423E+02 1 0.29959E-06 0.73055E-01 0.30033E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.4386e-13 1.1871e-13 -1.4334e-17 -3.6336e-18 v Velocity[Y] -0.00016285 0.00016061 -1.0279e-09 -5.2276e-12 v Velocity[Z] -0.00016061 0.00016285 9.3036e-10 -1.7337e-12 v ǁVelocityǁ 1.2164e-10 0.00018145 1.1067e-05 5.9558e-06 v Pressure -0.00054137 0.014455 0.00071947 -3.0543e-20 v k 7.0061e-09 0.0024544 0.001726 0.0021069 v omega 27.241 1.0313e+05 2675.3 510.86 v TempK 288 341.6 292.6 289.92 v Density 1.205 1.205 1.205 1.205 v TurbVisc 8.2479e-14 0.0001028 6.9567e-05 8.8169e-05 v CourantNb 1.274e-09 0.00029036 1.6194e-05 8.139e-06 v FourierNb 0.13995 0.6281 0.21631 0.18452 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9108 4.9108 0.00041164 -3.4041e-07 v volume_forces[Z] -4.9108 4.9108 -0.0004115 4.1736e-07 v ǁvolume_forcesǁ 4.4363e-09 4.9125 0.41821 0.17346 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.82 290.06 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.018627 6.4171e-05 3.6314e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.13995 0.6281 0.21632 0.18452 INSTANT 0.311049000E+00 TIME STEP NUMBER 323 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.17042E-05 0.27975E-02 Friction velocity uk : 0.17719E-05 0.27973E-02 Dimensionless distance yplus : 0.11800E-04 0.18611E-01 Friction thermal sca. tstar : -0.31996E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.82874E-05 0.13071E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.17042E-05 0.27975E-02 Friction velocity uk : 0.17719E-05 0.27973E-02 Dimensionless distance yplus : 0.11800E-04 0.18611E-01 Friction thermal sca. tstar : -0.31996E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.82874E-05 0.13071E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.37465E-08 4 0.42407E-06 0.13773E-11 0.20717E+01 c Velocity[X] 0.11279E-30 c Velocity[Y] 0.68866E-12 c Velocity[Z] 0.68866E-12 c Pressure 0.30252E-13 20 0.90728E-08 0.23803E-06 0.25477E+01 c k 0.73392E-06 2 0.11690E-06 0.33964E-07 0.27333E+01 c omega 0.13153E+02 1 0.58219E-08 0.31899E+01 0.92981E-02 c TempK 0.94424E+02 1 0.29833E-06 0.72726E-01 0.29965E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.4361e-13 1.185e-13 -1.4313e-17 -3.6287e-18 v Velocity[Y] -0.00016263 0.00016038 -1.0291e-09 -5.2112e-12 v Velocity[Z] -0.00016038 0.00016264 9.3108e-10 -1.737e-12 v ǁVelocityǁ 1.2061e-10 0.00018112 1.1055e-05 5.9524e-06 v Pressure -0.00054308 0.014478 0.00072103 -2.971e-20 v k 6.9538e-09 0.0024474 0.0017212 0.0021014 v omega 27.182 1.0313e+05 2675.3 510.81 v TempK 288 341.6 292.61 289.92 v Density 1.205 1.205 1.205 1.205 v TurbVisc 8.1862e-14 0.00010274 6.9522e-05 8.8124e-05 v CourantNb 1.2781e-09 0.00028986 1.6171e-05 8.1295e-06 v FourierNb 0.13984 0.6281 0.21619 0.18442 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.911 4.911 0.00041206 -3.412e-07 v volume_forces[Z] -4.911 4.911 -0.00041192 4.1827e-07 v ǁvolume_forcesǁ 4.3971e-09 4.9127 0.41862 0.17373 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.83 290.07 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.018611 6.4125e-05 3.6287e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.13985 0.6281 0.21621 0.18443 INSTANT 0.312012000E+00 TIME STEP NUMBER 324 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.14937E-05 0.27951E-02 Friction velocity uk : 0.15693E-05 0.27949E-02 Dimensionless distance yplus : 0.10451E-04 0.18595E-01 Friction thermal sca. tstar : -0.29290E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.73399E-05 0.13060E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.14937E-05 0.27951E-02 Friction velocity uk : 0.15693E-05 0.27949E-02 Dimensionless distance yplus : 0.10451E-04 0.18595E-01 Friction thermal sca. tstar : -0.29290E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.73399E-05 0.13060E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.37415E-08 4 0.42211E-06 0.13606E-11 0.20620E+01 c Velocity[X] 0.11131E-30 c Velocity[Y] 0.68032E-12 c Velocity[Z] 0.68032E-12 c Pressure 0.30059E-13 20 0.90294E-08 0.23650E-06 0.25396E+01 c k 0.73207E-06 2 0.11634E-06 0.33641E-07 0.27273E+01 c omega 0.13153E+02 1 0.57920E-08 0.31624E+01 0.92579E-02 c TempK 0.94424E+02 1 0.29708E-06 0.72399E-01 0.29897E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.4336e-13 1.1829e-13 -1.4293e-17 -3.6239e-18 v Velocity[Y] -0.00016242 0.00016015 -1.0303e-09 -5.1949e-12 v Velocity[Z] -0.00016015 0.00016242 9.3178e-10 -1.7401e-12 v ǁVelocityǁ 1.1964e-10 0.00018079 1.1042e-05 5.9491e-06 v Pressure -0.00054479 0.014501 0.00072259 -9.8617e-20 v k 6.9021e-09 0.0024404 0.0017164 0.0020958 v omega 27.124 1.0313e+05 2675.3 510.76 v TempK 288 341.6 292.61 289.93 v Density 1.205 1.205 1.205 1.205 v TurbVisc 8.1251e-14 0.00010268 6.9478e-05 8.8079e-05 v CourantNb 1.2823e-09 0.00028936 1.6148e-05 8.1201e-06 v FourierNb 0.13974 0.6281 0.21607 0.18432 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9111 4.9112 0.00041247 -3.4199e-07 v volume_forces[Z] -4.9111 4.9112 -0.00041233 4.1918e-07 v ǁvolume_forcesǁ 4.36e-09 4.9129 0.41904 0.174 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.83 290.07 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.018595 6.4079e-05 3.626e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.13974 0.6281 0.21609 0.18433 INSTANT 0.312975000E+00 TIME STEP NUMBER 325 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12471E-05 0.27927E-02 Friction velocity uk : 0.13350E-05 0.27925E-02 Dimensionless distance yplus : 0.88904E-05 0.18579E-01 Friction thermal sca. tstar : -0.27170E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.62441E-05 0.13049E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12471E-05 0.27927E-02 Friction velocity uk : 0.13350E-05 0.27925E-02 Dimensionless distance yplus : 0.88904E-05 0.18579E-01 Friction thermal sca. tstar : -0.27170E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.62441E-05 0.13049E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.37366E-08 4 0.42565E-06 0.13442E-11 0.20523E+01 c Velocity[X] 0.10985E-30 c Velocity[Y] 0.67209E-12 c Velocity[Z] 0.67209E-12 c Pressure 0.29867E-13 20 0.89872E-08 0.23497E-06 0.25315E+01 c k 0.73022E-06 2 0.11579E-06 0.33323E-07 0.27214E+01 c omega 0.13153E+02 1 0.57623E-08 0.31352E+01 0.92181E-02 c TempK 0.94425E+02 1 0.29584E-06 0.72074E-01 0.29830E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.4312e-13 1.1808e-13 -1.4273e-17 -3.619e-18 v Velocity[Y] -0.00016221 0.00015992 -1.0315e-09 -5.1786e-12 v Velocity[Z] -0.00015992 0.00016221 9.3246e-10 -1.7433e-12 v ǁVelocityǁ 1.1872e-10 0.00018047 1.103e-05 5.9458e-06 v Pressure -0.00054651 0.014523 0.00072414 -5.4468e-20 v k 6.8508e-09 0.0024334 0.0017116 0.0020903 v omega 27.066 1.0313e+05 2675.2 510.7 v TempK 288 341.61 292.62 289.93 v Density 1.205 1.205 1.205 1.205 v TurbVisc 8.0646e-14 0.00010263 6.9434e-05 8.8034e-05 v CourantNb 1.2864e-09 0.00028886 1.6125e-05 8.1108e-06 v FourierNb 0.13963 0.6281 0.21595 0.18423 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9113 4.9114 0.00041288 -3.4278e-07 v volume_forces[Z] -4.9113 4.9114 -0.00041274 4.2009e-07 v ǁvolume_forcesǁ 4.3249e-09 4.9131 0.41945 0.17427 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.84 290.07 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.018579 6.4034e-05 3.6233e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.13963 0.6281 0.21597 0.18424 INSTANT 0.313938000E+00 TIME STEP NUMBER 326 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.93745E-06 0.27903E-02 Friction velocity uk : 0.10482E-05 0.27901E-02 Dimensionless distance yplus : 0.69804E-05 0.18563E-01 Friction thermal sca. tstar : -0.25452E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.49026E-05 0.13037E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.93745E-06 0.27903E-02 Friction velocity uk : 0.10482E-05 0.27901E-02 Dimensionless distance yplus : 0.69804E-05 0.18563E-01 Friction thermal sca. tstar : -0.25452E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.49026E-05 0.13037E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.37317E-08 4 0.41824E-06 0.13280E-11 0.20427E+01 c Velocity[X] 0.10842E-30 c Velocity[Y] 0.66398E-12 c Velocity[Z] 0.66398E-12 c Pressure 0.29680E-13 20 0.89473E-08 0.23350E-06 0.25235E+01 c k 0.72837E-06 2 0.11524E-06 0.33007E-07 0.27154E+01 c omega 0.13153E+02 1 0.57329E-08 0.31084E+01 0.91785E-02 c TempK 0.94426E+02 1 0.29461E-06 0.71752E-01 0.29763E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.4287e-13 1.1787e-13 -1.4253e-17 -3.6142e-18 v Velocity[Y] -0.000162 0.00015969 -1.0327e-09 -5.1624e-12 v Velocity[Z] -0.0001597 0.000162 9.3314e-10 -1.7464e-12 v ǁVelocityǁ 1.1786e-10 0.00018014 1.1018e-05 5.9426e-06 v Pressure -0.00054822 0.014546 0.00072569 1.6179e-21 v k 6.8001e-09 0.0024265 0.0017068 0.0020849 v omega 27.008 1.0313e+05 2675.2 510.65 v TempK 288 341.61 292.62 289.93 v Density 1.205 1.205 1.205 1.205 v TurbVisc 8.0047e-14 0.00010257 6.939e-05 8.7989e-05 v CourantNb 1.2905e-09 0.00028836 1.6102e-05 8.1017e-06 v FourierNb 0.13952 0.6281 0.21584 0.18413 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9115 4.9116 0.00041329 -3.4357e-07 v volume_forces[Z] -4.9115 4.9116 -0.00041315 4.21e-07 v ǁvolume_forcesǁ 4.2918e-09 4.9132 0.41986 0.17454 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.84 290.08 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.018563 6.3989e-05 3.6206e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.13952 0.6281 0.21585 0.18414 INSTANT 0.314901000E+00 TIME STEP NUMBER 327 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.46328E-06 0.27879E-02 Friction velocity uk : 0.64211E-06 0.27878E-02 Dimensionless distance yplus : 0.42762E-05 0.18547E-01 Friction thermal sca. tstar : -0.24022E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.30033E-05 0.13026E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.46328E-06 0.27879E-02 Friction velocity uk : 0.64211E-06 0.27878E-02 Dimensionless distance yplus : 0.42762E-05 0.18547E-01 Friction thermal sca. tstar : -0.24022E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.30033E-05 0.13026E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.37268E-08 4 0.41633E-06 0.13120E-11 0.20331E+01 c Velocity[X] 0.10701E-30 c Velocity[Y] 0.65599E-12 c Velocity[Z] 0.65599E-12 c Pressure 0.29493E-13 20 0.89053E-08 0.23201E-06 0.25156E+01 c k 0.72654E-06 2 0.11470E-06 0.32696E-07 0.27095E+01 c omega 0.13153E+02 1 0.57036E-08 0.30818E+01 0.91391E-02 c TempK 0.94426E+02 1 0.29338E-06 0.71432E-01 0.29696E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.4263e-13 1.1767e-13 -1.4233e-17 -3.6095e-18 v Velocity[Y] -0.00016179 0.00015947 -1.0339e-09 -5.1463e-12 v Velocity[Z] -0.00015947 0.00016179 9.338e-10 -1.7496e-12 v ǁVelocityǁ 1.1707e-10 0.00017982 1.1007e-05 5.9396e-06 v Pressure -0.00054993 0.014569 0.00072724 -4.5447e-20 v k 6.7498e-09 0.0024196 0.0017021 0.0020794 v omega 26.95 1.0313e+05 2675.1 510.6 v TempK 288 341.61 292.63 289.94 v Density 1.205 1.205 1.205 1.205 v TurbVisc 7.9454e-14 0.00010251 6.9346e-05 8.7944e-05 v CourantNb 1.2946e-09 0.00028787 1.6079e-05 8.0926e-06 v FourierNb 0.13941 0.6281 0.21572 0.18404 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9117 4.9117 0.0004137 -3.4435e-07 v volume_forces[Z] -4.9117 4.9117 -0.00041356 4.219e-07 v ǁvolume_forcesǁ 4.2608e-09 4.9134 0.42027 0.17482 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.85 290.08 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.018547 6.3944e-05 3.6179e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.13941 0.6281 0.21574 0.18405 INSTANT 0.315864000E+00 TIME STEP NUMBER 328 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.55007E-06 0.27856E-02 Friction velocity uk : 0.71002E-06 0.27854E-02 Dimensionless distance yplus : 0.47284E-05 0.18532E-01 Friction thermal sca. tstar : -0.22808E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.33209E-05 0.13015E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.55007E-06 0.27856E-02 Friction velocity uk : 0.71002E-06 0.27854E-02 Dimensionless distance yplus : 0.47284E-05 0.18532E-01 Friction thermal sca. tstar : -0.22808E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.33209E-05 0.13015E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.37220E-08 4 0.41554E-06 0.12962E-11 0.20236E+01 c Velocity[X] 0.10562E-30 c Velocity[Y] 0.64811E-12 c Velocity[Z] 0.64811E-12 c Pressure 0.29310E-13 20 0.88643E-08 0.23056E-06 0.25076E+01 c k 0.72472E-06 2 0.11417E-06 0.32388E-07 0.27036E+01 c omega 0.13153E+02 1 0.56746E-08 0.30554E+01 0.91000E-02 c TempK 0.94427E+02 1 0.29217E-06 0.71115E-01 0.29630E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.4239e-13 1.1746e-13 -1.4213e-17 -3.6047e-18 v Velocity[Y] -0.00016158 0.00015924 -1.0351e-09 -5.1302e-12 v Velocity[Z] -0.00015925 0.00016158 9.3445e-10 -1.7527e-12 v ǁVelocityǁ 1.1633e-10 0.0001795 1.0995e-05 5.9366e-06 v Pressure -0.00055165 0.014591 0.00072879 4.6894e-20 v k 6.7001e-09 0.0024127 0.0016974 0.002074 v omega 26.893 1.0313e+05 2675.1 510.55 v TempK 288 341.61 292.63 289.94 v Density 1.205 1.205 1.205 1.205 v TurbVisc 7.8867e-14 0.00010245 6.9303e-05 8.79e-05 v CourantNb 1.2987e-09 0.00028738 1.6057e-05 8.0837e-06 v FourierNb 0.1393 0.6281 0.21561 0.18394 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9119 4.9119 0.00041411 -3.4513e-07 v volume_forces[Z] -4.9119 4.9119 -0.00041397 4.2279e-07 v ǁvolume_forcesǁ 4.232e-09 4.9136 0.42068 0.17509 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.85 290.08 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.018532 6.3899e-05 3.6152e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.13931 0.6281 0.21562 0.18395 INSTANT 0.316827000E+00 TIME STEP NUMBER 329 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.98974E-06 0.27832E-02 Friction velocity uk : 0.10925E-05 0.27831E-02 Dimensionless distance yplus : 0.72757E-05 0.18516E-01 Friction thermal sca. tstar : -0.21760E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.51100E-05 0.13004E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.98974E-06 0.27832E-02 Friction velocity uk : 0.10925E-05 0.27831E-02 Dimensionless distance yplus : 0.72757E-05 0.18516E-01 Friction thermal sca. tstar : -0.21760E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.51100E-05 0.13004E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.37173E-08 4 0.41257E-06 0.12807E-11 0.20141E+01 c Velocity[X] 0.10425E-30 c Velocity[Y] 0.64035E-12 c Velocity[Z] 0.64035E-12 c Pressure 0.29129E-13 20 0.88240E-08 0.22912E-06 0.24998E+01 c k 0.72290E-06 2 0.11364E-06 0.32084E-07 0.26978E+01 c omega 0.13153E+02 1 0.56458E-08 0.30294E+01 0.90612E-02 c TempK 0.94428E+02 1 0.29096E-06 0.70800E-01 0.29564E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.4215e-13 1.1726e-13 -1.4194e-17 -3.6e-18 v Velocity[Y] -0.00016137 0.00015902 -1.0362e-09 -5.1142e-12 v Velocity[Z] -0.00015902 0.00016138 9.3508e-10 -1.7559e-12 v ǁVelocityǁ 1.1566e-10 0.00017919 1.0983e-05 5.9337e-06 v Pressure -0.00055336 0.014614 0.00073033 6.3955e-20 v k 6.6508e-09 0.0024058 0.0016927 0.0020686 v omega 26.836 1.0313e+05 2675 510.49 v TempK 288 341.61 292.64 289.94 v Density 1.205 1.205 1.205 1.205 v TurbVisc 7.8286e-14 0.0001024 6.9259e-05 8.7855e-05 v CourantNb 1.3028e-09 0.0002869 1.6035e-05 8.0749e-06 v FourierNb 0.1392 0.6281 0.21549 0.18385 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.912 4.9121 0.00041452 -3.4591e-07 v volume_forces[Z] -4.912 4.9121 -0.00041438 4.2369e-07 v ǁvolume_forcesǁ 4.2054e-09 4.9138 0.42109 0.17536 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.86 290.09 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.018516 6.3855e-05 3.6126e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.1392 0.6281 0.21551 0.18386 INSTANT 0.317790000E+00 TIME STEP NUMBER 330 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12924E-05 0.27809E-02 Friction velocity uk : 0.13732E-05 0.27807E-02 Dimensionless distance yplus : 0.91451E-05 0.18500E-01 Friction thermal sca. tstar : -0.20845E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.64230E-05 0.12994E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12924E-05 0.27809E-02 Friction velocity uk : 0.13732E-05 0.27807E-02 Dimensionless distance yplus : 0.91451E-05 0.18500E-01 Friction thermal sca. tstar : -0.20845E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.64230E-05 0.12994E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.37126E-08 3 0.41289E-06 0.12654E-11 0.20046E+01 c Velocity[X] 0.10295E-30 c Velocity[Y] 0.63269E-12 c Velocity[Z] 0.63269E-12 c Pressure 0.29350E-13 20 0.84782E-08 0.23085E-06 0.24920E+01 c k 0.72109E-06 2 0.11311E-06 0.31783E-07 0.26919E+01 c omega 0.13153E+02 1 0.56172E-08 0.30036E+01 0.90225E-02 c TempK 0.94429E+02 1 0.28976E-06 0.70487E-01 0.29498E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.4191e-13 1.1706e-13 -1.4174e-17 -3.5953e-18 v Velocity[Y] -0.00016117 0.0001588 -1.0374e-09 -5.0958e-12 v Velocity[Z] -0.0001588 0.00016117 9.357e-10 -1.7633e-12 v ǁVelocityǁ 1.1506e-10 0.00017887 1.0972e-05 5.9309e-06 v Pressure -0.00055507 0.014637 0.00073188 -3.677e-20 v k 6.6021e-09 0.002399 0.001688 0.0020633 v omega 26.779 1.0313e+05 2675 510.44 v TempK 288 341.62 292.64 289.94 v Density 1.205 1.205 1.205 1.205 v TurbVisc 7.771e-14 0.00010234 6.9216e-05 8.7811e-05 v CourantNb 1.3069e-09 0.00028642 1.6013e-05 8.0663e-06 v FourierNb 0.13909 0.6281 0.21538 0.18375 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9122 4.9123 0.00041492 -3.4669e-07 v volume_forces[Z] -4.9122 4.9123 -0.00041478 4.2458e-07 v ǁvolume_forcesǁ 4.1811e-09 4.914 0.4215 0.17563 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.86 290.09 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.0185 6.381e-05 3.61e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.13909 0.6281 0.21539 0.18376 INSTANT 0.318753000E+00 TIME STEP NUMBER 331 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15405E-05 0.27786E-02 Friction velocity uk : 0.16087E-05 0.27784E-02 Dimensionless distance yplus : 0.10713E-04 0.18485E-01 Friction thermal sca. tstar : -0.20035E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.75245E-05 0.12983E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15405E-05 0.27786E-02 Friction velocity uk : 0.16087E-05 0.27784E-02 Dimensionless distance yplus : 0.10713E-04 0.18485E-01 Friction thermal sca. tstar : -0.20035E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.75245E-05 0.12983E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.37080E-08 3 0.41103E-06 0.12503E-11 0.19953E+01 c Velocity[X] 0.10159E-30 c Velocity[Y] 0.62515E-12 c Velocity[Z] 0.62515E-12 c Pressure 0.29161E-13 20 0.84371E-08 0.22935E-06 0.24842E+01 c k 0.71930E-06 2 0.11259E-06 0.31486E-07 0.26861E+01 c omega 0.13153E+02 1 0.55888E-08 0.29781E+01 0.89842E-02 c TempK 0.94429E+02 1 0.28857E-06 0.70176E-01 0.29433E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.4167e-13 1.1686e-13 -1.4155e-17 -3.5906e-18 v Velocity[Y] -0.00016097 0.00015858 -1.0385e-09 -5.08e-12 v Velocity[Z] -0.00015858 0.00016097 9.3631e-10 -1.7664e-12 v ǁVelocityǁ 1.1452e-10 0.00017856 1.0961e-05 5.9281e-06 v Pressure -0.00055679 0.014659 0.00073342 -4.1525e-20 v k 6.5538e-09 0.0023922 0.0016834 0.0020579 v omega 26.723 1.0313e+05 2674.9 510.39 v TempK 288 341.62 292.64 289.95 v Density 1.205 1.205 1.205 1.205 v TurbVisc 7.7141e-14 0.00010228 6.9173e-05 8.7767e-05 v CourantNb 1.311e-09 0.00028594 1.5991e-05 8.0577e-06 v FourierNb 0.13898 0.6281 0.21526 0.18366 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9124 4.9124 0.00041533 -3.4746e-07 v volume_forces[Z] -4.9124 4.9124 -0.00041519 4.2547e-07 v ǁvolume_forcesǁ 4.1593e-09 4.9141 0.42191 0.1759 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.87 290.09 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.018485 6.3766e-05 3.6073e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.13898 0.6281 0.21528 0.18367 INSTANT 0.319716000E+00 TIME STEP NUMBER 332 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.17530E-05 0.27763E-02 Friction velocity uk : 0.18129E-05 0.27761E-02 Dimensionless distance yplus : 0.12073E-04 0.18470E-01 Friction thermal sca. tstar : -0.19313E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.84793E-05 0.12972E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.17530E-05 0.27763E-02 Friction velocity uk : 0.18129E-05 0.27761E-02 Dimensionless distance yplus : 0.12073E-04 0.18470E-01 Friction thermal sca. tstar : -0.19313E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.84793E-05 0.12972E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.37035E-08 3 0.40919E-06 0.12355E-11 0.19860E+01 c Velocity[X] 0.10027E-30 c Velocity[Y] 0.61773E-12 c Velocity[Z] 0.61773E-12 c Pressure 0.28982E-13 20 0.83974E-08 0.22793E-06 0.24765E+01 c k 0.71750E-06 2 0.11207E-06 0.31192E-07 0.26803E+01 c omega 0.13153E+02 1 0.55606E-08 0.29529E+01 0.89460E-02 c TempK 0.94430E+02 1 0.28739E-06 0.69868E-01 0.29368E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.4144e-13 1.1666e-13 -1.4135e-17 -3.586e-18 v Velocity[Y] -0.00016076 0.00015836 -1.0396e-09 -5.0642e-12 v Velocity[Z] -0.00015836 0.00016077 9.3691e-10 -1.7695e-12 v ǁVelocityǁ 1.1405e-10 0.00017825 1.095e-05 5.9255e-06 v Pressure -0.0005585 0.014682 0.00073496 -4.0643e-20 v k 6.506e-09 0.0023855 0.0016787 0.0020526 v omega 26.666 1.0313e+05 2674.9 510.34 v TempK 288 341.62 292.65 289.95 v Density 1.205 1.205 1.205 1.205 v TurbVisc 7.6576e-14 0.00010222 6.9129e-05 8.7723e-05 v CourantNb 1.3151e-09 0.00028547 1.597e-05 8.0493e-06 v FourierNb 0.13888 0.6281 0.21515 0.18357 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9126 4.9126 0.00041573 -3.4823e-07 v volume_forces[Z] -4.9126 4.9126 -0.00041559 4.2635e-07 v ǁvolume_forcesǁ 4.1398e-09 4.9143 0.42232 0.17617 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.87 290.1 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.01847 6.3723e-05 3.6047e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.13888 0.6281 0.21516 0.18358 INSTANT 0.320679000E+00 TIME STEP NUMBER 333 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19430E-05 0.27740E-02 Friction velocity uk : 0.19968E-05 0.27738E-02 Dimensionless distance yplus : 0.13298E-04 0.18454E-01 Friction thermal sca. tstar : -0.18663E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.93394E-05 0.12961E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19430E-05 0.27740E-02 Friction velocity uk : 0.19968E-05 0.27738E-02 Dimensionless distance yplus : 0.13298E-04 0.18454E-01 Friction thermal sca. tstar : -0.18663E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.93394E-05 0.12961E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.36990E-08 3 0.40740E-06 0.12208E-11 0.19767E+01 c Velocity[X] 0.98989E-31 c Velocity[Y] 0.61041E-12 c Velocity[Z] 0.61042E-12 c Pressure 0.28809E-13 20 0.83576E-08 0.22656E-06 0.24688E+01 c k 0.71572E-06 2 0.11156E-06 0.30901E-07 0.26746E+01 c omega 0.13153E+02 1 0.55326E-08 0.29279E+01 0.89081E-02 c TempK 0.94431E+02 1 0.28621E-06 0.69562E-01 0.29303E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.412e-13 1.1647e-13 -1.4116e-17 -3.5813e-18 v Velocity[Y] -0.00016056 0.00015815 -1.0407e-09 -5.0485e-12 v Velocity[Z] -0.00015815 0.00016057 9.3749e-10 -1.7727e-12 v ǁVelocityǁ 1.1365e-10 0.00017794 1.0939e-05 5.9229e-06 v Pressure -0.00056021 0.014704 0.00073649 3.373e-20 v k 6.4587e-09 0.0023787 0.0016741 0.0020473 v omega 26.61 1.0313e+05 2674.9 510.29 v TempK 288 341.62 292.65 289.95 v Density 1.205 1.205 1.205 1.205 v TurbVisc 7.6018e-14 0.00010216 6.9086e-05 8.7679e-05 v CourantNb 1.3192e-09 0.00028499 1.5949e-05 8.041e-06 v FourierNb 0.13877 0.6281 0.21503 0.18347 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9128 4.9128 0.00041614 -3.49e-07 v volume_forces[Z] -4.9128 4.9128 -0.000416 4.2724e-07 v ǁvolume_forcesǁ 4.1228e-09 4.9145 0.42272 0.17644 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.87 290.1 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.018454 6.3679e-05 3.6021e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.13877 0.6281 0.21505 0.18348 INSTANT 0.321642000E+00 TIME STEP NUMBER 334 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.20513E-05 0.27717E-02 Friction velocity uk : 0.21019E-05 0.27715E-02 Dimensionless distance yplus : 0.13996E-04 0.18439E-01 Friction thermal sca. tstar : -0.18074E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.98301E-05 0.12951E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.20513E-05 0.27717E-02 Friction velocity uk : 0.21019E-05 0.27715E-02 Dimensionless distance yplus : 0.13996E-04 0.18439E-01 Friction thermal sca. tstar : -0.18074E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.98301E-05 0.12951E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.36945E-08 3 0.40559E-06 0.12064E-11 0.19675E+01 c Velocity[X] 0.97731E-31 c Velocity[Y] 0.60321E-12 c Velocity[Z] 0.60321E-12 c Pressure 0.28636E-13 20 0.83180E-08 0.22519E-06 0.24612E+01 c k 0.71395E-06 2 0.11105E-06 0.30614E-07 0.26688E+01 c omega 0.13153E+02 1 0.55048E-08 0.29032E+01 0.88705E-02 c TempK 0.94431E+02 1 0.28505E-06 0.69258E-01 0.29239E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.4097e-13 1.1627e-13 -1.4097e-17 -3.5768e-18 v Velocity[Y] -0.00016036 0.00015793 -1.0418e-09 -5.0329e-12 v Velocity[Z] -0.00015793 0.00016037 9.3807e-10 -1.7758e-12 v ǁVelocityǁ 1.1332e-10 0.00017764 1.0928e-05 5.9204e-06 v Pressure -0.00056192 0.014726 0.00073803 -1.0933e-20 v k 6.4118e-09 0.002372 0.0016696 0.002042 v omega 26.554 1.0313e+05 2674.8 510.24 v TempK 288 341.62 292.66 289.96 v Density 1.205 1.205 1.205 1.205 v TurbVisc 7.5465e-14 0.00010211 6.9044e-05 8.7635e-05 v CourantNb 1.3233e-09 0.00028453 1.5928e-05 8.0328e-06 v FourierNb 0.13866 0.6281 0.21492 0.18338 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9129 4.913 0.00041654 -3.4976e-07 v volume_forces[Z] -4.9129 4.913 -0.0004164 4.2811e-07 v ǁvolume_forcesǁ 4.1083e-09 4.9146 0.42313 0.1767 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.88 290.1 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.018439 6.3635e-05 3.5995e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.13866 0.6281 0.21494 0.18339 INSTANT 0.322605000E+00 TIME STEP NUMBER 335 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19418E-05 0.27694E-02 Friction velocity uk : 0.19945E-05 0.27693E-02 Dimensionless distance yplus : 0.13281E-04 0.18424E-01 Friction thermal sca. tstar : -0.17537E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.93280E-05 0.12940E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19418E-05 0.27694E-02 Friction velocity uk : 0.19945E-05 0.27693E-02 Dimensionless distance yplus : 0.13281E-04 0.18424E-01 Friction thermal sca. tstar : -0.17537E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.93280E-05 0.12940E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.36901E-08 3 0.40383E-06 0.11922E-11 0.19584E+01 c Velocity[X] 0.96493E-31 c Velocity[Y] 0.59612E-12 c Velocity[Z] 0.59612E-12 c Pressure 0.28501E-13 20 0.82832E-08 0.22412E-06 0.24536E+01 c k 0.71218E-06 2 0.11055E-06 0.30330E-07 0.26631E+01 c omega 0.13153E+02 1 0.54772E-08 0.28788E+01 0.88331E-02 c TempK 0.94432E+02 1 0.28389E-06 0.68957E-01 0.29175E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.4074e-13 1.1608e-13 -1.4078e-17 -3.5722e-18 v Velocity[Y] -0.00016017 0.00015772 -1.0428e-09 -5.0173e-12 v Velocity[Z] -0.00015772 0.00016017 9.3863e-10 -1.7789e-12 v ǁVelocityǁ 1.1306e-10 0.00017733 1.0917e-05 5.918e-06 v Pressure -0.00056364 0.014749 0.00073956 -3.1083e-20 v k 6.3654e-09 0.0023654 0.001665 0.0020368 v omega 26.499 1.0313e+05 2674.8 510.19 v TempK 288 341.63 292.66 289.96 v Density 1.205 1.205 1.205 1.205 v TurbVisc 7.4917e-14 0.00010205 6.9001e-05 8.7591e-05 v CourantNb 1.3274e-09 0.00028406 1.5907e-05 8.0247e-06 v FourierNb 0.13856 0.6281 0.21481 0.18329 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9131 4.9132 0.00041694 -3.5053e-07 v volume_forces[Z] -4.9131 4.9132 -0.0004168 4.2899e-07 v ǁvolume_forcesǁ 4.0965e-09 4.9148 0.42353 0.17697 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.88 290.1 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.018424 6.3592e-05 3.5969e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.13856 0.6281 0.21482 0.1833 INSTANT 0.323568000E+00 TIME STEP NUMBER 336 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.18252E-05 0.27671E-02 Friction velocity uk : 0.18806E-05 0.27670E-02 Dimensionless distance yplus : 0.12523E-04 0.18409E-01 Friction thermal sca. tstar : -0.17045E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.87951E-05 0.12929E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.18252E-05 0.27671E-02 Friction velocity uk : 0.18806E-05 0.27670E-02 Dimensionless distance yplus : 0.12523E-04 0.18409E-01 Friction thermal sca. tstar : -0.17045E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.87951E-05 0.12929E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.36858E-08 3 0.40199E-06 0.11783E-11 0.19493E+01 c Velocity[X] 0.95277E-31 c Velocity[Y] 0.58913E-12 c Velocity[Z] 0.58913E-12 c Pressure 0.28295E-13 20 0.82402E-08 0.22249E-06 0.24461E+01 c k 0.71042E-06 2 0.11005E-06 0.30050E-07 0.26574E+01 c omega 0.13153E+02 1 0.54498E-08 0.28546E+01 0.87959E-02 c TempK 0.94433E+02 1 0.28274E-06 0.68657E-01 0.29111E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.4051e-13 1.1589e-13 -1.4059e-17 -3.5676e-18 v Velocity[Y] -0.00015997 0.00015751 -1.0439e-09 -5.0017e-12 v Velocity[Z] -0.00015751 0.00015997 9.3917e-10 -1.782e-12 v ǁVelocityǁ 1.1288e-10 0.00017703 1.0907e-05 5.9157e-06 v Pressure -0.00056535 0.014771 0.00074109 4.8536e-20 v k 6.3194e-09 0.002359 0.0016605 0.0020316 v omega 26.443 1.0313e+05 2674.7 510.14 v TempK 288 341.63 292.67 289.96 v Density 1.205 1.205 1.205 1.205 v TurbVisc 7.4375e-14 0.00010199 6.8958e-05 8.7547e-05 v CourantNb 1.3315e-09 0.0002836 1.5886e-05 8.0167e-06 v FourierNb 0.13845 0.6281 0.21469 0.1832 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9133 4.9133 0.00041734 -3.5129e-07 v volume_forces[Z] -4.9133 4.9133 -0.0004172 4.2986e-07 v ǁvolume_forcesǁ 4.0873e-09 4.915 0.42393 0.17724 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.89 290.11 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.018409 6.3549e-05 3.5944e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.13845 0.6281 0.21471 0.18321 INSTANT 0.324531000E+00 TIME STEP NUMBER 337 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.17002E-05 0.27649E-02 Friction velocity uk : 0.17588E-05 0.27648E-02 Dimensionless distance yplus : 0.11712E-04 0.18394E-01 Friction thermal sca. tstar : -0.16592E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.82255E-05 0.12919E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.17002E-05 0.27649E-02 Friction velocity uk : 0.17588E-05 0.27648E-02 Dimensionless distance yplus : 0.11712E-04 0.18394E-01 Friction thermal sca. tstar : -0.16592E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.82255E-05 0.12919E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.36815E-08 3 0.40020E-06 0.11645E-11 0.19403E+01 c Velocity[X] 0.94080E-31 c Velocity[Y] 0.58224E-12 c Velocity[Z] 0.58225E-12 c Pressure 0.28122E-13 20 0.82018E-08 0.22112E-06 0.24386E+01 c k 0.70867E-06 2 0.10955E-06 0.29772E-07 0.26518E+01 c omega 0.13153E+02 1 0.54226E-08 0.28307E+01 0.87589E-02 c TempK 0.94433E+02 1 0.28159E-06 0.68360E-01 0.29047E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.4028e-13 1.157e-13 -1.404e-17 -3.5631e-18 v Velocity[Y] -0.00015977 0.0001573 -1.045e-09 -4.9862e-12 v Velocity[Z] -0.0001573 0.00015978 9.3971e-10 -1.7851e-12 v ǁVelocityǁ 1.1278e-10 0.00017673 1.0896e-05 5.9135e-06 v Pressure -0.00056706 0.014794 0.00074262 3.3828e-21 v k 6.2739e-09 0.0023527 0.001656 0.0020264 v omega 26.388 1.0313e+05 2674.7 510.09 v TempK 288 341.63 292.67 289.97 v Density 1.205 1.205 1.205 1.205 v TurbVisc 7.3838e-14 0.00010193 6.8916e-05 8.7503e-05 v CourantNb 1.3356e-09 0.00028314 1.5866e-05 8.0089e-06 v FourierNb 0.13834 0.6281 0.21458 0.18311 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9135 4.9135 0.00041774 -3.5204e-07 v volume_forces[Z] -4.9135 4.9135 -0.0004176 4.3073e-07 v ǁvolume_forcesǁ 4.0808e-09 4.9152 0.42434 0.17751 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.89 290.11 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.018394 6.3506e-05 3.5918e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.13835 0.6281 0.2146 0.18311 INSTANT 0.325494000E+00 TIME STEP NUMBER 338 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15647E-05 0.27627E-02 Friction velocity uk : 0.16274E-05 0.27625E-02 Dimensionless distance yplus : 0.10837E-04 0.18379E-01 Friction thermal sca. tstar : -0.16173E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.76110E-05 0.12908E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15647E-05 0.27627E-02 Friction velocity uk : 0.16274E-05 0.27625E-02 Dimensionless distance yplus : 0.10837E-04 0.18379E-01 Friction thermal sca. tstar : -0.16173E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.76110E-05 0.12908E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.36772E-08 3 0.39850E-06 0.11509E-11 0.19313E+01 c Velocity[X] 0.92901E-31 c Velocity[Y] 0.57547E-12 c Velocity[Z] 0.57547E-12 c Pressure 0.28037E-13 20 0.81708E-08 0.22044E-06 0.24311E+01 c k 0.70693E-06 2 0.10907E-06 0.29498E-07 0.26461E+01 c omega 0.13153E+02 1 0.53955E-08 0.28070E+01 0.87222E-02 c TempK 0.94434E+02 1 0.28046E-06 0.68065E-01 0.28984E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.4006e-13 1.1551e-13 -1.4021e-17 -3.5586e-18 v Velocity[Y] -0.00015958 0.00015709 -1.046e-09 -4.971e-12 v Velocity[Z] -0.00015709 0.00015958 9.4023e-10 -1.7884e-12 v ǁVelocityǁ 1.1276e-10 0.00017643 1.0886e-05 5.9113e-06 v Pressure -0.00056877 0.014816 0.00074415 2.6278e-20 v k 6.2288e-09 0.0023465 0.0016515 0.0020212 v omega 26.333 1.0313e+05 2674.7 510.03 v TempK 288 341.63 292.68 289.97 v Density 1.205 1.205 1.205 1.205 v TurbVisc 7.3306e-14 0.00010188 6.8873e-05 8.746e-05 v CourantNb 1.3397e-09 0.00028268 1.5845e-05 8.0011e-06 v FourierNb 0.13824 0.6281 0.21447 0.18301 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9136 4.9137 0.00041814 -3.528e-07 v volume_forces[Z] -4.9136 4.9137 -0.000418 4.316e-07 v ǁvolume_forcesǁ 4.077e-09 4.9153 0.42474 0.17777 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.9 290.11 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.018379 6.3464e-05 3.5893e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.13824 0.6281 0.21449 0.18302 INSTANT 0.326457000E+00 TIME STEP NUMBER 339 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.14159E-05 0.27604E-02 Friction velocity uk : 0.14839E-05 0.27603E-02 Dimensionless distance yplus : 0.98812E-05 0.18365E-01 Friction thermal sca. tstar : -0.15784E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.69399E-05 0.12898E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.14159E-05 0.27604E-02 Friction velocity uk : 0.14839E-05 0.27603E-02 Dimensionless distance yplus : 0.98812E-05 0.18365E-01 Friction thermal sca. tstar : -0.15784E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.69399E-05 0.12898E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.36730E-08 3 0.39669E-06 0.11376E-11 0.19225E+01 c Velocity[X] 0.91743E-31 c Velocity[Y] 0.56879E-12 c Velocity[Z] 0.56880E-12 c Pressure 0.27800E-13 20 0.81263E-08 0.21856E-06 0.24237E+01 c k 0.70519E-06 2 0.10858E-06 0.29227E-07 0.26405E+01 c omega 0.13153E+02 1 0.53687E-08 0.27835E+01 0.86857E-02 c TempK 0.94435E+02 1 0.27933E-06 0.67772E-01 0.28922E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.3983e-13 1.1532e-13 -1.4002e-17 -3.5541e-18 v Velocity[Y] -0.00015939 0.00015688 -1.047e-09 -4.9554e-12 v Velocity[Z] -0.00015688 0.00015939 9.4074e-10 -1.7915e-12 v ǁVelocityǁ 1.1281e-10 0.00017614 1.0876e-05 5.9092e-06 v Pressure -0.00057049 0.014838 0.00074567 -3.5765e-20 v k 6.1842e-09 0.0023403 0.001647 0.0020161 v omega 26.279 1.0313e+05 2674.6 509.98 v TempK 288 341.63 292.68 289.97 v Density 1.205 1.205 1.205 1.205 v TurbVisc 7.2779e-14 0.00010182 6.8831e-05 8.7417e-05 v CourantNb 1.3438e-09 0.00028223 1.5825e-05 7.9935e-06 v FourierNb 0.13813 0.6281 0.21436 0.18292 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9138 4.9138 0.00041854 -3.5355e-07 v volume_forces[Z] -4.9138 4.9138 -0.0004184 4.3246e-07 v ǁvolume_forcesǁ 4.0761e-09 4.9155 0.42514 0.17804 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.9 290.12 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.018365 6.3421e-05 3.5867e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.13813 0.6281 0.21438 0.18293 INSTANT 0.327420000E+00 TIME STEP NUMBER 340 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12488E-05 0.27582E-02 Friction velocity uk : 0.13242E-05 0.27581E-02 Dimensionless distance yplus : 0.88176E-05 0.18350E-01 Friction thermal sca. tstar : -0.15421E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.61929E-05 0.12888E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12488E-05 0.27582E-02 Friction velocity uk : 0.13242E-05 0.27581E-02 Dimensionless distance yplus : 0.88176E-05 0.18350E-01 Friction thermal sca. tstar : -0.15421E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.61929E-05 0.12888E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.36689E-08 3 0.39491E-06 0.11244E-11 0.19136E+01 c Velocity[X] 0.90601E-31 c Velocity[Y] 0.56222E-12 c Velocity[Z] 0.56223E-12 c Pressure 0.27624E-13 20 0.80899E-08 0.21717E-06 0.24164E+01 c k 0.70346E-06 2 0.10810E-06 0.28959E-07 0.26349E+01 c omega 0.13153E+02 1 0.53420E-08 0.27603E+01 0.86494E-02 c TempK 0.94435E+02 1 0.27821E-06 0.67481E-01 0.28859E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.3961e-13 1.1513e-13 -1.3984e-17 -3.5497e-18 v Velocity[Y] -0.0001592 0.00015667 -1.048e-09 -4.9399e-12 v Velocity[Z] -0.00015667 0.0001592 9.4123e-10 -1.7945e-12 v ǁVelocityǁ 1.1294e-10 0.00017584 1.0866e-05 5.9072e-06 v Pressure -0.0005722 0.01486 0.0007472 2.2479e-20 v k 6.14e-09 0.0023341 0.0016426 0.0020109 v omega 26.224 1.0313e+05 2674.6 509.94 v TempK 288 341.63 292.68 289.97 v Density 1.205 1.205 1.205 1.205 v TurbVisc 7.2258e-14 0.00010176 6.8789e-05 8.7373e-05 v CourantNb 1.348e-09 0.00028178 1.5805e-05 7.986e-06 v FourierNb 0.13803 0.6281 0.21425 0.18283 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.914 4.914 0.00041894 -3.543e-07 v volume_forces[Z] -4.914 4.914 -0.0004188 4.3333e-07 v ǁvolume_forcesǁ 4.078e-09 4.9157 0.42554 0.17831 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.91 290.12 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.01835 6.3379e-05 3.5842e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.13803 0.6281 0.21427 0.18284 INSTANT 0.328383000E+00 TIME STEP NUMBER 341 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10551E-05 0.27560E-02 Friction velocity uk : 0.11417E-05 0.27559E-02 Dimensionless distance yplus : 0.76024E-05 0.18335E-01 Friction thermal sca. tstar : -0.15082E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.53394E-05 0.12877E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10551E-05 0.27560E-02 Friction velocity uk : 0.11417E-05 0.27559E-02 Dimensionless distance yplus : 0.76024E-05 0.18335E-01 Friction thermal sca. tstar : -0.15082E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.53394E-05 0.12877E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.36648E-08 3 0.41046E-06 0.11115E-11 0.19049E+01 c Velocity[X] 0.89478E-31 c Velocity[Y] 0.55575E-12 c Velocity[Z] 0.55576E-12 c Pressure 0.27503E-13 20 0.80535E-08 0.21620E-06 0.24090E+01 c k 0.70175E-06 2 0.10762E-06 0.28693E-07 0.26294E+01 c omega 0.13153E+02 1 0.53156E-08 0.27373E+01 0.86133E-02 c TempK 0.94436E+02 1 0.27710E-06 0.67192E-01 0.28797E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.3938e-13 1.1495e-13 -1.3965e-17 -3.5452e-18 v Velocity[Y] -0.00015901 0.00015647 -1.049e-09 -4.9247e-12 v Velocity[Z] -0.00015647 0.00015901 9.4172e-10 -1.7976e-12 v ǁVelocityǁ 1.1315e-10 0.00017555 1.0856e-05 5.9053e-06 v Pressure -0.00057391 0.014883 0.00074872 -4.4148e-20 v k 6.0962e-09 0.0023279 0.0016381 0.0020058 v omega 26.17 1.0313e+05 2674.5 509.89 v TempK 288 341.64 292.69 289.98 v Density 1.205 1.205 1.205 1.205 v TurbVisc 7.1741e-14 0.0001017 6.8747e-05 8.733e-05 v CourantNb 1.3521e-09 0.00028133 1.5786e-05 7.9786e-06 v FourierNb 0.13792 0.6281 0.21414 0.18274 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9141 4.9142 0.00041934 -3.5505e-07 v volume_forces[Z] -4.9141 4.9142 -0.00041919 4.3418e-07 v ǁvolume_forcesǁ 4.0828e-09 4.9158 0.42594 0.17857 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.91 290.12 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.018335 6.3337e-05 3.5817e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.13792 0.6281 0.21416 0.18275 INSTANT 0.329346000E+00 TIME STEP NUMBER 342 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.81702E-06 0.27538E-02 Friction velocity uk : 0.92298E-06 0.27537E-02 Dimensionless distance yplus : 0.61460E-05 0.18321E-01 Friction thermal sca. tstar : -0.14765E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.43166E-05 0.12867E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.81702E-06 0.27538E-02 Friction velocity uk : 0.92298E-06 0.27537E-02 Dimensionless distance yplus : 0.61460E-05 0.18321E-01 Friction thermal sca. tstar : -0.14765E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.43166E-05 0.12867E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.36608E-08 3 0.39147E-06 0.10988E-11 0.18962E+01 c Velocity[X] 0.88374E-31 c Velocity[Y] 0.54938E-12 c Velocity[Z] 0.54938E-12 c Pressure 0.27326E-13 20 0.80165E-08 0.21481E-06 0.24018E+01 c k 0.70003E-06 2 0.10715E-06 0.28431E-07 0.26238E+01 c omega 0.13153E+02 1 0.52893E-08 0.27146E+01 0.85775E-02 c TempK 0.94437E+02 1 0.27599E-06 0.66905E-01 0.28735E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.3916e-13 1.1476e-13 -1.3947e-17 -3.5408e-18 v Velocity[Y] -0.00015882 0.00015626 -1.05e-09 -4.9094e-12 v Velocity[Z] -0.00015626 0.00015882 9.4219e-10 -1.8007e-12 v ǁVelocityǁ 1.1344e-10 0.00017526 1.0846e-05 5.9035e-06 v Pressure -0.00057563 0.014905 0.00075023 8.7267e-21 v k 6.0528e-09 0.0023218 0.0016337 0.0020008 v omega 26.116 1.0313e+05 2674.5 509.84 v TempK 288 341.64 292.69 289.98 v Density 1.205 1.205 1.205 1.205 v TurbVisc 7.1229e-14 0.00010164 6.8705e-05 8.7287e-05 v CourantNb 1.3562e-09 0.00028089 1.5766e-05 7.9713e-06 v FourierNb 0.13781 0.6281 0.21403 0.18265 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9143 4.9144 0.00041973 -3.558e-07 v volume_forces[Z] -4.9143 4.9144 -0.00041959 4.3504e-07 v ǁvolume_forcesǁ 4.0905e-09 4.916 0.42633 0.17884 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.91 290.12 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.018321 6.3295e-05 3.5792e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.13782 0.6281 0.21405 0.18266 INSTANT 0.330309000E+00 TIME STEP NUMBER 343 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.47799E-06 0.27517E-02 Friction velocity uk : 0.63131E-06 0.27515E-02 Dimensionless distance yplus : 0.42038E-05 0.18306E-01 Friction thermal sca. tstar : -0.15067E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.29525E-05 0.12857E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.47799E-06 0.27517E-02 Friction velocity uk : 0.63131E-06 0.27515E-02 Dimensionless distance yplus : 0.42038E-05 0.18306E-01 Friction thermal sca. tstar : -0.15067E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.29525E-05 0.12857E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.36568E-08 3 0.38974E-06 0.10862E-11 0.18875E+01 c Velocity[X] 0.87286E-31 c Velocity[Y] 0.54311E-12 c Velocity[Z] 0.54312E-12 c Pressure 0.27153E-13 20 0.79791E-08 0.21344E-06 0.23945E+01 c k 0.69833E-06 2 0.10668E-06 0.28172E-07 0.26183E+01 c omega 0.13153E+02 1 0.52632E-08 0.26921E+01 0.85419E-02 c TempK 0.94437E+02 1 0.27490E-06 0.66620E-01 0.28674E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.3894e-13 1.1458e-13 -1.3928e-17 -3.5364e-18 v Velocity[Y] -0.00015863 0.00015606 -1.051e-09 -4.8944e-12 v Velocity[Z] -0.00015606 0.00015864 9.4265e-10 -1.8039e-12 v ǁVelocityǁ 1.1382e-10 0.00017497 1.0837e-05 5.9017e-06 v Pressure -0.00057734 0.014927 0.00075175 -2.6082e-20 v k 6.0098e-09 0.0023156 0.0016294 0.0019957 v omega 26.062 1.0313e+05 2674.5 509.79 v TempK 288 341.64 292.7 289.98 v Density 1.205 1.205 1.205 1.205 v TurbVisc 7.0723e-14 0.00010159 6.8663e-05 8.7244e-05 v CourantNb 1.3603e-09 0.00028045 1.5747e-05 7.9641e-06 v FourierNb 0.13771 0.6281 0.21392 0.18256 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9145 4.9145 0.00042013 -3.5654e-07 v volume_forces[Z] -4.9145 4.9145 -0.00041999 4.3589e-07 v ǁvolume_forcesǁ 4.101e-09 4.9162 0.42673 0.1791 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.92 290.13 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.018306 6.3254e-05 3.5767e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.13771 0.6281 0.21394 0.18257 INSTANT 0.331272000E+00 TIME STEP NUMBER 344 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.30574E-06 0.27495E-02 Friction velocity uk : 0.49804E-06 0.27494E-02 Dimensionless distance yplus : 0.33164E-05 0.18292E-01 Friction thermal sca. tstar : -0.15430E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.23292E-05 0.12847E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.30574E-06 0.27495E-02 Friction velocity uk : 0.49804E-06 0.27494E-02 Dimensionless distance yplus : 0.33164E-05 0.18292E-01 Friction thermal sca. tstar : -0.15430E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.23292E-05 0.12847E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.36529E-08 3 0.38808E-06 0.10739E-11 0.18790E+01 c Velocity[X] 0.86217E-31 c Velocity[Y] 0.53694E-12 c Velocity[Z] 0.53695E-12 c Pressure 0.27001E-13 20 0.79451E-08 0.21223E-06 0.23873E+01 c k 0.69663E-06 2 0.10621E-06 0.27916E-07 0.26128E+01 c omega 0.13153E+02 1 0.52373E-08 0.26698E+01 0.85065E-02 c TempK 0.94438E+02 1 0.27381E-06 0.66338E-01 0.28612E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.3872e-13 1.144e-13 -1.391e-17 -3.532e-18 v Velocity[Y] -0.00015845 0.00015586 -1.052e-09 -4.8793e-12 v Velocity[Z] -0.00015586 0.00015845 9.4309e-10 -1.8072e-12 v ǁVelocityǁ 1.1427e-10 0.00017468 1.0827e-05 5.9e-06 v Pressure -0.00057905 0.014949 0.00075326 -1.8507e-20 v k 5.9673e-09 0.0023096 0.001625 0.0019907 v omega 26.009 1.0313e+05 2674.4 509.74 v TempK 288 341.64 292.7 289.99 v Density 1.205 1.205 1.205 1.205 v TurbVisc 7.0221e-14 0.00010153 6.8621e-05 8.7201e-05 v CourantNb 1.3644e-09 0.00028001 1.5728e-05 7.957e-06 v FourierNb 0.1376 0.6281 0.21381 0.18247 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9146 4.9147 0.00042052 -3.5728e-07 v volume_forces[Z] -4.9146 4.9147 -0.00042038 4.3674e-07 v ǁvolume_forcesǁ 4.1145e-09 4.9163 0.42713 0.17937 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.92 290.13 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.018292 6.3212e-05 3.5743e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.13761 0.6281 0.21383 0.18248 INSTANT 0.332235000E+00 TIME STEP NUMBER 345 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.72522E-06 0.27474E-02 Friction velocity uk : 0.83825E-06 0.27472E-02 Dimensionless distance yplus : 0.55818E-05 0.18277E-01 Friction thermal sca. tstar : -0.15820E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.39203E-05 0.12837E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.72522E-06 0.27474E-02 Friction velocity uk : 0.83825E-06 0.27472E-02 Dimensionless distance yplus : 0.55818E-05 0.18277E-01 Friction thermal sca. tstar : -0.15820E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.39203E-05 0.12837E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.36490E-08 3 0.38638E-06 0.10617E-11 0.18705E+01 c Velocity[X] 0.85163E-31 c Velocity[Y] 0.53087E-12 c Velocity[Z] 0.53087E-12 c Pressure 0.26887E-13 20 0.79172E-08 0.21132E-06 0.23802E+01 c k 0.69494E-06 2 0.10575E-06 0.27663E-07 0.26074E+01 c omega 0.13153E+02 1 0.52115E-08 0.26478E+01 0.84713E-02 c TempK 0.94439E+02 1 0.27272E-06 0.66057E-01 0.28551E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.3851e-13 1.1422e-13 -1.3892e-17 -3.5277e-18 v Velocity[Y] -0.00015826 0.00015566 -1.0529e-09 -4.8645e-12 v Velocity[Z] -0.00015566 0.00015826 9.4353e-10 -1.8101e-12 v ǁVelocityǁ 1.1413e-10 0.0001744 1.0818e-05 5.8984e-06 v Pressure -0.00058077 0.014971 0.00075478 4.8046e-21 v k 5.9252e-09 0.0023035 0.0016207 0.0019857 v omega 25.955 1.0313e+05 2674.4 509.69 v TempK 288 341.64 292.71 289.99 v Density 1.205 1.205 1.205 1.205 v TurbVisc 6.9724e-14 0.00010147 6.858e-05 8.7158e-05 v CourantNb 1.3685e-09 0.00027957 1.5709e-05 7.95e-06 v FourierNb 0.1375 0.6281 0.2137 0.18238 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9148 4.9149 0.00042092 -3.5802e-07 v volume_forces[Z] -4.9148 4.9149 -0.00042077 4.3759e-07 v ǁvolume_forcesǁ 4.1309e-09 4.9165 0.42752 0.17963 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.93 290.13 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.018277 6.3171e-05 3.5718e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.1375 0.6281 0.21372 0.18239 INSTANT 0.333198000E+00 TIME STEP NUMBER 346 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.98944E-06 0.27452E-02 Friction velocity uk : 0.10765E-05 0.27451E-02 Dimensionless distance yplus : 0.71684E-05 0.18263E-01 Friction thermal sca. tstar : -0.16242E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.50346E-05 0.12827E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.98944E-06 0.27452E-02 Friction velocity uk : 0.10765E-05 0.27451E-02 Dimensionless distance yplus : 0.71684E-05 0.18263E-01 Friction thermal sca. tstar : -0.16242E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.50346E-05 0.12827E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.36451E-08 3 0.38468E-06 0.10498E-11 0.18620E+01 c Velocity[X] 0.84129E-31 c Velocity[Y] 0.52489E-12 c Velocity[Z] 0.52489E-12 c Pressure 0.26679E-13 20 0.78698E-08 0.20968E-06 0.23731E+01 c k 0.69326E-06 2 0.10529E-06 0.27412E-07 0.26019E+01 c omega 0.13153E+02 1 0.51860E-08 0.26260E+01 0.84363E-02 c TempK 0.94440E+02 1 0.27165E-06 0.65778E-01 0.28491E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.3829e-13 1.1404e-13 -1.3874e-17 -3.5233e-18 v Velocity[Y] -0.00015808 0.00015546 -1.0539e-09 -4.8475e-12 v Velocity[Z] -0.00015546 0.00015808 9.4397e-10 -1.7949e-12 v ǁVelocityǁ 1.1383e-10 0.00017412 1.0809e-05 5.8969e-06 v Pressure -0.00058248 0.014993 0.00075629 5.0742e-20 v k 5.8834e-09 0.0022975 0.0016163 0.0019807 v omega 25.902 1.0313e+05 2674.3 509.64 v TempK 288 341.65 292.71 289.99 v Density 1.205 1.205 1.205 1.205 v TurbVisc 6.9231e-14 0.00010141 6.8538e-05 8.7116e-05 v CourantNb 1.3726e-09 0.00027914 1.569e-05 7.9432e-06 v FourierNb 0.13739 0.6281 0.2136 0.18229 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.915 4.915 0.00042131 -3.5875e-07 v volume_forces[Z] -4.915 4.915 -0.00042117 4.3843e-07 v ǁvolume_forcesǁ 4.1258e-09 4.9167 0.42791 0.17989 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.93 290.14 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.018263 6.313e-05 3.5694e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.1374 0.6281 0.21361 0.1823 INSTANT 0.334161000E+00 TIME STEP NUMBER 347 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11973E-05 0.27431E-02 Friction velocity uk : 0.12703E-05 0.27429E-02 Dimensionless distance yplus : 0.84588E-05 0.18249E-01 Friction thermal sca. tstar : -0.16700E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.59409E-05 0.12817E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11973E-05 0.27431E-02 Friction velocity uk : 0.12703E-05 0.27429E-02 Dimensionless distance yplus : 0.84588E-05 0.18249E-01 Friction thermal sca. tstar : -0.16700E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.59409E-05 0.12817E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.36413E-08 3 0.38302E-06 0.10380E-11 0.18537E+01 c Velocity[X] 0.83111E-31 c Velocity[Y] 0.51900E-12 c Velocity[Z] 0.51901E-12 c Pressure 0.26522E-13 20 0.78366E-08 0.20844E-06 0.23660E+01 c k 0.69159E-06 2 0.10484E-06 0.27164E-07 0.25965E+01 c omega 0.13153E+02 1 0.51606E-08 0.26044E+01 0.84016E-02 c TempK 0.94440E+02 1 0.27058E-06 0.65501E-01 0.28430E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.3808e-13 1.1386e-13 -1.3856e-17 -3.519e-18 v Velocity[Y] -0.0001579 0.00015526 -1.0548e-09 -4.8324e-12 v Velocity[Z] -0.00015526 0.0001579 9.4438e-10 -1.798e-12 v ǁVelocityǁ 1.137e-10 0.00017384 1.08e-05 5.8955e-06 v Pressure -0.00058419 0.015015 0.0007578 6.0253e-20 v k 5.8421e-09 0.0022914 0.001612 0.0019757 v omega 25.849 1.0313e+05 2674.3 509.59 v TempK 288 341.65 292.72 289.99 v Density 1.205 1.205 1.205 1.205 v TurbVisc 6.8744e-14 0.00010136 6.8497e-05 8.7073e-05 v CourantNb 1.3767e-09 0.00027871 1.5672e-05 7.9364e-06 v FourierNb 0.13729 0.6281 0.21349 0.1822 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9151 4.9152 0.0004217 -3.5949e-07 v volume_forces[Z] -4.9151 4.9152 -0.00042156 4.3927e-07 v ǁvolume_forcesǁ 4.1149e-09 4.9168 0.42831 0.18016 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.94 290.14 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.018249 6.3089e-05 3.5669e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.13729 0.6281 0.2135 0.18221 INSTANT 0.335124000E+00 TIME STEP NUMBER 348 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12708E-05 0.27410E-02 Friction velocity uk : 0.13393E-05 0.27408E-02 Dimensionless distance yplus : 0.89185E-05 0.18235E-01 Friction thermal sca. tstar : -0.17198E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.62638E-05 0.12807E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12708E-05 0.27410E-02 Friction velocity uk : 0.13393E-05 0.27408E-02 Dimensionless distance yplus : 0.89185E-05 0.18235E-01 Friction thermal sca. tstar : -0.17198E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.62638E-05 0.12807E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.36376E-08 3 0.38137E-06 0.10264E-11 0.18454E+01 c Velocity[X] 0.82108E-31 c Velocity[Y] 0.51321E-12 c Velocity[Z] 0.51322E-12 c Pressure 0.26370E-13 20 0.78023E-08 0.20724E-06 0.23590E+01 c k 0.68992E-06 2 0.10439E-06 0.26919E-07 0.25911E+01 c omega 0.13153E+02 1 0.51354E-08 0.25830E+01 0.83670E-02 c TempK 0.94441E+02 1 0.26952E-06 0.65226E-01 0.28370E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.3786e-13 1.1368e-13 -1.3838e-17 -3.5147e-18 v Velocity[Y] -0.00015772 0.00015507 -1.0557e-09 -4.8176e-12 v Velocity[Z] -0.00015507 0.00015772 9.4477e-10 -1.8012e-12 v ǁVelocityǁ 1.1374e-10 0.00017356 1.0791e-05 5.8941e-06 v Pressure -0.00058591 0.015037 0.0007593 7.1824e-21 v k 5.8011e-09 0.0022854 0.0016078 0.0019708 v omega 25.796 1.0313e+05 2674.3 509.54 v TempK 288 341.65 292.72 290 v Density 1.205 1.205 1.205 1.205 v TurbVisc 6.8261e-14 0.00010132 6.8456e-05 8.7031e-05 v CourantNb 1.3808e-09 0.00027829 1.5654e-05 7.9297e-06 v FourierNb 0.13719 0.6281 0.21338 0.18211 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9153 4.9154 0.00042209 -3.6022e-07 v volume_forces[Z] -4.9153 4.9154 -0.00042195 4.4011e-07 v ǁvolume_forcesǁ 4.1101e-09 4.917 0.4287 0.18042 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.94 290.14 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.018235 6.3048e-05 3.5645e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.13719 0.6281 0.2134 0.18212 INSTANT 0.336087000E+00 TIME STEP NUMBER 349 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.97139E-06 0.27389E-02 Friction velocity uk : 0.10573E-05 0.27387E-02 Dimensionless distance yplus : 0.70404E-05 0.18221E-01 Friction thermal sca. tstar : -0.17745E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.49447E-05 0.12797E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.97139E-06 0.27389E-02 Friction velocity uk : 0.10573E-05 0.27387E-02 Dimensionless distance yplus : 0.70404E-05 0.18221E-01 Friction thermal sca. tstar : -0.17745E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.49447E-05 0.12797E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.36339E-08 3 0.46986E-06 0.10150E-11 0.18372E+01 c Velocity[X] 0.81122E-31 c Velocity[Y] 0.50751E-12 c Velocity[Z] 0.50752E-12 c Pressure 0.26231E-13 20 0.77690E-08 0.20613E-06 0.23520E+01 c k 0.68826E-06 2 0.10395E-06 0.26677E-07 0.25857E+01 c omega 0.13153E+02 1 0.51103E-08 0.25619E+01 0.83327E-02 c TempK 0.94442E+02 1 0.26846E-06 0.64953E-01 0.28311E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.3765e-13 1.1351e-13 -1.382e-17 -3.5105e-18 v Velocity[Y] -0.00015754 0.00015487 -1.0566e-09 -4.803e-12 v Velocity[Z] -0.00015487 0.00015754 9.4516e-10 -1.8041e-12 v ǁVelocityǁ 1.1397e-10 0.00017328 1.0782e-05 5.8928e-06 v Pressure -0.00058762 0.015059 0.00076081 -2.7455e-21 v k 5.7606e-09 0.0022795 0.0016035 0.0019659 v omega 25.744 1.0313e+05 2674.2 509.5 v TempK 288 341.65 292.72 290 v Density 1.205 1.205 1.205 1.205 v TurbVisc 6.7782e-14 0.00010127 6.8415e-05 8.6988e-05 v CourantNb 1.3849e-09 0.00027786 1.5635e-05 7.9232e-06 v FourierNb 0.13708 0.6281 0.21328 0.18203 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9155 4.9155 0.00042248 -3.6095e-07 v volume_forces[Z] -4.9155 4.9155 -0.00042234 4.4095e-07 v ǁvolume_forcesǁ 4.1117e-09 4.9172 0.42909 0.18068 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.94 290.15 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.018221 6.3008e-05 3.5621e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.13708 0.6281 0.21329 0.18203 INSTANT 0.337050000E+00 TIME STEP NUMBER 350 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.52717E-06 0.27368E-02 Friction velocity uk : 0.66282E-06 0.27366E-02 Dimensionless distance yplus : 0.44137E-05 0.18207E-01 Friction thermal sca. tstar : -0.18348E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.30999E-05 0.12787E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.52717E-06 0.27368E-02 Friction velocity uk : 0.66282E-06 0.27366E-02 Dimensionless distance yplus : 0.44137E-05 0.18207E-01 Friction thermal sca. tstar : -0.18348E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.30999E-05 0.12787E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.36303E-08 3 0.37815E-06 0.10038E-11 0.18290E+01 c Velocity[X] 0.80151E-31 c Velocity[Y] 0.50190E-12 c Velocity[Z] 0.50191E-12 c Pressure 0.26079E-13 20 0.77367E-08 0.20493E-06 0.23450E+01 c k 0.68661E-06 2 0.10350E-06 0.26437E-07 0.25804E+01 c omega 0.13153E+02 1 0.50855E-08 0.25409E+01 0.82985E-02 c TempK 0.94442E+02 1 0.26741E-06 0.64682E-01 0.28251E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.3744e-13 1.1334e-13 -1.3803e-17 -3.5062e-18 v Velocity[Y] -0.00015736 0.00015468 -1.0575e-09 -4.7882e-12 v Velocity[Z] -0.00015468 0.00015736 9.4553e-10 -1.8074e-12 v ǁVelocityǁ 1.1437e-10 0.000173 1.0773e-05 5.8915e-06 v Pressure -0.00058933 0.015081 0.00076231 -1.7404e-21 v k 5.7204e-09 0.0022735 0.0015993 0.001961 v omega 25.692 1.0313e+05 2674.2 509.45 v TempK 288 341.65 292.73 290 v Density 1.205 1.205 1.205 1.205 v TurbVisc 6.7308e-14 0.00010122 6.8374e-05 8.6946e-05 v CourantNb 1.389e-09 0.00027744 1.5617e-05 7.9167e-06 v FourierNb 0.13698 0.6281 0.21317 0.18194 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9156 4.9157 0.00042287 -3.6167e-07 v volume_forces[Z] -4.9156 4.9157 -0.00042273 4.4178e-07 v ǁvolume_forcesǁ 4.1198e-09 4.9173 0.42948 0.18094 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.95 290.15 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.018207 6.2968e-05 3.5597e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.13698 0.6281 0.21318 0.18195 INSTANT 0.338013000E+00 TIME STEP NUMBER 351 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.51048E-06 0.27347E-02 Friction velocity uk : 0.64783E-06 0.27345E-02 Dimensionless distance yplus : 0.43138E-05 0.18193E-01 Friction thermal sca. tstar : -0.19017E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.30298E-05 0.12778E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.51048E-06 0.27347E-02 Friction velocity uk : 0.64783E-06 0.27345E-02 Dimensionless distance yplus : 0.43138E-05 0.18193E-01 Friction thermal sca. tstar : -0.19017E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.30298E-05 0.12778E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.36267E-08 3 0.37653E-06 0.99278E-12 0.18209E+01 c Velocity[X] 0.79196E-31 c Velocity[Y] 0.49639E-12 c Velocity[Z] 0.49639E-12 c Pressure 0.25982E-13 20 0.77072E-08 0.20416E-06 0.23381E+01 c k 0.68496E-06 2 0.10307E-06 0.26200E-07 0.25751E+01 c omega 0.13153E+02 1 0.50608E-08 0.25202E+01 0.82646E-02 c TempK 0.94443E+02 1 0.26637E-06 0.64412E-01 0.28192E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.3723e-13 1.1316e-13 -1.3785e-17 -3.502e-18 v Velocity[Y] -0.00015718 0.00015449 -1.0584e-09 -4.7736e-12 v Velocity[Z] -0.00015449 0.00015718 9.4589e-10 -1.8106e-12 v ǁVelocityǁ 1.1495e-10 0.00017273 1.0764e-05 5.8904e-06 v Pressure -0.00059104 0.015103 0.00076381 -5.3463e-20 v k 5.6806e-09 0.0022676 0.0015951 0.0019561 v omega 25.64 1.0313e+05 2674.1 509.4 v TempK 288 341.65 292.73 290.01 v Density 1.205 1.205 1.205 1.205 v TurbVisc 6.6839e-14 0.00010118 6.8333e-05 8.6904e-05 v CourantNb 1.3931e-09 0.00027702 1.56e-05 7.9103e-06 v FourierNb 0.13687 0.6281 0.21306 0.18185 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9158 4.9158 0.00042326 -3.624e-07 v volume_forces[Z] -4.9158 4.9158 -0.00042311 4.4261e-07 v ǁvolume_forcesǁ 4.1344e-09 4.9175 0.42987 0.18121 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.95 290.15 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.018193 6.2928e-05 3.5573e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.13687 0.6281 0.21308 0.18186 INSTANT 0.338976000E+00 TIME STEP NUMBER 352 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.96538E-06 0.27326E-02 Friction velocity uk : 0.10493E-05 0.27325E-02 Dimensionless distance yplus : 0.69870E-05 0.18179E-01 Friction thermal sca. tstar : -0.19765E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.49072E-05 0.12768E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.96538E-06 0.27326E-02 Friction velocity uk : 0.10493E-05 0.27325E-02 Dimensionless distance yplus : 0.69870E-05 0.18179E-01 Friction thermal sca. tstar : -0.19765E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.49072E-05 0.12768E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.36231E-08 3 0.37490E-06 0.98192E-12 0.18129E+01 c Velocity[X] 0.78257E-31 c Velocity[Y] 0.49096E-12 c Velocity[Z] 0.49096E-12 c Pressure 0.25776E-13 20 0.77112E-08 0.20253E-06 0.23313E+01 c k 0.68333E-06 2 0.10263E-06 0.25966E-07 0.25698E+01 c omega 0.13153E+02 1 0.50362E-08 0.24997E+01 0.82309E-02 c TempK 0.94444E+02 1 0.26534E-06 0.64145E-01 0.28133E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.3702e-13 1.1299e-13 -1.3767e-17 -3.4978e-18 v Velocity[Y] -0.000157 0.0001543 -1.0595e-09 -5.01e-12 v Velocity[Z] -0.0001543 0.00015701 9.462e-10 -1.8545e-12 v ǁVelocityǁ 1.1565e-10 0.00017246 1.0756e-05 5.8893e-06 v Pressure -0.00059276 0.015124 0.00076531 -6.3538e-20 v k 5.6411e-09 0.0022617 0.0015909 0.0019512 v omega 25.588 1.0313e+05 2674.1 509.35 v TempK 288 341.66 292.74 290.01 v Density 1.205 1.205 1.205 1.205 v TurbVisc 6.6373e-14 0.00010113 6.8292e-05 8.6862e-05 v CourantNb 1.3972e-09 0.00027661 1.5582e-05 7.9041e-06 v FourierNb 0.13677 0.6281 0.21296 0.18176 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.916 4.916 0.00042364 -3.6312e-07 v volume_forces[Z] -4.916 4.916 -0.0004235 4.4344e-07 v ǁvolume_forcesǁ 4.1555e-09 4.9176 0.43026 0.18147 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.96 290.15 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.018179 6.2888e-05 3.5549e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.13677 0.6281 0.21297 0.18177 INSTANT 0.339939000E+00 TIME STEP NUMBER 353 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12408E-05 0.27305E-02 Friction velocity uk : 0.13074E-05 0.27304E-02 Dimensionless distance yplus : 0.87059E-05 0.18166E-01 Friction thermal sca. tstar : -0.20609E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.61145E-05 0.12758E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12408E-05 0.27305E-02 Friction velocity uk : 0.13074E-05 0.27304E-02 Dimensionless distance yplus : 0.87059E-05 0.18166E-01 Friction thermal sca. tstar : -0.20609E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.61145E-05 0.12758E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.36196E-08 3 0.37334E-06 0.97124E-12 0.18049E+01 c Velocity[X] 0.77332E-31 c Velocity[Y] 0.48561E-12 c Velocity[Z] 0.48562E-12 c Pressure 0.25690E-13 20 0.76845E-08 0.20185E-06 0.23244E+01 c k 0.68170E-06 2 0.10220E-06 0.25734E-07 0.25645E+01 c omega 0.13153E+02 1 0.50119E-08 0.24794E+01 0.81974E-02 c TempK 0.94444E+02 1 0.26431E-06 0.63879E-01 0.28075E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.3681e-13 1.1282e-13 -1.375e-17 -3.4936e-18 v Velocity[Y] -0.00015683 0.00015411 -1.0604e-09 -4.9964e-12 v Velocity[Z] -0.00015411 0.00015683 9.4654e-10 -1.8571e-12 v ǁVelocityǁ 1.1656e-10 0.00017219 1.0748e-05 5.8883e-06 v Pressure -0.00059447 0.015146 0.0007668 6.7166e-21 v k 5.6021e-09 0.0022559 0.0015867 0.0019464 v omega 25.536 1.0313e+05 2674.1 509.31 v TempK 288 341.66 292.74 290.01 v Density 1.205 1.205 1.205 1.205 v TurbVisc 6.5913e-14 0.00010108 6.8252e-05 8.682e-05 v CourantNb 1.4013e-09 0.00027619 1.5565e-05 7.8979e-06 v FourierNb 0.13666 0.6281 0.21285 0.18167 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9161 4.9162 0.00042403 -3.6384e-07 v volume_forces[Z] -4.9161 4.9162 -0.00042389 4.4427e-07 v ǁvolume_forcesǁ 4.1807e-09 4.9178 0.43065 0.18173 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.96 290.16 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.018166 6.2848e-05 3.5525e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.13667 0.6281 0.21287 0.18168 INSTANT 0.340902000E+00 TIME STEP NUMBER 354 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.14774E-05 0.27285E-02 Friction velocity uk : 0.15335E-05 0.27283E-02 Dimensionless distance yplus : 0.10212E-04 0.18152E-01 Friction thermal sca. tstar : -0.21572E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.71724E-05 0.12749E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.14774E-05 0.27285E-02 Friction velocity uk : 0.15335E-05 0.27283E-02 Dimensionless distance yplus : 0.10212E-04 0.18152E-01 Friction thermal sca. tstar : -0.21572E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.71724E-05 0.12749E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.36161E-08 3 0.37174E-06 0.96072E-12 0.17970E+01 c Velocity[X] 0.76422E-31 c Velocity[Y] 0.48036E-12 c Velocity[Z] 0.48037E-12 c Pressure 0.25502E-13 20 0.76469E-08 0.20036E-06 0.23177E+01 c k 0.68007E-06 2 0.10177E-06 0.25505E-07 0.25592E+01 c omega 0.13153E+02 1 0.49877E-08 0.24592E+01 0.81641E-02 c TempK 0.94445E+02 1 0.26329E-06 0.63615E-01 0.28016E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.3661e-13 1.1265e-13 -1.3733e-17 -3.4894e-18 v Velocity[Y] -0.00015665 0.00015392 -1.0612e-09 -4.9811e-12 v Velocity[Z] -0.00015392 0.00015666 9.4686e-10 -1.8605e-12 v ǁVelocityǁ 1.1766e-10 0.00017193 1.0739e-05 5.8874e-06 v Pressure -0.00059618 0.015168 0.0007683 -1.939e-20 v k 5.5634e-09 0.00225 0.0015825 0.0019416 v omega 25.485 1.0313e+05 2674 509.26 v TempK 288 341.66 292.75 290.02 v Density 1.205 1.205 1.205 1.205 v TurbVisc 6.5456e-14 0.00010104 6.8211e-05 8.6778e-05 v CourantNb 1.4054e-09 0.00027578 1.5547e-05 7.8918e-06 v FourierNb 0.13656 0.6281 0.21275 0.18159 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9163 4.9163 0.00042442 -3.6456e-07 v volume_forces[Z] -4.9163 4.9163 -0.00042427 4.4509e-07 v ǁvolume_forcesǁ 4.2138e-09 4.918 0.43104 0.18199 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.97 290.16 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.018152 6.2808e-05 3.5502e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.13656 0.6281 0.21276 0.18159 INSTANT 0.341865000E+00 TIME STEP NUMBER 355 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12319E-05 0.27264E-02 Friction velocity uk : 0.12976E-05 0.27263E-02 Dimensionless distance yplus : 0.86411E-05 0.18138E-01 Friction thermal sca. tstar : -0.22685E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.60690E-05 0.12739E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12319E-05 0.27264E-02 Friction velocity uk : 0.12976E-05 0.27263E-02 Dimensionless distance yplus : 0.86411E-05 0.18138E-01 Friction thermal sca. tstar : -0.22685E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.60690E-05 0.12739E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.36127E-08 3 0.37016E-06 0.95039E-12 0.17892E+01 c Velocity[X] 0.75527E-31 c Velocity[Y] 0.47519E-12 c Velocity[Z] 0.47520E-12 c Pressure 0.25368E-13 20 0.76133E-08 0.19930E-06 0.23109E+01 c k 0.67846E-06 2 0.10135E-06 0.25278E-07 0.25540E+01 c omega 0.13153E+02 1 0.49636E-08 0.24393E+01 0.81310E-02 c TempK 0.94446E+02 1 0.26228E-06 0.63353E-01 0.27958E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.364e-13 1.1248e-13 -1.3715e-17 -3.4853e-18 v Velocity[Y] -0.00015648 0.00015373 -1.062e-09 -4.9665e-12 v Velocity[Z] -0.00015373 0.00015648 9.4718e-10 -1.8636e-12 v ǁVelocityǁ 1.1893e-10 0.00017168 1.0731e-05 5.8865e-06 v Pressure -0.00059789 0.01519 0.00076979 2.3239e-20 v k 5.525e-09 0.0022442 0.0015784 0.0019368 v omega 25.433 1.0313e+05 2674 509.21 v TempK 288 341.66 292.75 290.02 v Density 1.205 1.205 1.205 1.205 v TurbVisc 6.5004e-14 0.00010099 6.8171e-05 8.6736e-05 v CourantNb 1.4095e-09 0.00027538 1.553e-05 7.8859e-06 v FourierNb 0.13646 0.6281 0.21264 0.1815 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9164 4.9165 0.0004248 -3.6527e-07 v volume_forces[Z] -4.9164 4.9165 -0.00042466 4.4591e-07 v ǁvolume_forcesǁ 4.2534e-09 4.9181 0.43142 0.18225 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.97 290.16 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.018138 6.2769e-05 3.5478e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.13646 0.6281 0.21266 0.18151 INSTANT 0.342828000E+00 TIME STEP NUMBER 356 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.92290E-06 0.27244E-02 Friction velocity uk : 0.10066E-05 0.27243E-02 Dimensionless distance yplus : 0.67037E-05 0.18125E-01 Friction thermal sca. tstar : -0.23990E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.47083E-05 0.12730E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.92290E-06 0.27244E-02 Friction velocity uk : 0.10066E-05 0.27243E-02 Dimensionless distance yplus : 0.67037E-05 0.18125E-01 Friction thermal sca. tstar : -0.23990E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.47083E-05 0.12730E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.36093E-08 3 0.37284E-06 0.94021E-12 0.17815E+01 c Velocity[X] 0.74647E-31 c Velocity[Y] 0.47010E-12 c Velocity[Z] 0.47011E-12 c Pressure 0.25226E-13 20 0.75853E-08 0.19817E-06 0.23042E+01 c k 0.67685E-06 2 0.10093E-06 0.25054E-07 0.25488E+01 c omega 0.13153E+02 1 0.49398E-08 0.24196E+01 0.80980E-02 c TempK 0.94446E+02 1 0.26127E-06 0.63093E-01 0.27900E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.362e-13 1.1231e-13 -1.3698e-17 -3.4811e-18 v Velocity[Y] -0.00015631 0.00015355 -1.0629e-09 -4.9519e-12 v Velocity[Z] -0.00015355 0.00015631 9.4748e-10 -1.8669e-12 v ǁVelocityǁ 1.2036e-10 0.00017143 1.0723e-05 5.8857e-06 v Pressure -0.0005996 0.015211 0.00077128 5.3096e-20 v k 5.487e-09 0.0022384 0.0015743 0.0019321 v omega 25.382 1.0313e+05 2673.9 509.17 v TempK 288 341.66 292.75 290.02 v Density 1.205 1.205 1.205 1.205 v TurbVisc 6.4556e-14 0.00010094 6.8131e-05 8.6694e-05 v CourantNb 1.4136e-09 0.00027497 1.5513e-05 7.88e-06 v FourierNb 0.13635 0.6281 0.21254 0.18141 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9166 4.9167 0.00042519 -3.6599e-07 v volume_forces[Z] -4.9166 4.9167 -0.00042504 4.4673e-07 v ǁvolume_forcesǁ 4.2992e-09 4.9183 0.43181 0.18251 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.97 290.17 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.018125 6.273e-05 3.5455e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.13636 0.6281 0.21255 0.18142 INSTANT 0.343791000E+00 TIME STEP NUMBER 357 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.44068E-06 0.27224E-02 Friction velocity uk : 0.58367E-06 0.27222E-02 Dimensionless distance yplus : 0.38870E-05 0.18111E-01 Friction thermal sca. tstar : -0.25550E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.27300E-05 0.12720E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.44068E-06 0.27224E-02 Friction velocity uk : 0.58367E-06 0.27222E-02 Dimensionless distance yplus : 0.38870E-05 0.18111E-01 Friction thermal sca. tstar : -0.25550E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.27300E-05 0.12720E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.36060E-08 3 0.37153E-06 0.93021E-12 0.17738E+01 c Velocity[X] 0.73779E-31 c Velocity[Y] 0.46510E-12 c Velocity[Z] 0.46511E-12 c Pressure 0.25076E-13 20 0.75548E-08 0.19699E-06 0.22975E+01 c k 0.67524E-06 2 0.10051E-06 0.24832E-07 0.25436E+01 c omega 0.13153E+02 1 0.49161E-08 0.24001E+01 0.80653E-02 c TempK 0.94447E+02 1 0.26027E-06 0.62834E-01 0.27843E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.36e-13 1.1215e-13 -1.3681e-17 -3.477e-18 v Velocity[Y] -0.00015614 0.00015336 -1.0637e-09 -4.9374e-12 v Velocity[Z] -0.00015336 0.00015614 9.4777e-10 -1.8698e-12 v ǁVelocityǁ 1.2196e-10 0.00017117 1.0715e-05 5.885e-06 v Pressure -0.00060132 0.015233 0.00077277 2.4513e-22 v k 5.4494e-09 0.0022326 0.0015702 0.0019273 v omega 25.332 1.0313e+05 2673.9 509.12 v TempK 288 341.67 292.76 290.02 v Density 1.205 1.205 1.205 1.205 v TurbVisc 6.4112e-14 0.0001009 6.809e-05 8.6653e-05 v CourantNb 1.4177e-09 0.00027457 1.5496e-05 7.8742e-06 v FourierNb 0.13625 0.6281 0.21244 0.18133 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9168 4.9168 0.00042557 -3.667e-07 v volume_forces[Z] -4.9168 4.9168 -0.00042543 4.4754e-07 v ǁvolume_forcesǁ 4.3511e-09 4.9184 0.43219 0.18277 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.98 290.17 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.018111 6.2691e-05 3.5431e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.13625 0.6281 0.21245 0.18133 INSTANT 0.344754000E+00 TIME STEP NUMBER 358 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.59002E-06 0.27203E-02 Friction velocity uk : 0.70687E-06 0.27202E-02 Dimensionless distance yplus : 0.47074E-05 0.18098E-01 Friction thermal sca. tstar : -0.27462E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.33062E-05 0.12711E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.59002E-06 0.27203E-02 Friction velocity uk : 0.70687E-06 0.27202E-02 Dimensionless distance yplus : 0.47074E-05 0.18098E-01 Friction thermal sca. tstar : -0.27462E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.33062E-05 0.12711E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.36027E-08 3 0.36554E-06 0.92037E-12 0.17662E+01 c Velocity[X] 0.72926E-31 c Velocity[Y] 0.46018E-12 c Velocity[Z] 0.46019E-12 c Pressure 0.24936E-13 20 0.75236E-08 0.19587E-06 0.22909E+01 c k 0.67365E-06 2 0.10010E-06 0.24613E-07 0.25384E+01 c omega 0.13153E+02 1 0.48925E-08 0.23808E+01 0.80328E-02 c TempK 0.94448E+02 1 0.25927E-06 0.62578E-01 0.27786E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.358e-13 1.1198e-13 -1.3664e-17 -3.4729e-18 v Velocity[Y] -0.00015597 0.00015318 -1.0645e-09 -4.9229e-12 v Velocity[Z] -0.00015318 0.00015597 9.4805e-10 -1.8731e-12 v ǁVelocityǁ 1.2373e-10 0.00017092 1.0707e-05 5.8843e-06 v Pressure -0.00060303 0.015255 0.00077425 5.0203e-20 v k 5.4121e-09 0.0022269 0.0015661 0.0019226 v omega 25.281 1.0313e+05 2673.9 509.07 v TempK 288 341.67 292.76 290.03 v Density 1.205 1.205 1.205 1.205 v TurbVisc 6.3672e-14 0.00010085 6.805e-05 8.6611e-05 v CourantNb 1.4218e-09 0.00027417 1.548e-05 7.8685e-06 v FourierNb 0.13615 0.6281 0.21233 0.18124 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9169 4.917 0.00042595 -3.674e-07 v volume_forces[Z] -4.9169 4.917 -0.00042581 4.4835e-07 v ǁvolume_forcesǁ 4.409e-09 4.9186 0.43258 0.18303 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.98 290.17 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.018098 6.2652e-05 3.5408e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.13615 0.6281 0.21235 0.18125 INSTANT 0.345717000E+00 TIME STEP NUMBER 359 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10088E-05 0.27183E-02 Friction velocity uk : 0.10842E-05 0.27182E-02 Dimensionless distance yplus : 0.72202E-05 0.18084E-01 Friction thermal sca. tstar : -0.29879E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.50710E-05 0.12701E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10088E-05 0.27183E-02 Friction velocity uk : 0.10842E-05 0.27182E-02 Dimensionless distance yplus : 0.72202E-05 0.18084E-01 Friction thermal sca. tstar : -0.29879E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.50710E-05 0.12701E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.35995E-08 3 0.36404E-06 0.91069E-12 0.17587E+01 c Velocity[X] 0.72086E-31 c Velocity[Y] 0.45534E-12 c Velocity[Z] 0.45535E-12 c Pressure 0.24819E-13 20 0.74916E-08 0.19495E-06 0.22843E+01 c k 0.67206E-06 2 0.99689E-07 0.24396E-07 0.25332E+01 c omega 0.13153E+02 1 0.48691E-08 0.23617E+01 0.80005E-02 c TempK 0.94448E+02 1 0.25828E-06 0.62323E-01 0.27729E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.356e-13 1.1182e-13 -1.3647e-17 -3.4689e-18 v Velocity[Y] -0.0001558 0.000153 -1.0653e-09 -4.9085e-12 v Velocity[Z] -0.000153 0.00015581 9.4832e-10 -1.8761e-12 v ǁVelocityǁ 1.2564e-10 0.00017067 1.07e-05 5.8837e-06 v Pressure -0.00060474 0.015276 0.00077574 3.1965e-20 v k 5.3752e-09 0.0022212 0.001562 0.0019179 v omega 25.231 1.0313e+05 2673.8 509.03 v TempK 288 341.67 292.77 290.03 v Density 1.205 1.205 1.205 1.205 v TurbVisc 6.3237e-14 0.00010081 6.801e-05 8.657e-05 v CourantNb 1.4259e-09 0.00027377 1.5463e-05 7.8629e-06 v FourierNb 0.13605 0.6281 0.21223 0.18116 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9171 4.9171 0.00042633 -3.6811e-07 v volume_forces[Z] -4.9171 4.9171 -0.00042619 4.4916e-07 v ǁvolume_forcesǁ 4.4727e-09 4.9187 0.43296 0.18329 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.99 290.17 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.018084 6.2613e-05 3.5385e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.13605 0.6281 0.21225 0.18116 INSTANT 0.346680000E+00 TIME STEP NUMBER 360 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.13021E-05 0.27163E-02 Friction velocity uk : 0.13615E-05 0.27162E-02 Dimensionless distance yplus : 0.90671E-05 0.18071E-01 Friction thermal sca. tstar : -0.33075E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.63682E-05 0.12692E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.13021E-05 0.27163E-02 Friction velocity uk : 0.13615E-05 0.27162E-02 Dimensionless distance yplus : 0.90671E-05 0.18071E-01 Friction thermal sca. tstar : -0.33075E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.63682E-05 0.12692E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.35963E-08 3 0.36251E-06 0.90117E-12 0.17512E+01 c Velocity[X] 0.71260E-31 c Velocity[Y] 0.45058E-12 c Velocity[Z] 0.45059E-12 c Pressure 0.24665E-13 20 0.74631E-08 0.19374E-06 0.22777E+01 c k 0.67048E-06 2 0.99282E-07 0.24181E-07 0.25281E+01 c omega 0.13153E+02 1 0.48459E-08 0.23427E+01 0.79683E-02 c TempK 0.94449E+02 1 0.25730E-06 0.62069E-01 0.27672E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.354e-13 1.1166e-13 -1.363e-17 -3.4648e-18 v Velocity[Y] -0.00015563 0.00015282 -1.066e-09 -4.894e-12 v Velocity[Z] -0.00015281 0.00015564 9.4857e-10 -1.8792e-12 v ǁVelocityǁ 1.2771e-10 0.00017043 1.0692e-05 5.8832e-06 v Pressure -0.00060645 0.015298 0.00077722 5.5302e-20 v k 5.3385e-09 0.0022155 0.001558 0.0019132 v omega 25.18 1.0313e+05 2673.8 508.98 v TempK 288 341.67 292.77 290.03 v Density 1.205 1.205 1.205 1.205 v TurbVisc 6.2805e-14 0.00010076 6.7971e-05 8.6528e-05 v CourantNb 1.43e-09 0.00027338 1.5447e-05 7.8574e-06 v FourierNb 0.13594 0.6281 0.21213 0.18107 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9172 4.9173 0.00042671 -3.6881e-07 v volume_forces[Z] -4.9172 4.9173 -0.00042657 4.4996e-07 v ǁvolume_forcesǁ 4.542e-09 4.9189 0.43334 0.18355 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 292.99 290.18 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.018071 6.2574e-05 3.5362e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.13594 0.6281 0.21214 0.18108 INSTANT 0.347643000E+00 TIME STEP NUMBER 361 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15417E-05 0.27144E-02 Friction velocity uk : 0.15920E-05 0.27142E-02 Dimensionless distance yplus : 0.10602E-04 0.18058E-01 Friction thermal sca. tstar : -0.37580E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.74460E-05 0.12683E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15417E-05 0.27144E-02 Friction velocity uk : 0.15920E-05 0.27142E-02 Dimensionless distance yplus : 0.10602E-04 0.18058E-01 Friction thermal sca. tstar : -0.37580E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.74460E-05 0.12683E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.35931E-08 3 0.36102E-06 0.89181E-12 0.17439E+01 c Velocity[X] 0.70447E-31 c Velocity[Y] 0.44590E-12 c Velocity[Z] 0.44591E-12 c Pressure 0.24533E-13 20 0.74337E-08 0.19269E-06 0.22712E+01 c k 0.66890E-06 2 0.98878E-07 0.23969E-07 0.25230E+01 c omega 0.13153E+02 1 0.48228E-08 0.23240E+01 0.79364E-02 c TempK 0.94450E+02 1 0.25632E-06 0.61818E-01 0.27616E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.352e-13 1.1149e-13 -1.3613e-17 -3.4608e-18 v Velocity[Y] -0.00015547 0.00015263 -1.0668e-09 -4.8798e-12 v Velocity[Z] -0.00015263 0.00015547 9.4881e-10 -1.8823e-12 v ǁVelocityǁ 1.2993e-10 0.00017018 1.0685e-05 5.8828e-06 v Pressure -0.00060816 0.015319 0.0007787 5.0497e-20 v k 5.3023e-09 0.0022098 0.001554 0.0019085 v omega 25.13 1.0313e+05 2673.8 508.94 v TempK 288 341.67 292.78 290.04 v Density 1.205 1.205 1.205 1.205 v TurbVisc 6.2377e-14 0.00010071 6.7931e-05 8.6487e-05 v CourantNb 1.4341e-09 0.00027299 1.5431e-05 7.852e-06 v FourierNb 0.13584 0.6281 0.21203 0.18098 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9174 4.9174 0.00042709 -3.6952e-07 v volume_forces[Z] -4.9174 4.9174 -0.00042695 4.5077e-07 v ǁvolume_forcesǁ 4.6168e-09 4.9191 0.43372 0.1838 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293 290.18 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.018058 6.2536e-05 3.5339e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.13584 0.6281 0.21204 0.18099 INSTANT 0.348606000E+00 TIME STEP NUMBER 362 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.17496E-05 0.27124E-02 Friction velocity uk : 0.17937E-05 0.27123E-02 Dimensionless distance yplus : 0.11945E-04 0.18045E-01 Friction thermal sca. tstar : -0.44633E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.83897E-05 0.12674E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.17496E-05 0.27124E-02 Friction velocity uk : 0.17937E-05 0.27123E-02 Dimensionless distance yplus : 0.11945E-04 0.18045E-01 Friction thermal sca. tstar : -0.44633E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.83897E-05 0.12674E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.35900E-08 3 0.35953E-06 0.88260E-12 0.17366E+01 c Velocity[X] 0.69647E-31 c Velocity[Y] 0.44130E-12 c Velocity[Z] 0.44131E-12 c Pressure 0.24403E-13 20 0.74039E-08 0.19166E-06 0.22647E+01 c k 0.66733E-06 2 0.98477E-07 0.23759E-07 0.25179E+01 c omega 0.13153E+02 1 0.47999E-08 0.23054E+01 0.79046E-02 c TempK 0.94450E+02 1 0.25536E-06 0.61568E-01 0.27559E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.35e-13 1.1133e-13 -1.3596e-17 -3.4567e-18 v Velocity[Y] -0.0001553 0.00015246 -1.0676e-09 -4.8655e-12 v Velocity[Z] -0.00015246 0.00015531 9.4905e-10 -1.8854e-12 v ǁVelocityǁ 1.3228e-10 0.00016994 1.0677e-05 5.8824e-06 v Pressure -0.00060987 0.015341 0.00078018 1.5836e-20 v k 5.2663e-09 0.0022041 0.00155 0.0019039 v omega 25.08 1.0313e+05 2673.7 508.89 v TempK 288 341.67 292.78 290.04 v Density 1.205 1.205 1.205 1.205 v TurbVisc 6.1953e-14 0.00010067 6.7891e-05 8.6446e-05 v CourantNb 1.4382e-09 0.0002726 1.5415e-05 7.8467e-06 v FourierNb 0.13574 0.6281 0.21192 0.1809 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9176 4.9176 0.00042747 -3.7022e-07 v volume_forces[Z] -4.9176 4.9176 -0.00042733 4.5157e-07 v ǁvolume_forcesǁ 4.6969e-09 4.9192 0.4341 0.18406 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293 290.18 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.018045 6.2497e-05 3.5316e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.13574 0.6281 0.21194 0.18091 INSTANT 0.349569000E+00 TIME STEP NUMBER 363 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19359E-05 0.27104E-02 Friction velocity uk : 0.19756E-05 0.27103E-02 Dimensionless distance yplus : 0.13157E-04 0.18032E-01 Friction thermal sca. tstar : -0.58142E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.92403E-05 0.12664E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19359E-05 0.27104E-02 Friction velocity uk : 0.19756E-05 0.27103E-02 Dimensionless distance yplus : 0.13157E-04 0.18032E-01 Friction thermal sca. tstar : -0.58142E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.92403E-05 0.12664E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.35869E-08 3 0.35808E-06 0.87355E-12 0.17293E+01 c Velocity[X] 0.68859E-31 c Velocity[Y] 0.43677E-12 c Velocity[Z] 0.43678E-12 c Pressure 0.24286E-13 20 0.73774E-08 0.19073E-06 0.22582E+01 c k 0.66577E-06 2 0.98080E-07 0.23551E-07 0.25128E+01 c omega 0.13153E+02 1 0.47771E-08 0.22870E+01 0.78730E-02 c TempK 0.94451E+02 1 0.25439E-06 0.61320E-01 0.27503E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.3481e-13 1.1117e-13 -1.358e-17 -3.4527e-18 v Velocity[Y] -0.00015514 0.00015228 -1.0683e-09 -4.8513e-12 v Velocity[Z] -0.00015228 0.00015514 9.4927e-10 -1.8883e-12 v ǁVelocityǁ 1.3477e-10 0.00016969 1.067e-05 5.8821e-06 v Pressure -0.00061158 0.015362 0.00078166 3.5642e-20 v k 5.2307e-09 0.0021985 0.001546 0.0018993 v omega 25.031 1.0313e+05 2673.7 508.85 v TempK 288 341.68 292.78 290.04 v Density 1.205 1.205 1.205 1.205 v TurbVisc 6.1533e-14 0.00010063 6.7852e-05 8.6405e-05 v CourantNb 1.4423e-09 0.00027221 1.5399e-05 7.8414e-06 v FourierNb 0.13564 0.6281 0.21182 0.18081 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9177 4.9178 0.00042785 -3.7091e-07 v volume_forces[Z] -4.9177 4.9178 -0.00042771 4.5237e-07 v ǁvolume_forcesǁ 4.7819e-09 4.9194 0.43448 0.18432 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293 290.19 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.018032 6.2459e-05 3.5293e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.13564 0.6281 0.21184 0.18082 INSTANT 0.350532000E+00 TIME STEP NUMBER 364 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.21065E-05 0.27085E-02 Friction velocity uk : 0.21426E-05 0.27083E-02 Dimensionless distance yplus : 0.14269E-04 0.18019E-01 Friction thermal sca. tstar : -0.10566E+05 0.00000E+00 Dim-less thermal sca. tplus : 0.10022E-04 0.12655E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.21065E-05 0.27085E-02 Friction velocity uk : 0.21426E-05 0.27083E-02 Dimensionless distance yplus : 0.14269E-04 0.18019E-01 Friction thermal sca. tstar : -0.10566E+05 0.00000E+00 Dim-less thermal sca. tplus : 0.10022E-04 0.12655E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.35839E-08 3 0.35660E-06 0.86464E-12 0.17221E+01 c Velocity[X] 0.68085E-31 c Velocity[Y] 0.43232E-12 c Velocity[Z] 0.43233E-12 c Pressure 0.24152E-13 20 0.73465E-08 0.18967E-06 0.22518E+01 c k 0.66422E-06 2 0.97686E-07 0.23346E-07 0.25078E+01 c omega 0.13153E+02 1 0.47545E-08 0.22688E+01 0.78417E-02 c TempK 0.94452E+02 1 0.25343E-06 0.61073E-01 0.27448E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.3461e-13 1.1102e-13 -1.3563e-17 -3.4487e-18 v Velocity[Y] -0.00015498 0.0001521 -1.069e-09 -4.8371e-12 v Velocity[Z] -0.0001521 0.00015498 9.4948e-10 -1.8914e-12 v ǁVelocityǁ 1.3738e-10 0.00016945 1.0663e-05 5.8818e-06 v Pressure -0.0006133 0.015384 0.00078313 -9.6092e-21 v k 5.1954e-09 0.0021929 0.001542 0.0018947 v omega 24.981 1.0313e+05 2673.6 508.8 v TempK 288 341.68 292.79 290.04 v Density 1.205 1.205 1.205 1.205 v TurbVisc 6.1117e-14 0.00010061 6.7812e-05 8.6364e-05 v CourantNb 1.4464e-09 0.00027183 1.5384e-05 7.8363e-06 v FourierNb 0.13553 0.6281 0.21172 0.18073 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9179 4.9179 0.00042823 -3.7161e-07 v volume_forces[Z] -4.9179 4.9179 -0.00042809 4.5316e-07 v ǁvolume_forcesǁ 4.8719e-09 4.9195 0.43486 0.18458 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.01 290.19 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.018019 6.242e-05 3.5269e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.13554 0.6281 0.21174 0.18074 INSTANT 0.351495000E+00 TIME STEP NUMBER 365 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.22647E-05 0.27065E-02 Friction velocity uk : 0.22981E-05 0.27064E-02 Dimensionless distance yplus : 0.15304E-04 0.18006E-01 Friction thermal sca. tstar : -0.20159E+05 0.00000E+00 Dim-less thermal sca. tplus : 0.10749E-04 0.12646E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.22647E-05 0.27065E-02 Friction velocity uk : 0.22981E-05 0.27064E-02 Dimensionless distance yplus : 0.15304E-04 0.18006E-01 Friction thermal sca. tstar : -0.20159E+05 0.00000E+00 Dim-less thermal sca. tplus : 0.10749E-04 0.12646E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.35809E-08 3 0.35514E-06 0.85589E-12 0.17151E+01 c Velocity[X] 0.67322E-31 c Velocity[Y] 0.42794E-12 c Velocity[Z] 0.42795E-12 c Pressure 0.24017E-13 20 0.73182E-08 0.18860E-06 0.22454E+01 c k 0.66267E-06 2 0.97295E-07 0.23142E-07 0.25028E+01 c omega 0.13153E+02 1 0.47321E-08 0.22508E+01 0.78104E-02 c TempK 0.94452E+02 1 0.25248E-06 0.60828E-01 0.27392E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.3442e-13 1.1086e-13 -1.3547e-17 -3.4448e-18 v Velocity[Y] -0.00015481 0.00015193 -1.0697e-09 -4.8229e-12 v Velocity[Z] -0.00015192 0.00015482 9.4967e-10 -1.8944e-12 v ǁVelocityǁ 1.4012e-10 0.00016921 1.0656e-05 5.8816e-06 v Pressure -0.00061501 0.015405 0.00078461 1.0546e-19 v k 5.1605e-09 0.0021873 0.0015381 0.0018901 v omega 24.932 1.0313e+05 2673.6 508.76 v TempK 288 341.68 292.79 290.05 v Density 1.205 1.205 1.205 1.205 v TurbVisc 6.0705e-14 0.00010059 6.7773e-05 8.6323e-05 v CourantNb 1.4505e-09 0.00027145 1.5368e-05 7.8313e-06 v FourierNb 0.13543 0.6281 0.21162 0.18065 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.918 4.9181 0.00042861 -3.723e-07 v volume_forces[Z] -4.918 4.9181 -0.00042846 4.5395e-07 v ǁvolume_forcesǁ 4.9664e-09 4.9197 0.43524 0.18483 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.01 290.19 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.018006 6.2382e-05 3.5247e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.13543 0.6281 0.21164 0.18065 INSTANT 0.352458000E+00 TIME STEP NUMBER 366 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.24131E-05 0.27046E-02 Friction velocity uk : 0.24441E-05 0.27045E-02 Dimensionless distance yplus : 0.16277E-04 0.17993E-01 Friction thermal sca. tstar : -0.65838E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.11432E-04 0.12637E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.24131E-05 0.27046E-02 Friction velocity uk : 0.24441E-05 0.27045E-02 Dimensionless distance yplus : 0.16277E-04 0.17993E-01 Friction thermal sca. tstar : -0.65838E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.11432E-04 0.12637E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.35780E-08 3 0.35371E-06 0.84728E-12 0.17080E+01 c Velocity[X] 0.66572E-31 c Velocity[Y] 0.42363E-12 c Velocity[Z] 0.42364E-12 c Pressure 0.23895E-13 20 0.72898E-08 0.18764E-06 0.22391E+01 c k 0.66113E-06 2 0.96907E-07 0.22941E-07 0.24978E+01 c omega 0.13153E+02 1 0.47098E-08 0.22330E+01 0.77794E-02 c TempK 0.94453E+02 1 0.25154E-06 0.60585E-01 0.27337E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.3423e-13 1.107e-13 -1.353e-17 -3.4408e-18 v Velocity[Y] -0.00015465 0.00015175 -1.0704e-09 -4.8088e-12 v Velocity[Z] -0.00015175 0.00015466 9.4986e-10 -1.8973e-12 v ǁVelocityǁ 1.4287e-10 0.00016897 1.0649e-05 5.8815e-06 v Pressure -0.00061672 0.015426 0.00078608 3.6181e-20 v k 5.1258e-09 0.0021818 0.0015341 0.0018855 v omega 24.883 1.0313e+05 2673.6 508.71 v TempK 288 341.68 292.8 290.05 v Density 1.205 1.205 1.205 1.205 v TurbVisc 6.0296e-14 0.00010057 6.7734e-05 8.6282e-05 v CourantNb 1.4545e-09 0.00027107 1.5353e-05 7.8263e-06 v FourierNb 0.13533 0.6281 0.21152 0.18056 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9182 4.9182 0.00042898 -3.7299e-07 v volume_forces[Z] -4.9182 4.9182 -0.00042884 4.5475e-07 v ǁvolume_forcesǁ 5.0654e-09 4.9198 0.43562 0.18509 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.02 290.19 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.017993 6.2347e-05 3.5226e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.13533 0.6281 0.21154 0.18057 INSTANT 0.353421000E+00 TIME STEP NUMBER 367 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.25533E-05 0.27026E-02 Friction velocity uk : 0.25824E-05 0.27025E-02 Dimensionless distance yplus : 0.17198E-04 0.17980E-01 Friction thermal sca. tstar : -0.47845E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.12079E-04 0.12628E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.25533E-05 0.27026E-02 Friction velocity uk : 0.25824E-05 0.27025E-02 Dimensionless distance yplus : 0.17198E-04 0.17980E-01 Friction thermal sca. tstar : -0.47845E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.12079E-04 0.12628E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.35750E-08 3 0.35301E-06 0.83881E-12 0.17011E+01 c Velocity[X] 0.65833E-31 c Velocity[Y] 0.41940E-12 c Velocity[Z] 0.41941E-12 c Pressure 0.23773E-13 20 0.72617E-08 0.18667E-06 0.22328E+01 c k 0.65959E-06 2 0.96522E-07 0.22742E-07 0.24928E+01 c omega 0.13153E+02 1 0.46876E-08 0.22153E+01 0.77486E-02 c TempK 0.94454E+02 1 0.25060E-06 0.60343E-01 0.27282E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.3404e-13 1.1054e-13 -1.3514e-17 -3.4369e-18 v Velocity[Y] -0.00015449 0.00015158 -1.0711e-09 -4.7949e-12 v Velocity[Z] -0.00015158 0.0001545 9.5003e-10 -1.9e-12 v ǁVelocityǁ 1.4491e-10 0.00016874 1.0642e-05 5.8815e-06 v Pressure -0.00061843 0.015448 0.00078755 4.0055e-20 v k 5.0915e-09 0.0021763 0.0015302 0.001881 v omega 24.834 1.0313e+05 2673.5 508.67 v TempK 288 341.68 292.8 290.05 v Density 1.205 1.205 1.205 1.205 v TurbVisc 5.9891e-14 0.00010055 6.7695e-05 8.6242e-05 v CourantNb 1.4586e-09 0.00027069 1.5338e-05 7.8214e-06 v FourierNb 0.13523 0.6281 0.21142 0.18048 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9183 4.9184 0.00042936 -3.7368e-07 v volume_forces[Z] -4.9183 4.9184 -0.00042921 4.5553e-07 v ǁvolume_forcesǁ 5.1647e-09 4.92 0.43599 0.18534 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.02 290.2 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.01798 6.2312e-05 3.5204e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.13523 0.6281 0.21144 0.18049 INSTANT 0.354384000E+00 TIME STEP NUMBER 368 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.26867E-05 0.27007E-02 Friction velocity uk : 0.27141E-05 0.27006E-02 Dimensionless distance yplus : 0.18075E-04 0.17967E-01 Friction thermal sca. tstar : -0.39435E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.12694E-04 0.12619E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.26867E-05 0.27007E-02 Friction velocity uk : 0.27141E-05 0.27006E-02 Dimensionless distance yplus : 0.18075E-04 0.17967E-01 Friction thermal sca. tstar : -0.39435E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.12694E-04 0.12619E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.35722E-08 3 0.35090E-06 0.83049E-12 0.16942E+01 c Velocity[X] 0.65107E-31 c Velocity[Y] 0.41524E-12 c Velocity[Z] 0.41525E-12 c Pressure 0.23650E-13 20 0.72354E-08 0.18569E-06 0.22265E+01 c k 0.65806E-06 2 0.96140E-07 0.22545E-07 0.24878E+01 c omega 0.13153E+02 1 0.46656E-08 0.21978E+01 0.77179E-02 c TempK 0.94454E+02 1 0.24966E-06 0.60103E-01 0.27228E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.3385e-13 1.1039e-13 -1.3497e-17 -3.433e-18 v Velocity[Y] -0.00015433 0.00015141 -1.0718e-09 -4.7809e-12 v Velocity[Z] -0.0001514 0.00015434 9.5019e-10 -1.903e-12 v ǁVelocityǁ 1.4701e-10 0.0001685 1.0635e-05 5.8815e-06 v Pressure -0.00062014 0.015469 0.00078901 3.4956e-20 v k 5.0574e-09 0.0021707 0.0015263 0.0018765 v omega 24.786 1.0313e+05 2673.5 508.62 v TempK 288 341.68 292.8 290.06 v Density 1.205 1.205 1.205 1.205 v TurbVisc 5.949e-14 0.00010053 6.7656e-05 8.6201e-05 v CourantNb 1.4627e-09 0.00027032 1.5323e-05 7.8166e-06 v FourierNb 0.13513 0.6281 0.21132 0.18039 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9185 4.9185 0.00042973 -3.7437e-07 v volume_forces[Z] -4.9185 4.9185 -0.00042959 4.5632e-07 v ǁvolume_forcesǁ 5.2386e-09 4.9201 0.43637 0.1856 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.02 290.2 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.017967 6.2276e-05 3.5183e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.13513 0.6281 0.21134 0.1804 INSTANT 0.355347000E+00 TIME STEP NUMBER 369 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.28142E-05 0.26988E-02 Friction velocity uk : 0.28401E-05 0.26987E-02 Dimensionless distance yplus : 0.18914E-04 0.17955E-01 Friction thermal sca. tstar : -0.34314E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.13284E-04 0.12610E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.28142E-05 0.26988E-02 Friction velocity uk : 0.28401E-05 0.26987E-02 Dimensionless distance yplus : 0.18914E-04 0.17955E-01 Friction thermal sca. tstar : -0.34314E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.13284E-04 0.12610E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.35693E-08 3 0.36514E-06 0.82230E-12 0.16874E+01 c Velocity[X] 0.64391E-31 c Velocity[Y] 0.41115E-12 c Velocity[Z] 0.41116E-12 c Pressure 0.23532E-13 20 0.72083E-08 0.18476E-06 0.22202E+01 c k 0.65654E-06 2 0.95761E-07 0.22350E-07 0.24829E+01 c omega 0.13153E+02 1 0.46437E-08 0.21805E+01 0.76875E-02 c TempK 0.94455E+02 1 0.24874E-06 0.59864E-01 0.27173E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.3366e-13 1.1024e-13 -1.3481e-17 -3.4291e-18 v Velocity[Y] -0.00015418 0.00015123 -1.0725e-09 -4.7672e-12 v Velocity[Z] -0.00015123 0.00015418 9.5034e-10 -1.906e-12 v ǁVelocityǁ 1.4916e-10 0.00016827 1.0629e-05 5.8815e-06 v Pressure -0.00062185 0.01549 0.00079048 4.6085e-20 v k 5.0237e-09 0.0021653 0.0015224 0.001872 v omega 24.737 1.0313e+05 2673.5 508.58 v TempK 288 341.69 292.81 290.06 v Density 1.205 1.205 1.205 1.205 v TurbVisc 5.9092e-14 0.00010051 6.7617e-05 8.6161e-05 v CourantNb 1.4668e-09 0.00026994 1.5308e-05 7.8119e-06 v FourierNb 0.13503 0.6281 0.21122 0.18031 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9186 4.9187 0.00043011 -3.7505e-07 v volume_forces[Z] -4.9186 4.9187 -0.00042996 4.571e-07 v ǁvolume_forcesǁ 5.3144e-09 4.9203 0.43674 0.18586 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.03 290.2 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.017955 6.224e-05 3.5162e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.13503 0.6281 0.21124 0.18032 INSTANT 0.356310000E+00 TIME STEP NUMBER 370 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.29366E-05 0.26969E-02 Friction velocity uk : 0.29612E-05 0.26968E-02 Dimensionless distance yplus : 0.19720E-04 0.17942E-01 Friction thermal sca. tstar : -0.30780E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.13850E-04 0.12601E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.29366E-05 0.26969E-02 Friction velocity uk : 0.29612E-05 0.26968E-02 Dimensionless distance yplus : 0.19720E-04 0.17942E-01 Friction thermal sca. tstar : -0.30780E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.13850E-04 0.12601E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.35665E-08 3 0.34804E-06 0.81426E-12 0.16807E+01 c Velocity[X] 0.63686E-31 c Velocity[Y] 0.40712E-12 c Velocity[Z] 0.40713E-12 c Pressure 0.23405E-13 20 0.71811E-08 0.18376E-06 0.22140E+01 c k 0.65503E-06 2 0.95385E-07 0.22158E-07 0.24779E+01 c omega 0.13153E+02 1 0.46220E-08 0.21633E+01 0.76572E-02 c TempK 0.94456E+02 1 0.24781E-06 0.59627E-01 0.27119E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.3347e-13 1.1008e-13 -1.3465e-17 -3.4252e-18 v Velocity[Y] -0.00015402 0.00015106 -1.0731e-09 -4.7532e-12 v Velocity[Z] -0.00015106 0.00015402 9.5048e-10 -1.9089e-12 v ǁVelocityǁ 1.5135e-10 0.00016803 1.0622e-05 5.8817e-06 v Pressure -0.00062356 0.015512 0.00079194 -4.231e-20 v k 4.9903e-09 0.0021598 0.0015186 0.0018675 v omega 24.689 1.0313e+05 2673.4 508.53 v TempK 288 341.69 292.81 290.06 v Density 1.205 1.205 1.205 1.205 v TurbVisc 5.8698e-14 0.00010049 6.7578e-05 8.612e-05 v CourantNb 1.4709e-09 0.00026957 1.5293e-05 7.8073e-06 v FourierNb 0.13492 0.6281 0.21112 0.18023 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9188 4.9188 0.00043048 -3.7573e-07 v volume_forces[Z] -4.9188 4.9188 -0.00043033 4.5788e-07 v ǁvolume_forcesǁ 5.392e-09 4.9204 0.43712 0.18611 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.03 290.21 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.017942 6.2205e-05 3.514e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.13493 0.6281 0.21114 0.18023 INSTANT 0.357273000E+00 TIME STEP NUMBER 371 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.30544E-05 0.26950E-02 Friction velocity uk : 0.30778E-05 0.26949E-02 Dimensionless distance yplus : 0.20497E-04 0.17929E-01 Friction thermal sca. tstar : -0.28151E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.14396E-04 0.12592E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.30544E-05 0.26950E-02 Friction velocity uk : 0.30778E-05 0.26949E-02 Dimensionless distance yplus : 0.20497E-04 0.17929E-01 Friction thermal sca. tstar : -0.28151E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.14396E-04 0.12592E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.35638E-08 3 0.34670E-06 0.80635E-12 0.16740E+01 c Velocity[X] 0.62992E-31 c Velocity[Y] 0.40317E-12 c Velocity[Z] 0.40318E-12 c Pressure 0.23348E-13 20 0.71635E-08 0.18330E-06 0.22078E+01 c k 0.65352E-06 2 0.95012E-07 0.21967E-07 0.24730E+01 c omega 0.13153E+02 1 0.46004E-08 0.21463E+01 0.76270E-02 c TempK 0.94456E+02 1 0.24690E-06 0.59392E-01 0.27065E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.3329e-13 1.0993e-13 -1.3449e-17 -3.4213e-18 v Velocity[Y] -0.00015386 0.00015089 -1.0738e-09 -4.7396e-12 v Velocity[Z] -0.00015089 0.00015387 9.5061e-10 -1.9119e-12 v ǁVelocityǁ 1.536e-10 0.0001678 1.0616e-05 5.8819e-06 v Pressure -0.00062527 0.015533 0.0007934 5.4223e-20 v k 4.9572e-09 0.0021543 0.0015147 0.001863 v omega 24.641 1.0313e+05 2673.4 508.49 v TempK 288 341.69 292.82 290.06 v Density 1.205 1.205 1.205 1.205 v TurbVisc 5.8308e-14 0.00010047 6.754e-05 8.608e-05 v CourantNb 1.475e-09 0.00026921 1.5278e-05 7.8028e-06 v FourierNb 0.13482 0.6281 0.21103 0.18014 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9189 4.919 0.00043085 -3.7642e-07 v volume_forces[Z] -4.9189 4.919 -0.00043071 4.5866e-07 v ǁvolume_forcesǁ 5.4714e-09 4.9206 0.43749 0.18636 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.04 290.21 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.017929 6.2169e-05 3.5119e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.13482 0.6281 0.21104 0.18015 INSTANT 0.358236000E+00 TIME STEP NUMBER 372 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.31683E-05 0.26931E-02 Friction velocity uk : 0.31906E-05 0.26930E-02 Dimensionless distance yplus : 0.21248E-04 0.17917E-01 Friction thermal sca. tstar : -0.26097E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.14923E-04 0.12584E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.31683E-05 0.26931E-02 Friction velocity uk : 0.31906E-05 0.26930E-02 Dimensionless distance yplus : 0.21248E-04 0.17917E-01 Friction thermal sca. tstar : -0.26097E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.14923E-04 0.12584E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.35611E-08 3 0.36099E-06 0.79857E-12 0.16674E+01 c Velocity[X] 0.62311E-31 c Velocity[Y] 0.39928E-12 c Velocity[Z] 0.39929E-12 c Pressure 0.23170E-13 20 0.71279E-08 0.18190E-06 0.22017E+01 c k 0.65201E-06 2 0.94642E-07 0.21778E-07 0.24682E+01 c omega 0.13153E+02 1 0.45789E-08 0.21295E+01 0.75971E-02 c TempK 0.94457E+02 1 0.24599E-06 0.59158E-01 0.27012E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.331e-13 1.0978e-13 -1.3433e-17 -3.4174e-18 v Velocity[Y] -0.00015371 0.00015073 -1.0744e-09 -4.7259e-12 v Velocity[Z] -0.00015072 0.00015371 9.5073e-10 -1.9148e-12 v ǁVelocityǁ 1.5589e-10 0.00016757 1.061e-05 5.8821e-06 v Pressure -0.00062698 0.015554 0.00079486 1.2011e-20 v k 4.9243e-09 0.0021489 0.0015109 0.0018586 v omega 24.593 1.0313e+05 2673.4 508.45 v TempK 288 341.69 292.82 290.07 v Density 1.205 1.205 1.205 1.205 v TurbVisc 5.7921e-14 0.00010045 6.7501e-05 8.604e-05 v CourantNb 1.4791e-09 0.00026884 1.5264e-05 7.7983e-06 v FourierNb 0.13472 0.6281 0.21093 0.18006 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9191 4.9191 0.00043122 -3.7709e-07 v volume_forces[Z] -4.9191 4.9191 -0.00043108 4.5944e-07 v ǁvolume_forcesǁ 5.5525e-09 4.9207 0.43786 0.18662 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.04 290.21 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.017917 6.2134e-05 3.5098e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.13472 0.6281 0.21094 0.18007 INSTANT 0.359199000E+00 TIME STEP NUMBER 373 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.32785E-05 0.26913E-02 Friction velocity uk : 0.32999E-05 0.26912E-02 Dimensionless distance yplus : 0.21976E-04 0.17904E-01 Friction thermal sca. tstar : -0.24436E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.15434E-04 0.12575E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.32785E-05 0.26913E-02 Friction velocity uk : 0.32999E-05 0.26912E-02 Dimensionless distance yplus : 0.21976E-04 0.17904E-01 Friction thermal sca. tstar : -0.24436E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.15434E-04 0.12575E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.35584E-08 3 0.35968E-06 0.79093E-12 0.16609E+01 c Velocity[X] 0.61638E-31 c Velocity[Y] 0.39546E-12 c Velocity[Z] 0.39547E-12 c Pressure 0.23127E-13 20 0.71083E-08 0.18155E-06 0.21956E+01 c k 0.65052E-06 2 0.94274E-07 0.21592E-07 0.24633E+01 c omega 0.13153E+02 1 0.45576E-08 0.21129E+01 0.75673E-02 c TempK 0.94458E+02 1 0.24508E-06 0.58925E-01 0.26958E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.3291e-13 1.0963e-13 -1.3417e-17 -3.4136e-18 v Velocity[Y] -0.00015355 0.00015056 -1.075e-09 -4.7129e-12 v Velocity[Z] -0.00015056 0.00015356 9.5083e-10 -1.9177e-12 v ǁVelocityǁ 1.5823e-10 0.00016735 1.0603e-05 5.8825e-06 v Pressure -0.00062869 0.015575 0.00079632 4.8438e-20 v k 4.8918e-09 0.0021435 0.0015071 0.0018542 v omega 24.545 1.0313e+05 2673.3 508.4 v TempK 288 341.69 292.83 290.07 v Density 1.205 1.205 1.205 1.205 v TurbVisc 5.7537e-14 0.00010043 6.7463e-05 8.5999e-05 v CourantNb 1.4832e-09 0.00026848 1.525e-05 7.7939e-06 v FourierNb 0.13462 0.6281 0.21083 0.17998 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9192 4.9193 0.00043159 -3.7777e-07 v volume_forces[Z] -4.9192 4.9193 -0.00043145 4.6021e-07 v ǁvolume_forcesǁ 5.6354e-09 4.9209 0.43824 0.18687 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.05 290.21 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.017904 6.2099e-05 3.5077e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.13462 0.6281 0.21084 0.17999 INSTANT 0.360162000E+00 TIME STEP NUMBER 374 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+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-05 0.26894E-02 Friction velocity uk : 0.34060E-05 0.26893E-02 Dimensionless distance yplus : 0.22683E-04 0.17892E-01 Friction thermal sca. tstar : -0.23056E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.15931E-04 0.12566E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+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-05 0.26894E-02 Friction velocity uk : 0.34060E-05 0.26893E-02 Dimensionless distance yplus : 0.22683E-04 0.17892E-01 Friction thermal sca. tstar : -0.23056E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.15931E-04 0.12566E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.35557E-08 3 0.34256E-06 0.78341E-12 0.16544E+01 c Velocity[X] 0.60978E-31 c Velocity[Y] 0.39170E-12 c Velocity[Z] 0.39171E-12 c Pressure 0.22945E-13 20 0.70784E-08 0.18012E-06 0.21895E+01 c k 0.64903E-06 2 0.93909E-07 0.21407E-07 0.24584E+01 c omega 0.13153E+02 1 0.45364E-08 0.20964E+01 0.75377E-02 c TempK 0.94459E+02 1 0.24418E-06 0.58695E-01 0.26905E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.3273e-13 1.0948e-13 -1.3401e-17 -3.4098e-18 v Velocity[Y] -0.0001534 0.00015039 -1.0757e-09 -4.699e-12 v Velocity[Z] -0.00015039 0.0001534 9.5092e-10 -1.9208e-12 v ǁVelocityǁ 1.6061e-10 0.00016712 1.0597e-05 5.8828e-06 v Pressure -0.0006304 0.015596 0.00079778 4.4516e-20 v k 4.8595e-09 0.0021381 0.0015033 0.0018498 v omega 24.498 1.0313e+05 2673.3 508.36 v TempK 288 341.69 292.83 290.07 v Density 1.205 1.205 1.205 1.205 v TurbVisc 5.7157e-14 0.00010041 6.7424e-05 8.5959e-05 v CourantNb 1.4873e-09 0.00026812 1.5235e-05 7.7896e-06 v FourierNb 0.13452 0.6281 0.21073 0.1799 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9194 4.9194 0.00043196 -3.7844e-07 v volume_forces[Z] -4.9194 4.9194 -0.00043182 4.6098e-07 v ǁvolume_forcesǁ 5.7198e-09 4.921 0.43861 0.18713 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.05 290.22 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.017892 6.2063e-05 3.5056e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.13452 0.6281 0.21075 0.1799 INSTANT 0.361125000E+00 TIME STEP NUMBER 375 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.34896E-05 0.26876E-02 Friction velocity uk : 0.35093E-05 0.26874E-02 Dimensionless distance yplus : 0.23370E-04 0.17880E-01 Friction thermal sca. tstar : -0.21886E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.16414E-04 0.12558E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.34896E-05 0.26876E-02 Friction velocity uk : 0.35093E-05 0.26874E-02 Dimensionless distance yplus : 0.23370E-04 0.17880E-01 Friction thermal sca. tstar : -0.21886E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.16414E-04 0.12558E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.35531E-08 3 0.34120E-06 0.77602E-12 0.16480E+01 c Velocity[X] 0.60327E-31 c Velocity[Y] 0.38801E-12 c Velocity[Z] 0.38802E-12 c Pressure 0.22824E-13 20 0.70499E-08 0.17916E-06 0.21834E+01 c k 0.64754E-06 2 0.93547E-07 0.21224E-07 0.24536E+01 c omega 0.13153E+02 1 0.45154E-08 0.20800E+01 0.75083E-02 c TempK 0.94459E+02 1 0.24329E-06 0.58465E-01 0.26852E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.3255e-13 1.0933e-13 -1.3385e-17 -3.406e-18 v Velocity[Y] -0.00015325 0.00015023 -1.0763e-09 -4.6856e-12 v Velocity[Z] -0.00015023 0.00015325 9.5101e-10 -1.9238e-12 v ǁVelocityǁ 1.6303e-10 0.00016689 1.0591e-05 5.8833e-06 v Pressure -0.00063211 0.015617 0.00079923 -9.1238e-20 v k 4.8276e-09 0.0021328 0.0014995 0.0018454 v omega 24.45 1.0313e+05 2673.3 508.32 v TempK 288 341.7 292.83 290.08 v Density 1.205 1.205 1.205 1.205 v TurbVisc 5.678e-14 0.00010039 6.7386e-05 8.5919e-05 v CourantNb 1.4914e-09 0.00026776 1.5221e-05 7.7854e-06 v FourierNb 0.13442 0.6281 0.21064 0.17981 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9195 4.9196 0.00043233 -3.7912e-07 v volume_forces[Z] -4.9195 4.9196 -0.00043219 4.6175e-07 v ǁvolume_forcesǁ 5.806e-09 4.9212 0.43898 0.18738 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.05 290.22 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.01788 6.2028e-05 3.5035e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.13442 0.6281 0.21065 0.17982 INSTANT 0.362088000E+00 TIME STEP NUMBER 376 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.35910E-05 0.26857E-02 Friction velocity uk : 0.36099E-05 0.26856E-02 Dimensionless distance yplus : 0.24040E-04 0.17867E-01 Friction thermal sca. tstar : -0.20877E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.16884E-04 0.12549E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.35910E-05 0.26857E-02 Friction velocity uk : 0.36099E-05 0.26856E-02 Dimensionless distance yplus : 0.24040E-04 0.17867E-01 Friction thermal sca. tstar : -0.20877E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.16884E-04 0.12549E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.35506E-08 3 0.33987E-06 0.76876E-12 0.16417E+01 c Velocity[X] 0.59686E-31 c Velocity[Y] 0.38437E-12 c Velocity[Z] 0.38438E-12 c Pressure 0.22714E-13 20 0.70242E-08 0.17829E-06 0.21774E+01 c k 0.64607E-06 2 0.93188E-07 0.21044E-07 0.24488E+01 c omega 0.13153E+02 1 0.44945E-08 0.20638E+01 0.74790E-02 c TempK 0.94460E+02 1 0.24240E-06 0.58237E-01 0.26800E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.3237e-13 1.0919e-13 -1.3369e-17 -3.4022e-18 v Velocity[Y] -0.0001531 0.00015006 -1.0768e-09 -4.6722e-12 v Velocity[Z] -0.00015006 0.0001531 9.5108e-10 -1.9268e-12 v ǁVelocityǁ 1.655e-10 0.00016667 1.0585e-05 5.8838e-06 v Pressure -0.00063382 0.015638 0.00080068 3.1279e-20 v k 4.7959e-09 0.0021274 0.0014958 0.001841 v omega 24.403 1.0313e+05 2673.2 508.27 v TempK 288 341.7 292.84 290.08 v Density 1.205 1.205 1.205 1.205 v TurbVisc 5.6407e-14 0.00010038 6.7348e-05 8.588e-05 v CourantNb 1.4955e-09 0.0002674 1.5208e-05 7.7813e-06 v FourierNb 0.13432 0.6281 0.21054 0.17973 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9197 4.9197 0.0004327 -3.7979e-07 v volume_forces[Z] -4.9197 4.9197 -0.00043256 4.6251e-07 v ǁvolume_forcesǁ 5.8936e-09 4.9213 0.43935 0.18763 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.06 290.22 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.017867 6.1994e-05 3.5014e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.13432 0.6281 0.21055 0.17974 INSTANT 0.363051000E+00 TIME STEP NUMBER 377 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.36899E-05 0.26839E-02 Friction velocity uk : 0.37081E-05 0.26838E-02 Dimensionless distance yplus : 0.24694E-04 0.17855E-01 Friction thermal sca. tstar : -0.19994E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.17344E-04 0.12540E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.36899E-05 0.26839E-02 Friction velocity uk : 0.37081E-05 0.26838E-02 Dimensionless distance yplus : 0.24694E-04 0.17855E-01 Friction thermal sca. tstar : -0.19994E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.17344E-04 0.12540E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.35480E-08 3 0.33854E-06 0.76161E-12 0.16355E+01 c Velocity[X] 0.59056E-31 c Velocity[Y] 0.38080E-12 c Velocity[Z] 0.38081E-12 c Pressure 0.22598E-13 20 0.70018E-08 0.17737E-06 0.21714E+01 c k 0.64459E-06 2 0.92832E-07 0.20865E-07 0.24440E+01 c omega 0.13153E+02 1 0.44738E-08 0.20478E+01 0.74499E-02 c TempK 0.94461E+02 1 0.24151E-06 0.58011E-01 0.26747E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.3219e-13 1.0904e-13 -1.3353e-17 -3.3984e-18 v Velocity[Y] -0.00015295 0.0001499 -1.0774e-09 -4.659e-12 v Velocity[Z] -0.0001499 0.00015295 9.5114e-10 -1.9297e-12 v ǁVelocityǁ 1.68e-10 0.00016649 1.0579e-05 5.8843e-06 v Pressure -0.00063553 0.01566 0.00080213 1.7699e-20 v k 4.7645e-09 0.0021221 0.001492 0.0018367 v omega 24.356 1.0313e+05 2673.2 508.23 v TempK 288 341.7 292.84 290.08 v Density 1.205 1.205 1.205 1.205 v TurbVisc 5.6037e-14 0.00010036 6.731e-05 8.584e-05 v CourantNb 1.4996e-09 0.00026705 1.5194e-05 7.7773e-06 v FourierNb 0.13422 0.6281 0.21044 0.17965 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9198 4.9199 0.00043307 -3.8046e-07 v volume_forces[Z] -4.9198 4.9199 -0.00043292 4.6328e-07 v ǁvolume_forcesǁ 5.9827e-09 4.9214 0.43972 0.18788 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.06 290.23 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.017855 6.1959e-05 3.4993e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.13422 0.6281 0.21046 0.17966 INSTANT 0.364014000E+00 TIME STEP NUMBER 378 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.37865E-05 0.26820E-02 Friction velocity uk : 0.38041E-05 0.26819E-02 Dimensionless distance yplus : 0.25334E-04 0.17843E-01 Friction thermal sca. tstar : -0.19215E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.17793E-04 0.12532E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.37865E-05 0.26820E-02 Friction velocity uk : 0.38041E-05 0.26819E-02 Dimensionless distance yplus : 0.25334E-04 0.17843E-01 Friction thermal sca. tstar : -0.19215E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.17793E-04 0.12532E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.35455E-08 3 0.33722E-06 0.75459E-12 0.16293E+01 c Velocity[X] 0.58435E-31 c Velocity[Y] 0.37729E-12 c Velocity[Z] 0.37730E-12 c Pressure 0.22479E-13 20 0.69774E-08 0.17643E-06 0.21655E+01 c k 0.64313E-06 2 0.92478E-07 0.20688E-07 0.24393E+01 c omega 0.13153E+02 1 0.44531E-08 0.20319E+01 0.74210E-02 c TempK 0.94461E+02 1 0.24064E-06 0.57786E-01 0.26695E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.3201e-13 1.089e-13 -1.3338e-17 -3.3946e-18 v Velocity[Y] -0.0001528 0.00014974 -1.078e-09 -4.6457e-12 v Velocity[Z] -0.00014973 0.0001528 9.5119e-10 -1.9326e-12 v ǁVelocityǁ 1.7055e-10 0.00016631 1.0574e-05 5.885e-06 v Pressure -0.00063724 0.015681 0.00080358 -1.3384e-20 v k 4.7334e-09 0.0021168 0.0014883 0.0018323 v omega 24.309 1.0313e+05 2673.1 508.19 v TempK 288 341.7 292.85 290.08 v Density 1.205 1.205 1.205 1.205 v TurbVisc 5.567e-14 0.00010034 6.7272e-05 8.58e-05 v CourantNb 1.5037e-09 0.0002667 1.518e-05 7.7733e-06 v FourierNb 0.13412 0.6281 0.21035 0.17957 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.92 4.92 0.00043344 -3.8112e-07 v volume_forces[Z] -4.92 4.92 -0.00043329 4.6404e-07 v ǁvolume_forcesǁ 6.0733e-09 4.9216 0.44008 0.18814 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.07 290.23 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.017843 6.1924e-05 3.4972e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.13412 0.6281 0.21036 0.17958 INSTANT 0.364977000E+00 TIME STEP NUMBER 379 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.38810E-05 0.26802E-02 Friction velocity uk : 0.38980E-05 0.26801E-02 Dimensionless distance yplus : 0.25959E-04 0.17831E-01 Friction thermal sca. tstar : -0.18521E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.18232E-04 0.12523E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.38810E-05 0.26802E-02 Friction velocity uk : 0.38980E-05 0.26801E-02 Dimensionless distance yplus : 0.25959E-04 0.17831E-01 Friction thermal sca. tstar : -0.18521E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.18232E-04 0.12523E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.35431E-08 3 0.33591E-06 0.74769E-12 0.16232E+01 c Velocity[X] 0.57824E-31 c Velocity[Y] 0.37384E-12 c Velocity[Z] 0.37385E-12 c Pressure 0.22371E-13 20 0.69528E-08 0.17557E-06 0.21596E+01 c k 0.64167E-06 2 0.92126E-07 0.20512E-07 0.24345E+01 c omega 0.13153E+02 1 0.44327E-08 0.20162E+01 0.73922E-02 c TempK 0.94462E+02 1 0.23976E-06 0.57562E-01 0.26643E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.3183e-13 1.0875e-13 -1.3322e-17 -3.3909e-18 v Velocity[Y] -0.00015265 0.00014958 -1.0786e-09 -4.6325e-12 v Velocity[Z] -0.00014957 0.00015265 9.5122e-10 -1.9355e-12 v ǁVelocityǁ 1.7313e-10 0.00016613 1.0568e-05 5.8856e-06 v Pressure -0.00063895 0.015701 0.00080503 -3.6329e-20 v k 4.7025e-09 0.0021116 0.0014846 0.001828 v omega 24.263 1.0313e+05 2673.1 508.14 v TempK 288 341.7 292.85 290.09 v Density 1.205 1.205 1.205 1.205 v TurbVisc 5.5306e-14 0.00010032 6.7234e-05 8.576e-05 v CourantNb 1.5078e-09 0.00026635 1.5167e-05 7.7694e-06 v FourierNb 0.13402 0.6281 0.21025 0.17949 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9201 4.9202 0.0004338 -3.8179e-07 v volume_forces[Z] -4.9201 4.9202 -0.00043366 4.648e-07 v ǁvolume_forcesǁ 6.1653e-09 4.9217 0.44045 0.18839 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.07 290.23 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.017831 6.189e-05 3.4951e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.13402 0.6281 0.21027 0.1795 INSTANT 0.365940000E+00 TIME STEP NUMBER 380 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.39736E-05 0.26784E-02 Friction velocity uk : 0.39900E-05 0.26783E-02 Dimensionless distance yplus : 0.26572E-04 0.17819E-01 Friction thermal sca. tstar : -0.17897E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.18662E-04 0.12515E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.39736E-05 0.26784E-02 Friction velocity uk : 0.39900E-05 0.26783E-02 Dimensionless distance yplus : 0.26572E-04 0.17819E-01 Friction thermal sca. tstar : -0.17897E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.18662E-04 0.12515E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.35407E-08 3 0.33461E-06 0.74091E-12 0.16172E+01 c Velocity[X] 0.57222E-31 c Velocity[Y] 0.37045E-12 c Velocity[Z] 0.37046E-12 c Pressure 0.22262E-13 20 0.69285E-08 0.17471E-06 0.21537E+01 c k 0.64021E-06 2 0.91778E-07 0.20339E-07 0.24298E+01 c omega 0.13153E+02 1 0.44123E-08 0.20006E+01 0.73636E-02 c TempK 0.94463E+02 1 0.23890E-06 0.57340E-01 0.26591E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.3165e-13 1.0861e-13 -1.3307e-17 -3.3872e-18 v Velocity[Y] -0.0001525 0.00014941 -1.0791e-09 -4.6193e-12 v Velocity[Z] -0.00014941 0.0001525 9.5125e-10 -1.9384e-12 v ǁVelocityǁ 1.7575e-10 0.00016595 1.0562e-05 5.8864e-06 v Pressure -0.00064066 0.015722 0.00080648 -3.1377e-21 v k 4.6719e-09 0.0021063 0.0014809 0.0018237 v omega 24.216 1.0313e+05 2673.1 508.1 v TempK 288 341.7 292.85 290.09 v Density 1.205 1.205 1.205 1.205 v TurbVisc 5.4946e-14 0.0001003 6.7196e-05 8.5721e-05 v CourantNb 1.5118e-09 0.000266 1.5153e-05 7.7656e-06 v FourierNb 0.13392 0.6281 0.21016 0.17941 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9203 4.9203 0.00043417 -3.8245e-07 v volume_forces[Z] -4.9203 4.9203 -0.00043402 4.6555e-07 v ǁvolume_forcesǁ 6.2587e-09 4.9219 0.44082 0.18864 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.07 290.23 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.017819 6.1855e-05 3.4931e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.13392 0.6281 0.21017 0.17942 INSTANT 0.366903000E+00 TIME STEP NUMBER 381 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.40643E-05 0.26766E-02 Friction velocity uk : 0.40803E-05 0.26765E-02 Dimensionless distance yplus : 0.27173E-04 0.17807E-01 Friction thermal sca. tstar : -0.17332E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.19084E-04 0.12506E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.40643E-05 0.26766E-02 Friction velocity uk : 0.40803E-05 0.26765E-02 Dimensionless distance yplus : 0.27173E-04 0.17807E-01 Friction thermal sca. tstar : -0.17332E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.19084E-04 0.12506E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.35383E-08 3 0.33332E-06 0.73424E-12 0.16112E+01 c Velocity[X] 0.56627E-31 c Velocity[Y] 0.36711E-12 c Velocity[Z] 0.36712E-12 c Pressure 0.22152E-13 20 0.71248E-08 0.17384E-06 0.21478E+01 c k 0.63877E-06 2 0.91432E-07 0.20168E-07 0.24251E+01 c omega 0.13153E+02 1 0.43921E-08 0.19852E+01 0.73352E-02 c TempK 0.94463E+02 1 0.23804E-06 0.57119E-01 0.26540E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.3147e-13 1.0846e-13 -1.3291e-17 -3.3835e-18 v Velocity[Y] -0.00015235 0.00014925 -1.08e-09 -4.948e-12 v Velocity[Z] -0.00014925 0.00015236 9.5119e-10 -2.0148e-12 v ǁVelocityǁ 1.7792e-10 0.00016578 1.0557e-05 5.8872e-06 v Pressure -0.00064237 0.015743 0.00080792 -4.7605e-20 v k 4.6416e-09 0.0021011 0.0014773 0.0018194 v omega 24.17 1.0313e+05 2673 508.06 v TempK 288 341.7 292.86 290.09 v Density 1.205 1.205 1.205 1.205 v TurbVisc 5.4588e-14 0.00010028 6.7159e-05 8.5681e-05 v CourantNb 1.5159e-09 0.00026566 1.514e-05 7.7618e-06 v FourierNb 0.13382 0.6281 0.21006 0.17933 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9204 4.9205 0.00043453 -3.8311e-07 v volume_forces[Z] -4.9204 4.9205 -0.00043439 4.6631e-07 v ǁvolume_forcesǁ 6.3535e-09 4.922 0.44118 0.18889 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.08 290.24 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.017807 6.1821e-05 3.491e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.13382 0.6281 0.21008 0.17934 INSTANT 0.367866000E+00 TIME STEP NUMBER 382 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.41764E-05 0.26748E-02 Friction velocity uk : 0.41918E-05 0.26747E-02 Dimensionless distance yplus : 0.27915E-04 0.17795E-01 Friction thermal sca. tstar : -0.16817E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.19606E-04 0.12498E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.41764E-05 0.26748E-02 Friction velocity uk : 0.41918E-05 0.26747E-02 Dimensionless distance yplus : 0.27915E-04 0.17795E-01 Friction thermal sca. tstar : -0.16817E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.19606E-04 0.12498E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.35359E-08 3 0.47019E-06 0.72769E-12 0.16053E+01 c Velocity[X] 0.56047E-31 c Velocity[Y] 0.36384E-12 c Velocity[Z] 0.36385E-12 c Pressure 0.22161E-13 20 0.71157E-08 0.17391E-06 0.21420E+01 c k 0.63733E-06 2 0.91088E-07 0.19998E-07 0.24204E+01 c omega 0.13153E+02 1 0.43720E-08 0.19699E+01 0.73069E-02 c TempK 0.94464E+02 1 0.23718E-06 0.56900E-01 0.26489E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.313e-13 1.0832e-13 -1.3276e-17 -3.3797e-18 v Velocity[Y] -0.00015221 0.0001491 -1.0805e-09 -4.9363e-12 v Velocity[Z] -0.00014909 0.00015221 9.5119e-10 -2.0173e-12 v ǁVelocityǁ 1.8064e-10 0.0001656 1.0552e-05 5.888e-06 v Pressure -0.00064408 0.015764 0.00080936 -2.2013e-20 v k 4.6116e-09 0.0020959 0.0014736 0.0018152 v omega 24.124 1.0313e+05 2673 508.02 v TempK 288 341.71 292.86 290.1 v Density 1.205 1.205 1.205 1.205 v TurbVisc 5.4234e-14 0.00010026 6.7121e-05 8.5642e-05 v CourantNb 1.52e-09 0.00026531 1.5127e-05 7.7582e-06 v FourierNb 0.13372 0.6281 0.20997 0.17925 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9206 4.9206 0.0004349 -3.8377e-07 v volume_forces[Z] -4.9206 4.9206 -0.00043475 4.6707e-07 v ǁvolume_forcesǁ 6.4319e-09 4.9222 0.44155 0.18914 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.08 290.24 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.017795 6.1787e-05 3.489e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.13372 0.6281 0.20998 0.17926 INSTANT 0.368829000E+00 TIME STEP NUMBER 383 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.42629E-05 0.26730E-02 Friction velocity uk : 0.42777E-05 0.26729E-02 Dimensionless distance yplus : 0.28488E-04 0.17783E-01 Friction thermal sca. tstar : -0.16346E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.20008E-04 0.12490E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.42629E-05 0.26730E-02 Friction velocity uk : 0.42777E-05 0.26729E-02 Dimensionless distance yplus : 0.28488E-04 0.17783E-01 Friction thermal sca. tstar : -0.16346E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.20008E-04 0.12490E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.35336E-08 3 0.33082E-06 0.72124E-12 0.15995E+01 c Velocity[X] 0.55472E-31 c Velocity[Y] 0.36062E-12 c Velocity[Z] 0.36063E-12 c Pressure 0.21996E-13 20 0.70855E-08 0.17261E-06 0.21362E+01 c k 0.63589E-06 2 0.90747E-07 0.19830E-07 0.24157E+01 c omega 0.13153E+02 1 0.43520E-08 0.19548E+01 0.72788E-02 c TempK 0.94465E+02 1 0.23633E-06 0.56682E-01 0.26438E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.3112e-13 1.0818e-13 -1.326e-17 -3.3761e-18 v Velocity[Y] -0.00015206 0.00014894 -1.081e-09 -4.9221e-12 v Velocity[Z] -0.00014894 0.00015207 9.5119e-10 -2.0219e-12 v ǁVelocityǁ 1.8337e-10 0.00016542 1.0546e-05 5.8889e-06 v Pressure -0.00064578 0.015785 0.0008108 -4.5644e-20 v k 4.5818e-09 0.0020907 0.00147 0.0018109 v omega 24.078 1.0313e+05 2673 507.98 v TempK 288 341.71 292.87 290.1 v Density 1.205 1.205 1.205 1.205 v TurbVisc 5.3883e-14 0.00010024 6.7084e-05 8.5603e-05 v CourantNb 1.5241e-09 0.00026497 1.5114e-05 7.7546e-06 v FourierNb 0.13362 0.6281 0.20987 0.17917 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9207 4.9207 0.00043526 -3.8443e-07 v volume_forces[Z] -4.9207 4.9207 -0.00043511 4.6782e-07 v ǁvolume_forcesǁ 6.5301e-09 4.9223 0.44191 0.18939 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.09 290.24 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.017783 6.1753e-05 3.4869e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.13362 0.6281 0.20989 0.17918 INSTANT 0.369792000E+00 TIME STEP NUMBER 384 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.43482E-05 0.26712E-02 Friction velocity uk : 0.43627E-05 0.26711E-02 Dimensionless distance yplus : 0.29053E-04 0.17771E-01 Friction thermal sca. tstar : -0.16506E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.20405E-04 0.12481E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.43482E-05 0.26712E-02 Friction velocity uk : 0.43627E-05 0.26711E-02 Dimensionless distance yplus : 0.29053E-04 0.17771E-01 Friction thermal sca. tstar : -0.16506E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.20405E-04 0.12481E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.35313E-08 3 0.32953E-06 0.71491E-12 0.15937E+01 c Velocity[X] 0.54906E-31 c Velocity[Y] 0.35745E-12 c Velocity[Z] 0.35746E-12 c Pressure 0.21848E-13 20 0.70556E-08 0.17143E-06 0.21304E+01 c k 0.63446E-06 2 0.90409E-07 0.19663E-07 0.24110E+01 c omega 0.13153E+02 1 0.43322E-08 0.19398E+01 0.72508E-02 c TempK 0.94465E+02 1 0.23548E-06 0.56466E-01 0.26387E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.3095e-13 1.0804e-13 -1.3245e-17 -3.3724e-18 v Velocity[Y] -0.00015192 0.00014878 -1.0815e-09 -4.9088e-12 v Velocity[Z] -0.00014878 0.00015192 9.5117e-10 -2.0248e-12 v ǁVelocityǁ 1.8612e-10 0.00016525 1.0541e-05 5.8899e-06 v Pressure -0.00064749 0.015806 0.00081224 2.1523e-20 v k 4.5523e-09 0.0020855 0.0014663 0.0018067 v omega 24.032 1.0313e+05 2672.9 507.93 v TempK 288 341.71 292.87 290.1 v Density 1.205 1.205 1.205 1.205 v TurbVisc 5.3535e-14 0.00010022 6.7046e-05 8.5564e-05 v CourantNb 1.5282e-09 0.00026463 1.5101e-05 7.7511e-06 v FourierNb 0.13352 0.6281 0.20978 0.17909 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9208 4.9209 0.00043562 -3.8508e-07 v volume_forces[Z] -4.9208 4.9209 -0.00043548 4.6857e-07 v ǁvolume_forcesǁ 6.6287e-09 4.9224 0.44228 0.18964 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.09 290.25 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.017771 6.1719e-05 3.4849e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.13353 0.6281 0.20979 0.1791 INSTANT 0.370755000E+00 TIME STEP NUMBER 385 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.44323E-05 0.26695E-02 Friction velocity uk : 0.44463E-05 0.26693E-02 Dimensionless distance yplus : 0.29610E-04 0.17759E-01 Friction thermal sca. tstar : -0.16907E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.20796E-04 0.12473E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.44323E-05 0.26695E-02 Friction velocity uk : 0.44463E-05 0.26693E-02 Dimensionless distance yplus : 0.29610E-04 0.17759E-01 Friction thermal sca. tstar : -0.16907E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.20796E-04 0.12473E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.35290E-08 3 0.32827E-06 0.70869E-12 0.15880E+01 c Velocity[X] 0.54349E-31 c Velocity[Y] 0.35434E-12 c Velocity[Z] 0.35435E-12 c Pressure 0.21739E-13 20 0.70323E-08 0.17057E-06 0.21247E+01 c k 0.63304E-06 2 0.90073E-07 0.19499E-07 0.24064E+01 c omega 0.13153E+02 1 0.43125E-08 0.19250E+01 0.72230E-02 c TempK 0.94466E+02 1 0.23464E-06 0.56250E-01 0.26336E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.3077e-13 1.079e-13 -1.323e-17 -3.3687e-18 v Velocity[Y] -0.00015177 0.00014863 -1.082e-09 -4.8956e-12 v Velocity[Z] -0.00014862 0.00015178 9.5114e-10 -2.0275e-12 v ǁVelocityǁ 1.8891e-10 0.00016508 1.0536e-05 5.8909e-06 v Pressure -0.0006492 0.015827 0.00081367 -1.1207e-19 v k 4.523e-09 0.0020804 0.0014627 0.0018025 v omega 23.987 1.0313e+05 2672.9 507.89 v TempK 288 341.71 292.87 290.1 v Density 1.205 1.205 1.205 1.205 v TurbVisc 5.319e-14 0.0001002 6.7009e-05 8.5524e-05 v CourantNb 1.5323e-09 0.0002643 1.5089e-05 7.7477e-06 v FourierNb 0.13342 0.6281 0.20968 0.17901 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.921 4.921 0.00043598 -3.8573e-07 v volume_forces[Z] -4.921 4.921 -0.00043584 4.6932e-07 v ǁvolume_forcesǁ 6.7283e-09 4.9226 0.44264 0.18989 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.09 290.25 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.017759 6.1686e-05 3.4829e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.13343 0.6281 0.2097 0.17902 INSTANT 0.371718000E+00 TIME STEP NUMBER 386 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.45150E-05 0.26677E-02 Friction velocity uk : 0.45287E-05 0.26676E-02 Dimensionless distance yplus : 0.30159E-04 0.17748E-01 Friction thermal sca. tstar : -0.17341E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.21182E-04 0.12465E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.45150E-05 0.26677E-02 Friction velocity uk : 0.45287E-05 0.26676E-02 Dimensionless distance yplus : 0.30159E-04 0.17748E-01 Friction thermal sca. tstar : -0.17341E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.21182E-04 0.12465E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.35268E-08 3 0.32705E-06 0.70257E-12 0.15824E+01 c Velocity[X] 0.53800E-31 c Velocity[Y] 0.35128E-12 c Velocity[Z] 0.35129E-12 c Pressure 0.21637E-13 20 0.70096E-08 0.16977E-06 0.21190E+01 c k 0.63162E-06 2 0.89739E-07 0.19336E-07 0.24018E+01 c omega 0.13153E+02 1 0.42929E-08 0.19103E+01 0.71954E-02 c TempK 0.94467E+02 1 0.23380E-06 0.56037E-01 0.26286E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.306e-13 1.0776e-13 -1.3215e-17 -3.3651e-18 v Velocity[Y] -0.00015163 0.00014847 -1.0825e-09 -4.8824e-12 v Velocity[Z] -0.00014847 0.00015163 9.5111e-10 -2.0303e-12 v ǁVelocityǁ 1.9173e-10 0.0001649 1.0531e-05 5.892e-06 v Pressure -0.00065091 0.015848 0.00081511 3.8829e-20 v k 4.494e-09 0.0020752 0.0014591 0.0017983 v omega 23.941 1.0313e+05 2672.9 507.85 v TempK 288 341.71 292.88 290.11 v Density 1.205 1.205 1.205 1.205 v TurbVisc 5.2848e-14 0.00010019 6.6972e-05 8.5485e-05 v CourantNb 1.5364e-09 0.00026396 1.5076e-05 7.7443e-06 v FourierNb 0.13333 0.6281 0.20959 0.17893 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9211 4.9212 0.00043634 -3.8639e-07 v volume_forces[Z] -4.9211 4.9212 -0.0004362 4.7006e-07 v ǁvolume_forcesǁ 6.8291e-09 4.9227 0.443 0.19014 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.1 290.25 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.017748 6.1652e-05 3.4809e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.13333 0.6281 0.20961 0.17894 INSTANT 0.372681000E+00 TIME STEP NUMBER 387 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.45864E-05 0.26659E-02 Friction velocity uk : 0.45997E-05 0.26658E-02 Dimensionless distance yplus : 0.30629E-04 0.17736E-01 Friction thermal sca. tstar : -0.17811E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.21512E-04 0.12457E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.45864E-05 0.26659E-02 Friction velocity uk : 0.45997E-05 0.26658E-02 Dimensionless distance yplus : 0.30629E-04 0.17736E-01 Friction thermal sca. tstar : -0.17811E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.21512E-04 0.12457E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.35246E-08 3 0.32579E-06 0.69655E-12 0.15769E+01 c Velocity[X] 0.53260E-31 c Velocity[Y] 0.34827E-12 c Velocity[Z] 0.34828E-12 c Pressure 0.21530E-13 20 0.69874E-08 0.16892E-06 0.21133E+01 c k 0.63021E-06 2 0.89408E-07 0.19175E-07 0.23972E+01 c omega 0.13153E+02 1 0.42734E-08 0.18957E+01 0.71679E-02 c TempK 0.94467E+02 1 0.23297E-06 0.55824E-01 0.26236E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.3043e-13 1.0762e-13 -1.32e-17 -3.3615e-18 v Velocity[Y] -0.00015149 0.00014832 -1.083e-09 -4.8692e-12 v Velocity[Z] -0.00014831 0.00015149 9.5106e-10 -2.0332e-12 v ǁVelocityǁ 1.9458e-10 0.00016473 1.0526e-05 5.8931e-06 v Pressure -0.00065262 0.015868 0.00081654 -1.3237e-21 v k 4.4652e-09 0.0020701 0.0014556 0.0017942 v omega 23.896 1.0313e+05 2672.8 507.81 v TempK 288 341.71 292.88 290.11 v Density 1.205 1.205 1.205 1.205 v TurbVisc 5.2509e-14 0.00010017 6.6935e-05 8.5446e-05 v CourantNb 1.5405e-09 0.00026363 1.5064e-05 7.741e-06 v FourierNb 0.13323 0.6281 0.2095 0.17885 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9213 4.9213 0.00043671 -3.8703e-07 v volume_forces[Z] -4.9213 4.9213 -0.00043656 4.708e-07 v ǁvolume_forcesǁ 6.931e-09 4.9229 0.44336 0.19039 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.1 290.25 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.017736 6.1618e-05 3.4789e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.13323 0.6281 0.20951 0.17886 INSTANT 0.373644000E+00 TIME STEP NUMBER 388 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.46436E-05 0.26642E-02 Friction velocity uk : 0.46566E-05 0.26641E-02 Dimensionless distance yplus : 0.31008E-04 0.17724E-01 Friction thermal sca. tstar : -0.18325E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.21778E-04 0.12448E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.46436E-05 0.26642E-02 Friction velocity uk : 0.46566E-05 0.26641E-02 Dimensionless distance yplus : 0.31008E-04 0.17724E-01 Friction thermal sca. tstar : -0.18325E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.21778E-04 0.12448E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.35225E-08 3 0.32456E-06 0.69064E-12 0.15714E+01 c Velocity[X] 0.52728E-31 c Velocity[Y] 0.34531E-12 c Velocity[Z] 0.34533E-12 c Pressure 0.21437E-13 20 0.69636E-08 0.16819E-06 0.21077E+01 c k 0.62880E-06 2 0.89079E-07 0.19015E-07 0.23926E+01 c omega 0.13153E+02 1 0.42541E-08 0.18813E+01 0.71406E-02 c TempK 0.94468E+02 1 0.23214E-06 0.55613E-01 0.26186E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.3026e-13 1.0749e-13 -1.3184e-17 -3.3578e-18 v Velocity[Y] -0.00015135 0.00014816 -1.0834e-09 -4.8561e-12 v Velocity[Z] -0.00014816 0.00015135 9.51e-10 -2.036e-12 v ǁVelocityǁ 1.9746e-10 0.00016456 1.0521e-05 5.8943e-06 v Pressure -0.00065433 0.015889 0.00081797 4.3781e-20 v k 4.4367e-09 0.002065 0.001452 0.00179 v omega 23.851 1.0313e+05 2672.8 507.77 v TempK 288 341.72 292.89 290.11 v Density 1.205 1.205 1.205 1.205 v TurbVisc 5.2173e-14 0.00010015 6.6898e-05 8.5408e-05 v CourantNb 1.5445e-09 0.0002633 1.5051e-05 7.7378e-06 v FourierNb 0.13313 0.6281 0.2094 0.17877 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9214 4.9215 0.00043706 -3.8768e-07 v volume_forces[Z] -4.9214 4.9215 -0.00043692 4.7154e-07 v ǁvolume_forcesǁ 7.034e-09 4.923 0.44372 0.19064 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.11 290.26 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.017724 6.1585e-05 3.4769e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.13313 0.6281 0.20942 0.17878 INSTANT 0.374607000E+00 TIME STEP NUMBER 389 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.47003E-05 0.26624E-02 Friction velocity uk : 0.47130E-05 0.26623E-02 Dimensionless distance yplus : 0.31383E-04 0.17713E-01 Friction thermal sca. tstar : -0.18888E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.22042E-04 0.12440E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.47003E-05 0.26624E-02 Friction velocity uk : 0.47130E-05 0.26623E-02 Dimensionless distance yplus : 0.31383E-04 0.17713E-01 Friction thermal sca. tstar : -0.18888E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.22042E-04 0.12440E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.35203E-08 3 0.32334E-06 0.68483E-12 0.15659E+01 c Velocity[X] 0.52204E-31 c Velocity[Y] 0.34241E-12 c Velocity[Z] 0.34242E-12 c Pressure 0.21331E-13 20 0.69434E-08 0.16735E-06 0.21020E+01 c k 0.62740E-06 2 0.88753E-07 0.18857E-07 0.23880E+01 c omega 0.13153E+02 1 0.42349E-08 0.18670E+01 0.71134E-02 c TempK 0.94469E+02 1 0.23132E-06 0.55403E-01 0.26136E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.3009e-13 1.0735e-13 -1.3169e-17 -3.3542e-18 v Velocity[Y] -0.00015121 0.00014801 -1.0839e-09 -4.8431e-12 v Velocity[Z] -0.00014801 0.00015121 9.5093e-10 -2.0388e-12 v ǁVelocityǁ 2.0037e-10 0.00016439 1.0516e-05 5.8955e-06 v Pressure -0.00065604 0.01591 0.0008194 -5.236e-20 v k 4.4084e-09 0.00206 0.0014484 0.0017859 v omega 23.806 1.0313e+05 2672.8 507.73 v TempK 288 341.72 292.89 290.12 v Density 1.205 1.205 1.205 1.205 v TurbVisc 5.184e-14 0.00010013 6.6861e-05 8.5369e-05 v CourantNb 1.5486e-09 0.00026297 1.5039e-05 7.7347e-06 v FourierNb 0.13303 0.6281 0.20931 0.17869 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9216 4.9216 0.00043742 -3.8833e-07 v volume_forces[Z] -4.9216 4.9216 -0.00043728 4.7227e-07 v ǁvolume_forcesǁ 7.1382e-09 4.9231 0.44408 0.19089 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.11 290.26 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.017713 6.1552e-05 3.4749e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.13303 0.6281 0.20933 0.1787 INSTANT 0.375570000E+00 TIME STEP NUMBER 390 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.47564E-05 0.26607E-02 Friction velocity uk : 0.47689E-05 0.26606E-02 Dimensionless distance yplus : 0.31756E-04 0.17701E-01 Friction thermal sca. tstar : -0.19509E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.22303E-04 0.12432E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.47564E-05 0.26607E-02 Friction velocity uk : 0.47689E-05 0.26606E-02 Dimensionless distance yplus : 0.31756E-04 0.17701E-01 Friction thermal sca. tstar : -0.19509E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.22303E-04 0.12432E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.35182E-08 3 0.32218E-06 0.67911E-12 0.15606E+01 c Velocity[X] 0.51688E-31 c Velocity[Y] 0.33955E-12 c Velocity[Z] 0.33956E-12 c Pressure 0.21265E-13 20 0.69205E-08 0.16682E-06 0.20965E+01 c k 0.62600E-06 2 0.88428E-07 0.18701E-07 0.23835E+01 c omega 0.13153E+02 1 0.42158E-08 0.18528E+01 0.70864E-02 c TempK 0.94469E+02 1 0.23051E-06 0.55195E-01 0.26087E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.2992e-13 1.0722e-13 -1.3155e-17 -3.3506e-18 v Velocity[Y] -0.00015107 0.00014786 -1.0843e-09 -4.83e-12 v Velocity[Z] -0.00014786 0.00015107 9.5085e-10 -2.0417e-12 v ǁVelocityǁ 2.0331e-10 0.00016423 1.0512e-05 5.8968e-06 v Pressure -0.00065775 0.01593 0.00082083 2.4072e-20 v k 4.3804e-09 0.0020549 0.0014449 0.0017818 v omega 23.762 1.0313e+05 2672.7 507.69 v TempK 288 341.72 292.89 290.12 v Density 1.205 1.205 1.205 1.205 v TurbVisc 5.1509e-14 0.00010011 6.6824e-05 8.533e-05 v CourantNb 1.5527e-09 0.00026264 1.5027e-05 7.7316e-06 v FourierNb 0.13293 0.6281 0.20922 0.17861 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9217 4.9217 0.00043778 -3.8897e-07 v volume_forces[Z] -4.9217 4.9217 -0.00043764 4.7301e-07 v ǁvolume_forcesǁ 7.2434e-09 4.9233 0.44444 0.19114 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.11 290.26 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.017701 6.1519e-05 3.4729e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.13293 0.6281 0.20924 0.17862 INSTANT 0.376533000E+00 TIME STEP NUMBER 391 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.48121E-05 0.26590E-02 Friction velocity uk : 0.48243E-05 0.26589E-02 Dimensionless distance yplus : 0.32125E-04 0.17690E-01 Friction thermal sca. tstar : -0.20199E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.22562E-04 0.12424E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.48121E-05 0.26590E-02 Friction velocity uk : 0.48243E-05 0.26589E-02 Dimensionless distance yplus : 0.32125E-04 0.17690E-01 Friction thermal sca. tstar : -0.20199E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.22562E-04 0.12424E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.35162E-08 3 0.32096E-06 0.67350E-12 0.15553E+01 c Velocity[X] 0.51180E-31 c Velocity[Y] 0.33674E-12 c Velocity[Z] 0.33676E-12 c Pressure 0.21157E-13 20 0.69001E-08 0.16597E-06 0.20909E+01 c k 0.62462E-06 2 0.88106E-07 0.18546E-07 0.23790E+01 c omega 0.13153E+02 1 0.41968E-08 0.18388E+01 0.70595E-02 c TempK 0.94470E+02 1 0.22969E-06 0.54987E-01 0.26037E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.2975e-13 1.0708e-13 -1.314e-17 -3.3471e-18 v Velocity[Y] -0.00015093 0.00014771 -1.0847e-09 -4.8172e-12 v Velocity[Z] -0.0001477 0.00015093 9.5075e-10 -2.0444e-12 v ǁVelocityǁ 2.0628e-10 0.00016406 1.0507e-05 5.8981e-06 v Pressure -0.00065945 0.015951 0.00082225 7.202e-20 v k 4.3526e-09 0.00205 0.0014414 0.0017777 v omega 23.717 1.0313e+05 2672.7 507.65 v TempK 288 341.72 292.9 290.12 v Density 1.205 1.205 1.205 1.205 v TurbVisc 5.1182e-14 0.00010009 6.6787e-05 8.5291e-05 v CourantNb 1.5568e-09 0.00026232 1.5015e-05 7.7286e-06 v FourierNb 0.13283 0.6281 0.20913 0.17853 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9218 4.9219 0.00043814 -3.8961e-07 v volume_forces[Z] -4.9218 4.9219 -0.00043799 4.7374e-07 v ǁvolume_forcesǁ 7.3496e-09 4.9234 0.4448 0.19138 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.12 290.27 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.01769 6.1486e-05 3.4709e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.13284 0.6281 0.20914 0.17854 INSTANT 0.377496000E+00 TIME STEP NUMBER 392 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.48673E-05 0.26573E-02 Friction velocity uk : 0.48793E-05 0.26571E-02 Dimensionless distance yplus : 0.32491E-04 0.17678E-01 Friction thermal sca. tstar : -0.20970E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.22819E-04 0.12416E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.48673E-05 0.26573E-02 Friction velocity uk : 0.48793E-05 0.26571E-02 Dimensionless distance yplus : 0.32491E-04 0.17678E-01 Friction thermal sca. tstar : -0.20970E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.22819E-04 0.12416E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.35142E-08 3 0.31975E-06 0.66798E-12 0.15500E+01 c Velocity[X] 0.50680E-31 c Velocity[Y] 0.33398E-12 c Velocity[Z] 0.33400E-12 c Pressure 0.21041E-13 20 0.68782E-08 0.16506E-06 0.20854E+01 c k 0.62323E-06 2 0.87787E-07 0.18393E-07 0.23745E+01 c omega 0.13153E+02 1 0.41779E-08 0.18249E+01 0.70328E-02 c TempK 0.94471E+02 1 0.22889E-06 0.54781E-01 0.25988E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.2958e-13 1.0695e-13 -1.3125e-17 -3.3435e-18 v Velocity[Y] -0.00015079 0.00014756 -1.0851e-09 -4.8043e-12 v Velocity[Z] -0.00014755 0.00015079 9.5065e-10 -2.0471e-12 v ǁVelocityǁ 2.0927e-10 0.00016389 1.0503e-05 5.8995e-06 v Pressure -0.00066116 0.015972 0.00082368 -4.6085e-20 v k 4.325e-09 0.0020452 0.0014379 0.0017736 v omega 23.673 1.0313e+05 2672.7 507.61 v TempK 288 341.72 292.9 290.12 v Density 1.205 1.205 1.205 1.205 v TurbVisc 5.0857e-14 0.00010007 6.6751e-05 8.5253e-05 v CourantNb 1.5609e-09 0.00026199 1.5004e-05 7.7256e-06 v FourierNb 0.13274 0.6281 0.20904 0.17846 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.922 4.922 0.0004385 -3.9025e-07 v volume_forces[Z] -4.922 4.922 -0.00043835 4.7447e-07 v ǁvolume_forcesǁ 7.4568e-09 4.9236 0.44516 0.19163 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.12 290.27 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.017678 6.1453e-05 3.4689e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.13274 0.6281 0.20905 0.17846 INSTANT 0.378459000E+00 TIME STEP NUMBER 393 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.49221E-05 0.26555E-02 Friction velocity uk : 0.49338E-05 0.26554E-02 Dimensionless distance yplus : 0.32854E-04 0.17667E-01 Friction thermal sca. tstar : -0.21842E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.23074E-04 0.12408E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.49221E-05 0.26555E-02 Friction velocity uk : 0.49338E-05 0.26554E-02 Dimensionless distance yplus : 0.32854E-04 0.17667E-01 Friction thermal sca. tstar : -0.21842E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.23074E-04 0.12408E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.35122E-08 3 0.31867E-06 0.66256E-12 0.15449E+01 c Velocity[X] 0.50186E-31 c Velocity[Y] 0.33128E-12 c Velocity[Z] 0.33129E-12 c Pressure 0.21135E-13 20 0.68660E-08 0.16578E-06 0.20799E+01 c k 0.62185E-06 2 0.87470E-07 0.18242E-07 0.23700E+01 c omega 0.13153E+02 1 0.41592E-08 0.18111E+01 0.70062E-02 c TempK 0.94471E+02 1 0.22809E-06 0.54577E-01 0.25939E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.2942e-13 1.0681e-13 -1.311e-17 -3.34e-18 v Velocity[Y] -0.00015065 0.00014741 -1.0855e-09 -4.7917e-12 v Velocity[Z] -0.00014741 0.00015066 9.5054e-10 -2.05e-12 v ǁVelocityǁ 2.1229e-10 0.00016373 1.0498e-05 5.9009e-06 v Pressure -0.00066287 0.015992 0.0008251 4.2212e-20 v k 4.2977e-09 0.0020405 0.0014344 0.0017695 v omega 23.629 1.0313e+05 2672.6 507.57 v TempK 288 341.72 292.91 290.13 v Density 1.205 1.205 1.205 1.205 v TurbVisc 5.0535e-14 0.00010005 6.6714e-05 8.5214e-05 v CourantNb 1.565e-09 0.00026167 1.4992e-05 7.7228e-06 v FourierNb 0.13264 0.6281 0.20895 0.17838 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9221 4.9221 0.00043885 -3.9089e-07 v volume_forces[Z] -4.9221 4.9221 -0.00043871 4.752e-07 v ǁvolume_forcesǁ 7.5651e-09 4.9237 0.44552 0.19188 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.13 290.27 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.017667 6.142e-05 3.467e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.13264 0.6281 0.20896 0.17839 INSTANT 0.379422000E+00 TIME STEP NUMBER 394 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.49764E-05 0.26538E-02 Friction velocity uk : 0.49878E-05 0.26537E-02 Dimensionless distance yplus : 0.33213E-04 0.17655E-01 Friction thermal sca. tstar : -0.22836E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.23327E-04 0.12400E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.49764E-05 0.26538E-02 Friction velocity uk : 0.49878E-05 0.26537E-02 Dimensionless distance yplus : 0.33213E-04 0.17655E-01 Friction thermal sca. tstar : -0.22836E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.23327E-04 0.12400E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.35102E-08 3 0.31744E-06 0.65723E-12 0.15398E+01 c Velocity[X] 0.49701E-31 c Velocity[Y] 0.32861E-12 c Velocity[Z] 0.32862E-12 c Pressure 0.20862E-13 20 0.68347E-08 0.16364E-06 0.20744E+01 c k 0.62048E-06 2 0.87154E-07 0.18092E-07 0.23655E+01 c omega 0.13153E+02 1 0.41406E-08 0.17975E+01 0.69798E-02 c TempK 0.94472E+02 1 0.22729E-06 0.54373E-01 0.25891E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.2925e-13 1.0668e-13 -1.3095e-17 -3.3364e-18 v Velocity[Y] -0.00015052 0.00014726 -1.0859e-09 -4.7787e-12 v Velocity[Z] -0.00014726 0.00015052 9.5041e-10 -2.0528e-12 v ǁVelocityǁ 2.1534e-10 0.00016356 1.0494e-05 5.9024e-06 v Pressure -0.00066458 0.016013 0.00082652 7.5305e-20 v k 4.2706e-09 0.0020357 0.001431 0.0017655 v omega 23.585 1.0313e+05 2672.6 507.53 v TempK 288 341.72 292.91 290.13 v Density 1.205 1.205 1.205 1.205 v TurbVisc 5.0216e-14 0.00010004 6.6678e-05 8.5176e-05 v CourantNb 1.569e-09 0.00026135 1.498e-05 7.72e-06 v FourierNb 0.13254 0.6281 0.20886 0.1783 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9222 4.9223 0.00043921 -3.9153e-07 v volume_forces[Z] -4.9222 4.9223 -0.00043906 4.7592e-07 v ǁvolume_forcesǁ 7.6742e-09 4.9238 0.44587 0.19213 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.13 290.27 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.017655 6.1387e-05 3.465e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.13254 0.6281 0.20887 0.17831 INSTANT 0.380385000E+00 TIME STEP NUMBER 395 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.50303E-05 0.26521E-02 Friction velocity uk : 0.50415E-05 0.26520E-02 Dimensionless distance yplus : 0.33571E-04 0.17644E-01 Friction thermal sca. tstar : -0.23984E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.23578E-04 0.12392E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.50303E-05 0.26521E-02 Friction velocity uk : 0.50415E-05 0.26520E-02 Dimensionless distance yplus : 0.33571E-04 0.17644E-01 Friction thermal sca. tstar : -0.23984E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.23578E-04 0.12392E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.35082E-08 3 0.31623E-06 0.65199E-12 0.15347E+01 c Velocity[X] 0.49223E-31 c Velocity[Y] 0.32599E-12 c Velocity[Z] 0.32600E-12 c Pressure 0.20756E-13 20 0.68172E-08 0.16280E-06 0.20689E+01 c k 0.61911E-06 2 0.86842E-07 0.17943E-07 0.23610E+01 c omega 0.13153E+02 1 0.41221E-08 0.17840E+01 0.69535E-02 c TempK 0.94473E+02 1 0.22649E-06 0.54171E-01 0.25842E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.2909e-13 1.0655e-13 -1.3081e-17 -3.3329e-18 v Velocity[Y] -0.00015038 0.00014711 -1.0863e-09 -4.7659e-12 v Velocity[Z] -0.00014711 0.00015038 9.5028e-10 -2.0556e-12 v ǁVelocityǁ 2.1841e-10 0.0001634 1.049e-05 5.904e-06 v Pressure -0.00066629 0.016033 0.00082794 -8.9718e-21 v k 4.2438e-09 0.002031 0.0014275 0.0017614 v omega 23.541 1.0313e+05 2672.6 507.49 v TempK 288 341.73 292.91 290.13 v Density 1.205 1.205 1.205 1.205 v TurbVisc 4.9899e-14 0.00010002 6.6642e-05 8.5138e-05 v CourantNb 1.5731e-09 0.00026104 1.4969e-05 7.7173e-06 v FourierNb 0.13244 0.6281 0.20876 0.17822 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9224 4.9224 0.00043956 -3.9216e-07 v volume_forces[Z] -4.9224 4.9224 -0.00043942 4.7664e-07 v ǁvolume_forcesǁ 7.7845e-09 4.924 0.44623 0.19237 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.13 290.28 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.017644 6.1355e-05 3.463e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.13245 0.6281 0.20878 0.17823 INSTANT 0.381348000E+00 TIME STEP NUMBER 396 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.50838E-05 0.26505E-02 Friction velocity uk : 0.50948E-05 0.26503E-02 Dimensionless distance yplus : 0.33926E-04 0.17633E-01 Friction thermal sca. tstar : -0.25331E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.23827E-04 0.12384E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.50838E-05 0.26505E-02 Friction velocity uk : 0.50948E-05 0.26503E-02 Dimensionless distance yplus : 0.33926E-04 0.17633E-01 Friction thermal sca. tstar : -0.25331E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.23827E-04 0.12384E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.35063E-08 3 0.31507E-06 0.64684E-12 0.15298E+01 c Velocity[X] 0.48751E-31 c Velocity[Y] 0.32341E-12 c Velocity[Z] 0.32342E-12 c Pressure 0.20668E-13 20 0.67956E-08 0.16210E-06 0.20635E+01 c k 0.61775E-06 2 0.86531E-07 0.17796E-07 0.23566E+01 c omega 0.13153E+02 1 0.41037E-08 0.17706E+01 0.69274E-02 c TempK 0.94473E+02 1 0.22571E-06 0.53970E-01 0.25794E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.2892e-13 1.0642e-13 -1.3066e-17 -3.3294e-18 v Velocity[Y] -0.00015025 0.00014697 -1.0867e-09 -4.7532e-12 v Velocity[Z] -0.00014696 0.00015025 9.5013e-10 -2.0584e-12 v ǁVelocityǁ 2.2151e-10 0.00016324 1.0485e-05 5.9055e-06 v Pressure -0.000668 0.016054 0.00082935 1.7699e-20 v k 4.2171e-09 0.0020263 0.0014241 0.0017574 v omega 23.497 1.0313e+05 2672.5 507.45 v TempK 288 341.73 292.92 290.13 v Density 1.205 1.205 1.205 1.205 v TurbVisc 4.9585e-14 9.9999e-05 6.6605e-05 8.5099e-05 v CourantNb 1.5772e-09 0.00026072 1.4957e-05 7.7146e-06 v FourierNb 0.13235 0.6281 0.20867 0.17815 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9225 4.9226 0.00043992 -3.9279e-07 v volume_forces[Z] -4.9225 4.9226 -0.00043977 4.7737e-07 v ǁvolume_forcesǁ 7.8956e-09 4.9241 0.44658 0.19262 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.14 290.28 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.017633 6.1322e-05 3.4611e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.13235 0.6281 0.20869 0.17815 INSTANT 0.382311000E+00 TIME STEP NUMBER 397 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.51369E-05 0.26488E-02 Friction velocity uk : 0.51476E-05 0.26487E-02 Dimensionless distance yplus : 0.34278E-04 0.17622E-01 Friction thermal sca. tstar : -0.26941E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.24074E-04 0.12376E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.51369E-05 0.26488E-02 Friction velocity uk : 0.51476E-05 0.26487E-02 Dimensionless distance yplus : 0.34278E-04 0.17622E-01 Friction thermal sca. tstar : -0.26941E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.24074E-04 0.12376E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.35044E-08 3 0.31391E-06 0.64177E-12 0.15248E+01 c Velocity[X] 0.48287E-31 c Velocity[Y] 0.32088E-12 c Velocity[Z] 0.32089E-12 c Pressure 0.20569E-13 20 0.67759E-08 0.16132E-06 0.20581E+01 c k 0.61640E-06 2 0.86222E-07 0.17650E-07 0.23522E+01 c omega 0.13153E+02 1 0.40854E-08 0.17574E+01 0.69014E-02 c TempK 0.94474E+02 1 0.22492E-06 0.53771E-01 0.25746E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.2876e-13 1.0629e-13 -1.3052e-17 -3.3259e-18 v Velocity[Y] -0.00015011 0.00014682 -1.087e-09 -4.7405e-12 v Velocity[Z] -0.00014682 0.00015012 9.4998e-10 -2.0612e-12 v ǁVelocityǁ 2.2464e-10 0.00016307 1.0481e-05 5.9072e-06 v Pressure -0.00066971 0.016074 0.00083077 5.3586e-20 v k 4.1907e-09 0.0020216 0.0014206 0.0017534 v omega 23.453 1.0313e+05 2672.5 507.41 v TempK 288 341.73 292.92 290.14 v Density 1.205 1.205 1.205 1.205 v TurbVisc 4.9274e-14 9.998e-05 6.6569e-05 8.5061e-05 v CourantNb 1.5813e-09 0.00026041 1.4946e-05 7.712e-06 v FourierNb 0.13225 0.6281 0.20858 0.17807 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9227 4.9227 0.00044027 -3.9342e-07 v volume_forces[Z] -4.9227 4.9227 -0.00044012 4.7808e-07 v ǁvolume_forcesǁ 8.0076e-09 4.9242 0.44694 0.19287 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.14 290.28 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.017622 6.129e-05 3.4591e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.13225 0.6281 0.2086 0.17808 INSTANT 0.383274000E+00 TIME STEP NUMBER 398 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.51896E-05 0.26471E-02 Friction velocity uk : 0.52001E-05 0.26470E-02 Dimensionless distance yplus : 0.34627E-04 0.17611E-01 Friction thermal sca. tstar : -0.28912E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.24320E-04 0.12369E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.51896E-05 0.26471E-02 Friction velocity uk : 0.52001E-05 0.26470E-02 Dimensionless distance yplus : 0.34627E-04 0.17611E-01 Friction thermal sca. tstar : -0.28912E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.24320E-04 0.12369E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.35026E-08 3 0.31277E-06 0.63679E-12 0.15200E+01 c Velocity[X] 0.47829E-31 c Velocity[Y] 0.31839E-12 c Velocity[Z] 0.31840E-12 c Pressure 0.20486E-13 20 0.67567E-08 0.16066E-06 0.20528E+01 c k 0.61505E-06 2 0.85916E-07 0.17506E-07 0.23477E+01 c omega 0.13153E+02 1 0.40673E-08 0.17442E+01 0.68755E-02 c TempK 0.94475E+02 1 0.22414E-06 0.53572E-01 0.25698E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.286e-13 1.0616e-13 -1.3037e-17 -3.3224e-18 v Velocity[Y] -0.00014998 0.00014667 -1.0874e-09 -4.7301e-12 v Velocity[Z] -0.00014667 0.00014998 9.4981e-10 -2.0665e-12 v ǁVelocityǁ 2.2778e-10 0.00016291 1.0477e-05 5.9089e-06 v Pressure -0.00067142 0.016095 0.00083218 -2.0885e-20 v k 4.1645e-09 0.0020169 0.0014172 0.0017494 v omega 23.41 1.0313e+05 2672.5 507.37 v TempK 288 341.73 292.93 290.14 v Density 1.205 1.205 1.205 1.205 v TurbVisc 4.8966e-14 9.9962e-05 6.6533e-05 8.5023e-05 v CourantNb 1.5853e-09 0.00026009 1.4935e-05 7.7095e-06 v FourierNb 0.13215 0.6281 0.2085 0.17799 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9228 4.9228 0.00044062 -3.9405e-07 v volume_forces[Z] -4.9228 4.9228 -0.00044048 4.788e-07 v ǁvolume_forcesǁ 8.1206e-09 4.9244 0.44729 0.19311 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.14 290.28 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.017611 6.1258e-05 3.4572e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.13215 0.6281 0.20851 0.178 INSTANT 0.384237000E+00 TIME STEP NUMBER 399 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.52418E-05 0.26454E-02 Friction velocity uk : 0.52522E-05 0.26453E-02 Dimensionless distance yplus : 0.34974E-04 0.17599E-01 Friction thermal sca. tstar : -0.31402E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.24563E-04 0.12361E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.52418E-05 0.26454E-02 Friction velocity uk : 0.52522E-05 0.26453E-02 Dimensionless distance yplus : 0.34974E-04 0.17599E-01 Friction thermal sca. tstar : -0.31402E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.24563E-04 0.12361E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.35008E-08 3 0.31164E-06 0.63190E-12 0.15152E+01 c Velocity[X] 0.47379E-31 c Velocity[Y] 0.31594E-12 c Velocity[Z] 0.31596E-12 c Pressure 0.20389E-13 20 0.67368E-08 0.15990E-06 0.20474E+01 c k 0.61370E-06 2 0.85612E-07 0.17364E-07 0.23434E+01 c omega 0.13153E+02 1 0.40493E-08 0.17312E+01 0.68498E-02 c TempK 0.94475E+02 1 0.22337E-06 0.53375E-01 0.25651E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.2844e-13 1.0603e-13 -1.3023e-17 -3.3189e-18 v Velocity[Y] -0.00014985 0.00014653 -1.0877e-09 -4.7176e-12 v Velocity[Z] -0.00014653 0.00014985 9.4963e-10 -2.0692e-12 v ǁVelocityǁ 2.3095e-10 0.00016275 1.0473e-05 5.9106e-06 v Pressure -0.00067312 0.016115 0.00083359 -2.6719e-20 v k 4.1386e-09 0.0020122 0.0014138 0.0017455 v omega 23.367 1.0313e+05 2672.4 507.33 v TempK 288 341.73 292.93 290.14 v Density 1.205 1.205 1.205 1.205 v TurbVisc 4.866e-14 9.9943e-05 6.6497e-05 8.4985e-05 v CourantNb 1.5894e-09 0.00025978 1.4924e-05 7.707e-06 v FourierNb 0.13205 0.6281 0.20841 0.17792 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9229 4.923 0.00044098 -3.9468e-07 v volume_forces[Z] -4.9229 4.923 -0.00044083 4.7952e-07 v ǁvolume_forcesǁ 8.2342e-09 4.9245 0.44764 0.19336 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.15 290.29 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.017599 6.1225e-05 3.4553e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.13206 0.6281 0.20842 0.17792 INSTANT 0.385200000E+00 TIME STEP NUMBER 400 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.52938E-05 0.26438E-02 Friction velocity uk : 0.53039E-05 0.26437E-02 Dimensionless distance yplus : 0.35318E-04 0.17588E-01 Friction thermal sca. tstar : -0.34684E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.24805E-04 0.12353E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.52938E-05 0.26438E-02 Friction velocity uk : 0.53039E-05 0.26437E-02 Dimensionless distance yplus : 0.35318E-04 0.17588E-01 Friction thermal sca. tstar : -0.34684E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.24805E-04 0.12353E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34990E-08 3 0.31052E-06 0.62709E-12 0.15104E+01 c Velocity[X] 0.46935E-31 c Velocity[Y] 0.31354E-12 c Velocity[Z] 0.31355E-12 c Pressure 0.20306E-13 20 0.67159E-08 0.15924E-06 0.20421E+01 c k 0.61236E-06 2 0.85309E-07 0.17223E-07 0.23390E+01 c omega 0.13153E+02 1 0.40313E-08 0.17183E+01 0.68243E-02 c TempK 0.94476E+02 1 0.22260E-06 0.53179E-01 0.25603E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.2828e-13 1.059e-13 -1.3008e-17 -3.3155e-18 v Velocity[Y] -0.00014971 0.00014639 -1.0881e-09 -4.7051e-12 v Velocity[Z] -0.00014638 0.00014972 9.4945e-10 -2.072e-12 v ǁVelocityǁ 2.3415e-10 0.00016259 1.0469e-05 5.9124e-06 v Pressure -0.00067483 0.016135 0.000835 5.1968e-21 v k 4.1128e-09 0.0020076 0.0014105 0.0017415 v omega 23.324 1.0313e+05 2672.4 507.29 v TempK 288 341.73 292.93 290.15 v Density 1.205 1.205 1.205 1.205 v TurbVisc 4.8356e-14 9.9925e-05 6.6461e-05 8.4947e-05 v CourantNb 1.5935e-09 0.00025948 1.4913e-05 7.7047e-06 v FourierNb 0.13196 0.6281 0.20832 0.17784 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9231 4.9231 0.00044133 -3.953e-07 v volume_forces[Z] -4.9231 4.9231 -0.00044118 4.8023e-07 v ǁvolume_forcesǁ 8.3489e-09 4.9246 0.448 0.1936 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.15 290.29 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.017588 6.1193e-05 3.4533e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.13196 0.6281 0.20833 0.17785 INSTANT 0.386163000E+00 TIME STEP NUMBER 401 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.53454E-05 0.26421E-02 Friction velocity uk : 0.53554E-05 0.26420E-02 Dimensionless distance yplus : 0.35661E-04 0.17577E-01 Friction thermal sca. tstar : -0.39294E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.25046E-04 0.12345E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.53454E-05 0.26421E-02 Friction velocity uk : 0.53554E-05 0.26420E-02 Dimensionless distance yplus : 0.35661E-04 0.17577E-01 Friction thermal sca. tstar : -0.39294E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.25046E-04 0.12345E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34972E-08 3 0.30940E-06 0.62236E-12 0.15058E+01 c Velocity[X] 0.46497E-31 c Velocity[Y] 0.31117E-12 c Velocity[Z] 0.31119E-12 c Pressure 0.20216E-13 20 0.66968E-08 0.15853E-06 0.20368E+01 c k 0.61103E-06 2 0.85009E-07 0.17083E-07 0.23346E+01 c omega 0.13153E+02 1 0.40135E-08 0.17055E+01 0.67989E-02 c TempK 0.94477E+02 1 0.22183E-06 0.52984E-01 0.25556E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.2812e-13 1.0577e-13 -1.2994e-17 -3.312e-18 v Velocity[Y] -0.00014958 0.00014624 -1.0884e-09 -4.6926e-12 v Velocity[Z] -0.00014624 0.00014958 9.4925e-10 -2.0747e-12 v ǁVelocityǁ 2.3736e-10 0.00016243 1.0466e-05 5.9142e-06 v Pressure -0.00067654 0.016156 0.00083641 3.525e-20 v k 4.0873e-09 0.002003 0.0014071 0.0017376 v omega 23.281 1.0313e+05 2672.4 507.25 v TempK 288 341.73 292.94 290.15 v Density 1.205 1.205 1.205 1.205 v TurbVisc 4.8055e-14 9.9907e-05 6.6425e-05 8.4909e-05 v CourantNb 1.5976e-09 0.00025917 1.4902e-05 7.7024e-06 v FourierNb 0.13186 0.6281 0.20823 0.17776 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9232 4.9232 0.00044168 -3.9593e-07 v volume_forces[Z] -4.9232 4.9232 -0.00044153 4.8094e-07 v ǁvolume_forcesǁ 8.4644e-09 4.9248 0.44835 0.19385 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.16 290.29 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.017577 6.1161e-05 3.4514e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.13186 0.6281 0.20824 0.17777 INSTANT 0.387126000E+00 TIME STEP NUMBER 402 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.53967E-05 0.26405E-02 Friction velocity uk : 0.54064E-05 0.26404E-02 Dimensionless distance yplus : 0.36001E-04 0.17566E-01 Friction thermal sca. tstar : -0.46457E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.25285E-04 0.12338E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.53967E-05 0.26405E-02 Friction velocity uk : 0.54064E-05 0.26404E-02 Dimensionless distance yplus : 0.36001E-04 0.17566E-01 Friction thermal sca. tstar : -0.46457E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.25285E-04 0.12338E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34955E-08 3 0.39211E-06 0.61771E-12 0.15011E+01 c Velocity[X] 0.46067E-31 c Velocity[Y] 0.30885E-12 c Velocity[Z] 0.30886E-12 c Pressure 0.20124E-13 20 0.66769E-08 0.15780E-06 0.20316E+01 c k 0.60970E-06 2 0.84711E-07 0.16944E-07 0.23303E+01 c omega 0.13153E+02 1 0.39958E-08 0.16929E+01 0.67736E-02 c TempK 0.94477E+02 1 0.22107E-06 0.52790E-01 0.25509E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.2796e-13 1.0565e-13 -1.298e-17 -3.3086e-18 v Velocity[Y] -0.00014945 0.0001461 -1.0887e-09 -4.68e-12 v Velocity[Z] -0.0001461 0.00014945 9.4904e-10 -2.0772e-12 v ǁVelocityǁ 2.406e-10 0.00016228 1.0462e-05 5.9161e-06 v Pressure -0.00067825 0.016176 0.00083782 3.9172e-20 v k 4.062e-09 0.0019983 0.0014037 0.0017336 v omega 23.238 1.0313e+05 2672.4 507.21 v TempK 288 341.74 292.94 290.15 v Density 1.205 1.205 1.205 1.205 v TurbVisc 4.7757e-14 9.9888e-05 6.639e-05 8.4872e-05 v CourantNb 1.6016e-09 0.00025886 1.4892e-05 7.7001e-06 v FourierNb 0.13177 0.6281 0.20814 0.17769 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9233 4.9234 0.00044203 -3.9655e-07 v volume_forces[Z] -4.9233 4.9234 -0.00044188 4.8165e-07 v ǁvolume_forcesǁ 8.5807e-09 4.9249 0.4487 0.19409 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.16 290.3 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.017566 6.1129e-05 3.4495e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.13177 0.6281 0.20815 0.17769 INSTANT 0.388089000E+00 TIME STEP NUMBER 403 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.54476E-05 0.26388E-02 Friction velocity uk : 0.54572E-05 0.26387E-02 Dimensionless distance yplus : 0.36339E-04 0.17556E-01 Friction thermal sca. tstar : -0.59946E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.25522E-04 0.12330E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.54476E-05 0.26388E-02 Friction velocity uk : 0.54572E-05 0.26387E-02 Dimensionless distance yplus : 0.36339E-04 0.17556E-01 Friction thermal sca. tstar : -0.59946E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.25522E-04 0.12330E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34938E-08 3 0.30729E-06 0.61314E-12 0.14966E+01 c Velocity[X] 0.45641E-31 c Velocity[Y] 0.30656E-12 c Velocity[Z] 0.30658E-12 c Pressure 0.20094E-13 20 0.66724E-08 0.15756E-06 0.20263E+01 c k 0.60837E-06 2 0.84415E-07 0.16807E-07 0.23260E+01 c omega 0.13153E+02 1 0.39782E-08 0.16803E+01 0.67484E-02 c TempK 0.94478E+02 1 0.22031E-06 0.52598E-01 0.25462E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.278e-13 1.0552e-13 -1.2965e-17 -3.3052e-18 v Velocity[Y] -0.00014932 0.00014596 -1.089e-09 -4.6676e-12 v Velocity[Z] -0.00014596 0.00014932 9.4883e-10 -2.0798e-12 v ǁVelocityǁ 2.4386e-10 0.00016212 1.0458e-05 5.918e-06 v Pressure -0.00067996 0.016196 0.00083922 -8.4031e-20 v k 4.0369e-09 0.0019938 0.0014004 0.0017297 v omega 23.195 1.0313e+05 2672.3 507.17 v TempK 288 341.74 292.95 290.15 v Density 1.205 1.205 1.205 1.205 v TurbVisc 4.7461e-14 9.987e-05 6.6354e-05 8.4834e-05 v CourantNb 1.6057e-09 0.00025856 1.4881e-05 7.6979e-06 v FourierNb 0.13167 0.6281 0.20805 0.17761 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9235 4.9235 0.00044238 -3.9717e-07 v volume_forces[Z] -4.9235 4.9235 -0.00044223 4.8235e-07 v ǁvolume_forcesǁ 8.6978e-09 4.925 0.44905 0.19433 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.16 290.3 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.017556 6.1097e-05 3.4476e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.13167 0.6281 0.20807 0.17762 INSTANT 0.389052000E+00 TIME STEP NUMBER 404 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.54982E-05 0.26372E-02 Friction velocity uk : 0.55076E-05 0.26371E-02 Dimensionless distance yplus : 0.36675E-04 0.17545E-01 Friction thermal sca. tstar : -0.10397E+05 0.00000E+00 Dim-less thermal sca. tplus : 0.25758E-04 0.12322E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.54982E-05 0.26372E-02 Friction velocity uk : 0.55076E-05 0.26371E-02 Dimensionless distance yplus : 0.36675E-04 0.17545E-01 Friction thermal sca. tstar : -0.10397E+05 0.00000E+00 Dim-less thermal sca. tplus : 0.25758E-04 0.12322E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34921E-08 3 0.30608E-06 0.60865E-12 0.14921E+01 c Velocity[X] 0.45223E-31 c Velocity[Y] 0.30432E-12 c Velocity[Z] 0.30433E-12 c Pressure 0.19949E-13 20 0.66418E-08 0.15641E-06 0.20211E+01 c k 0.60705E-06 2 0.84121E-07 0.16672E-07 0.23216E+01 c omega 0.13153E+02 1 0.39607E-08 0.16679E+01 0.67234E-02 c TempK 0.94478E+02 1 0.21956E-06 0.52406E-01 0.25416E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.2764e-13 1.054e-13 -1.2951e-17 -3.3018e-18 v Velocity[Y] -0.00014919 0.00014582 -1.0893e-09 -4.6552e-12 v Velocity[Z] -0.00014582 0.00014919 9.486e-10 -2.0826e-12 v ǁVelocityǁ 2.4715e-10 0.00016196 1.0454e-05 5.9199e-06 v Pressure -0.00068166 0.016217 0.00084062 6.6088e-20 v k 4.012e-09 0.0019892 0.0013971 0.0017259 v omega 23.153 1.0313e+05 2672.3 507.13 v TempK 288 341.74 292.95 290.16 v Density 1.205 1.205 1.205 1.205 v TurbVisc 4.7168e-14 9.9852e-05 6.6319e-05 8.4796e-05 v CourantNb 1.6098e-09 0.00025826 1.4871e-05 7.6958e-06 v FourierNb 0.13157 0.6281 0.20796 0.17753 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9236 4.9236 0.00044273 -3.9779e-07 v volume_forces[Z] -4.9236 4.9236 -0.00044258 4.8306e-07 v ǁvolume_forcesǁ 8.8157e-09 4.9252 0.4494 0.19458 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.17 290.3 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.017545 6.1064e-05 3.4456e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.13158 0.6281 0.20798 0.17754 INSTANT 0.390015000E+00 TIME STEP NUMBER 405 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.55485E-05 0.26356E-02 Friction velocity uk : 0.55577E-05 0.26355E-02 Dimensionless distance yplus : 0.37008E-04 0.17534E-01 Friction thermal sca. tstar : -0.11105E+05 0.00000E+00 Dim-less thermal sca. tplus : 0.25992E-04 0.12315E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.55485E-05 0.26356E-02 Friction velocity uk : 0.55577E-05 0.26355E-02 Dimensionless distance yplus : 0.37008E-04 0.17534E-01 Friction thermal sca. tstar : -0.11105E+05 0.00000E+00 Dim-less thermal sca. tplus : 0.25992E-04 0.12315E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34904E-08 3 0.30500E-06 0.60423E-12 0.14876E+01 c Velocity[X] 0.44811E-31 c Velocity[Y] 0.30211E-12 c Velocity[Z] 0.30212E-12 c Pressure 0.19871E-13 20 0.66239E-08 0.15580E-06 0.20159E+01 c k 0.60574E-06 2 0.83829E-07 0.16537E-07 0.23174E+01 c omega 0.13153E+02 1 0.39433E-08 0.16556E+01 0.66986E-02 c TempK 0.94479E+02 1 0.21881E-06 0.52216E-01 0.25369E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.2748e-13 1.0527e-13 -1.2937e-17 -3.2984e-18 v Velocity[Y] -0.00014906 0.00014568 -1.0895e-09 -4.6429e-12 v Velocity[Z] -0.00014568 0.00014906 9.4836e-10 -2.0852e-12 v ǁVelocityǁ 2.5045e-10 0.00016181 1.0451e-05 5.9219e-06 v Pressure -0.00068337 0.016237 0.00084202 6.1087e-20 v k 3.9873e-09 0.0019846 0.0013938 0.001722 v omega 23.111 1.0313e+05 2672.3 507.1 v TempK 288 341.74 292.95 290.16 v Density 1.205 1.205 1.205 1.205 v TurbVisc 4.6877e-14 9.9834e-05 6.6283e-05 8.4759e-05 v CourantNb 1.6139e-09 0.00025796 1.486e-05 7.6937e-06 v FourierNb 0.13148 0.6281 0.20788 0.17746 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9237 4.9238 0.00044307 -3.9841e-07 v volume_forces[Z] -4.9237 4.9238 -0.00044293 4.8376e-07 v ǁvolume_forcesǁ 8.9344e-09 4.9253 0.44975 0.19482 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.17 290.3 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.017534 6.1033e-05 3.4437e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.13148 0.6281 0.20789 0.17747 INSTANT 0.390978000E+00 TIME STEP NUMBER 406 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.55984E-05 0.26339E-02 Friction velocity uk : 0.56075E-05 0.26338E-02 Dimensionless distance yplus : 0.37340E-04 0.17523E-01 Friction thermal sca. tstar : -0.61058E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.26225E-04 0.12307E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.55984E-05 0.26339E-02 Friction velocity uk : 0.56075E-05 0.26338E-02 Dimensionless distance yplus : 0.37340E-04 0.17523E-01 Friction thermal sca. tstar : -0.61058E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.26225E-04 0.12307E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34888E-08 3 0.30403E-06 0.59989E-12 0.14832E+01 c Velocity[X] 0.44405E-31 c Velocity[Y] 0.29994E-12 c Velocity[Z] 0.29995E-12 c Pressure 0.19857E-13 20 0.66099E-08 0.15568E-06 0.20108E+01 c k 0.60443E-06 2 0.83538E-07 0.16404E-07 0.23131E+01 c omega 0.13153E+02 1 0.39261E-08 0.16434E+01 0.66739E-02 c TempK 0.94480E+02 1 0.21807E-06 0.52027E-01 0.25323E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.2733e-13 1.0515e-13 -1.2923e-17 -3.295e-18 v Velocity[Y] -0.00014893 0.00014554 -1.0898e-09 -4.6307e-12 v Velocity[Z] -0.00014554 0.00014894 9.4811e-10 -2.0879e-12 v ǁVelocityǁ 2.5377e-10 0.00016165 1.0447e-05 5.924e-06 v Pressure -0.00068508 0.016257 0.00084342 1.1815e-20 v k 3.9628e-09 0.0019801 0.0013905 0.0017181 v omega 23.069 1.0313e+05 2672.2 507.06 v TempK 288 341.74 292.96 290.16 v Density 1.205 1.205 1.205 1.205 v TurbVisc 4.6588e-14 9.9816e-05 6.6248e-05 8.4721e-05 v CourantNb 1.6179e-09 0.00025766 1.485e-05 7.6917e-06 v FourierNb 0.13138 0.6281 0.20779 0.17738 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9239 4.9239 0.00044342 -3.9902e-07 v volume_forces[Z] -4.9239 4.9239 -0.00044327 4.8446e-07 v ǁvolume_forcesǁ 9.0538e-09 4.9254 0.4501 0.19506 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.18 290.31 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.017523 6.1004e-05 3.442e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.13138 0.6281 0.2078 0.17739 INSTANT 0.391941000E+00 TIME STEP NUMBER 407 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.56481E-05 0.26323E-02 Friction velocity uk : 0.56570E-05 0.26322E-02 Dimensionless distance yplus : 0.37669E-04 0.17512E-01 Friction thermal sca. tstar : -0.46824E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.26456E-04 0.12300E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.56481E-05 0.26323E-02 Friction velocity uk : 0.56570E-05 0.26322E-02 Dimensionless distance yplus : 0.37669E-04 0.17512E-01 Friction thermal sca. tstar : -0.46824E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.26456E-04 0.12300E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34872E-08 3 0.30285E-06 0.59562E-12 0.14789E+01 c Velocity[X] 0.44004E-31 c Velocity[Y] 0.29780E-12 c Velocity[Z] 0.29782E-12 c Pressure 0.19711E-13 20 0.65840E-08 0.15453E-06 0.20057E+01 c k 0.60313E-06 2 0.83250E-07 0.16273E-07 0.23088E+01 c omega 0.13153E+02 1 0.39089E-08 0.16313E+01 0.66493E-02 c TempK 0.94480E+02 1 0.21733E-06 0.51839E-01 0.25277E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.2717e-13 1.0502e-13 -1.2909e-17 -3.2916e-18 v Velocity[Y] -0.00014881 0.0001454 -1.09e-09 -4.6183e-12 v Velocity[Z] -0.0001454 0.00014881 9.4785e-10 -2.0904e-12 v ǁVelocityǁ 2.5712e-10 0.0001615 1.0444e-05 5.9261e-06 v Pressure -0.00068679 0.016277 0.00084482 -2.9857e-20 v k 3.9385e-09 0.0019756 0.0013872 0.0017143 v omega 23.027 1.0313e+05 2672.2 507.02 v TempK 288 341.74 292.96 290.16 v Density 1.205 1.205 1.205 1.205 v TurbVisc 4.6302e-14 9.9798e-05 6.6213e-05 8.4684e-05 v CourantNb 1.622e-09 0.00025737 1.484e-05 7.6898e-06 v FourierNb 0.13129 0.6281 0.2077 0.17731 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.924 4.924 0.00044377 -3.9963e-07 v volume_forces[Z] -4.924 4.924 -0.00044362 4.8516e-07 v ǁvolume_forcesǁ 9.1739e-09 4.9256 0.45044 0.19531 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.18 290.31 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.017512 6.0974e-05 3.4402e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.13129 0.6281 0.20772 0.17732 INSTANT 0.392904000E+00 TIME STEP NUMBER 408 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.56975E-05 0.26307E-02 Friction velocity uk : 0.57062E-05 0.26306E-02 Dimensionless distance yplus : 0.37997E-04 0.17502E-01 Friction thermal sca. tstar : -0.39385E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.26687E-04 0.12292E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.56975E-05 0.26307E-02 Friction velocity uk : 0.57062E-05 0.26306E-02 Dimensionless distance yplus : 0.37997E-04 0.17502E-01 Friction thermal sca. tstar : -0.39385E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.26687E-04 0.12292E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34856E-08 3 0.30180E-06 0.59142E-12 0.14746E+01 c Velocity[X] 0.43610E-31 c Velocity[Y] 0.29571E-12 c Velocity[Z] 0.29572E-12 c Pressure 0.19646E-13 20 0.65633E-08 0.15402E-06 0.20006E+01 c k 0.60183E-06 2 0.82964E-07 0.16142E-07 0.23046E+01 c omega 0.13153E+02 1 0.38918E-08 0.16193E+01 0.66248E-02 c TempK 0.94481E+02 1 0.21659E-06 0.51652E-01 0.25231E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.2702e-13 1.049e-13 -1.2895e-17 -3.2883e-18 v Velocity[Y] -0.00014868 0.00014526 -1.0903e-09 -4.6061e-12 v Velocity[Z] -0.00014526 0.00014868 9.4759e-10 -2.093e-12 v ǁVelocityǁ 2.6048e-10 0.00016135 1.0441e-05 5.9282e-06 v Pressure -0.00068849 0.016297 0.00084622 1.8581e-20 v k 3.9144e-09 0.001971 0.0013839 0.0017105 v omega 22.985 1.0313e+05 2672.2 506.98 v TempK 288 341.74 292.96 290.17 v Density 1.205 1.205 1.205 1.205 v TurbVisc 4.6018e-14 9.9779e-05 6.6177e-05 8.4647e-05 v CourantNb 1.6261e-09 0.00025707 1.483e-05 7.6879e-06 v FourierNb 0.13119 0.6281 0.20762 0.17723 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9241 4.9242 0.00044411 -4.0024e-07 v volume_forces[Z] -4.9241 4.9242 -0.00044397 4.8585e-07 v ǁvolume_forcesǁ 9.2949e-09 4.9257 0.45079 0.19555 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.18 290.31 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.017502 6.0945e-05 3.4384e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.13119 0.6281 0.20763 0.17724 INSTANT 0.393867000E+00 TIME STEP NUMBER 409 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.57466E-05 0.26291E-02 Friction velocity uk : 0.57551E-05 0.26290E-02 Dimensionless distance yplus : 0.38323E-04 0.17491E-01 Friction thermal sca. tstar : -0.34628E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.26916E-04 0.12285E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.57466E-05 0.26291E-02 Friction velocity uk : 0.57551E-05 0.26290E-02 Dimensionless distance yplus : 0.38323E-04 0.17491E-01 Friction thermal sca. tstar : -0.34628E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.26916E-04 0.12285E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34840E-08 3 0.30073E-06 0.58730E-12 0.14704E+01 c Velocity[X] 0.43221E-31 c Velocity[Y] 0.29364E-12 c Velocity[Z] 0.29365E-12 c Pressure 0.19551E-13 20 0.65481E-08 0.15326E-06 0.19955E+01 c k 0.60054E-06 2 0.82679E-07 0.16013E-07 0.23004E+01 c omega 0.13153E+02 1 0.38749E-08 0.16074E+01 0.66005E-02 c TempK 0.94482E+02 1 0.21586E-06 0.51467E-01 0.25185E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.2686e-13 1.0478e-13 -1.2881e-17 -3.2849e-18 v Velocity[Y] -0.00014855 0.00014513 -1.0905e-09 -4.5941e-12 v Velocity[Z] -0.00014512 0.00014856 9.4731e-10 -2.0955e-12 v ǁVelocityǁ 2.6387e-10 0.00016119 1.0438e-05 5.9304e-06 v Pressure -0.0006902 0.016318 0.00084761 8.761e-20 v k 3.8905e-09 0.0019666 0.0013807 0.0017067 v omega 22.943 1.0313e+05 2672.1 506.94 v TempK 288 341.75 292.97 290.17 v Density 1.205 1.205 1.205 1.205 v TurbVisc 4.5737e-14 9.9761e-05 6.6142e-05 8.4609e-05 v CourantNb 1.6301e-09 0.00025678 1.482e-05 7.686e-06 v FourierNb 0.1311 0.6281 0.20753 0.17716 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9243 4.9243 0.00044446 -4.0085e-07 v volume_forces[Z] -4.9243 4.9243 -0.00044431 4.8655e-07 v ǁvolume_forcesǁ 9.4165e-09 4.9258 0.45114 0.19579 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.19 290.31 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.017491 6.0915e-05 3.4366e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.1311 0.6281 0.20754 0.17717 INSTANT 0.394830000E+00 TIME STEP NUMBER 410 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.57954E-05 0.26275E-02 Friction velocity uk : 0.58038E-05 0.26274E-02 Dimensionless distance yplus : 0.38647E-04 0.17480E-01 Friction thermal sca. tstar : -0.31250E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.27143E-04 0.12277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.57954E-05 0.26275E-02 Friction velocity uk : 0.58038E-05 0.26274E-02 Dimensionless distance yplus : 0.38647E-04 0.17480E-01 Friction thermal sca. tstar : -0.31250E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.27143E-04 0.12277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34825E-08 3 0.29967E-06 0.58324E-12 0.14662E+01 c Velocity[X] 0.42837E-31 c Velocity[Y] 0.29161E-12 c Velocity[Z] 0.29163E-12 c Pressure 0.19450E-13 20 0.65318E-08 0.15247E-06 0.19904E+01 c k 0.59925E-06 2 0.82397E-07 0.15886E-07 0.22961E+01 c omega 0.13153E+02 1 0.38580E-08 0.15957E+01 0.65763E-02 c TempK 0.94482E+02 1 0.21514E-06 0.51282E-01 0.25140E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.2671e-13 1.0466e-13 -1.2867e-17 -3.2816e-18 v Velocity[Y] -0.00014843 0.00014499 -1.0907e-09 -4.5819e-12 v Velocity[Z] -0.00014499 0.00014843 9.4702e-10 -2.098e-12 v ǁVelocityǁ 2.6727e-10 0.00016104 1.0434e-05 5.9326e-06 v Pressure -0.00069191 0.016338 0.000849 -2.6965e-20 v k 3.8668e-09 0.0019621 0.0013774 0.0017029 v omega 22.902 1.0313e+05 2672.1 506.91 v TempK 288 341.75 292.97 290.17 v Density 1.205 1.205 1.205 1.205 v TurbVisc 4.5458e-14 9.9743e-05 6.6107e-05 8.4572e-05 v CourantNb 1.6342e-09 0.00025649 1.481e-05 7.6842e-06 v FourierNb 0.131 0.6281 0.20744 0.17708 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9244 4.9244 0.0004448 -4.0146e-07 v volume_forces[Z] -4.9244 4.9244 -0.00044466 4.8724e-07 v ǁvolume_forcesǁ 9.5388e-09 4.9259 0.45148 0.19603 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.19 290.32 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.01748 6.0885e-05 3.4348e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.131 0.6281 0.20746 0.17709 INSTANT 0.395793000E+00 TIME STEP NUMBER 411 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.58439E-05 0.26259E-02 Friction velocity uk : 0.58522E-05 0.26258E-02 Dimensionless distance yplus : 0.38969E-04 0.17470E-01 Friction thermal sca. tstar : -0.28692E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.27369E-04 0.12270E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.58439E-05 0.26259E-02 Friction velocity uk : 0.58522E-05 0.26258E-02 Dimensionless distance yplus : 0.38969E-04 0.17470E-01 Friction thermal sca. tstar : -0.28692E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.27369E-04 0.12270E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34810E-08 3 0.29864E-06 0.57925E-12 0.14621E+01 c Velocity[X] 0.42460E-31 c Velocity[Y] 0.28962E-12 c Velocity[Z] 0.28963E-12 c Pressure 0.19404E-13 20 0.65108E-08 0.15210E-06 0.19854E+01 c k 0.59797E-06 2 0.82116E-07 0.15759E-07 0.22919E+01 c omega 0.13153E+02 1 0.38413E-08 0.15840E+01 0.65522E-02 c TempK 0.94483E+02 1 0.21441E-06 0.51098E-01 0.25095E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.2656e-13 1.0454e-13 -1.2853e-17 -3.2783e-18 v Velocity[Y] -0.0001483 0.00014485 -1.091e-09 -4.5698e-12 v Velocity[Z] -0.00014485 0.0001483 9.4672e-10 -2.1006e-12 v ǁVelocityǁ 2.7069e-10 0.00016089 1.0431e-05 5.9349e-06 v Pressure -0.00069361 0.016358 0.0008504 -1.5737e-20 v k 3.8433e-09 0.0019576 0.0013742 0.0016991 v omega 22.86 1.0313e+05 2672.1 506.87 v TempK 288 341.75 292.98 290.18 v Density 1.205 1.205 1.205 1.205 v TurbVisc 4.5181e-14 9.9725e-05 6.6072e-05 8.4535e-05 v CourantNb 1.6383e-09 0.0002562 1.48e-05 7.6825e-06 v FourierNb 0.1309 0.6281 0.20736 0.17701 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9245 4.9246 0.00044515 -4.0207e-07 v volume_forces[Z] -4.9245 4.9246 -0.000445 4.8793e-07 v ǁvolume_forcesǁ 9.6619e-09 4.9261 0.45183 0.19628 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.19 290.32 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.01747 6.0855e-05 3.433e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.13091 0.6281 0.20737 0.17702 INSTANT 0.396756000E+00 TIME STEP NUMBER 412 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.58922E-05 0.26243E-02 Friction velocity uk : 0.59003E-05 0.26242E-02 Dimensionless distance yplus : 0.39290E-04 0.17459E-01 Friction thermal sca. tstar : -0.26667E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.27594E-04 0.12262E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.58922E-05 0.26243E-02 Friction velocity uk : 0.59003E-05 0.26242E-02 Dimensionless distance yplus : 0.39290E-04 0.17459E-01 Friction thermal sca. tstar : -0.26667E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.27594E-04 0.12262E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34795E-08 3 0.29759E-06 0.57532E-12 0.14580E+01 c Velocity[X] 0.42087E-31 c Velocity[Y] 0.28766E-12 c Velocity[Z] 0.28767E-12 c Pressure 0.19290E-13 20 0.64965E-08 0.15121E-06 0.19804E+01 c k 0.59669E-06 2 0.81837E-07 0.15634E-07 0.22878E+01 c omega 0.13153E+02 1 0.38246E-08 0.15725E+01 0.65283E-02 c TempK 0.94484E+02 1 0.21369E-06 0.50916E-01 0.25050E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.2641e-13 1.0442e-13 -1.284e-17 -3.2749e-18 v Velocity[Y] -0.00014818 0.00014472 -1.0912e-09 -4.5579e-12 v Velocity[Z] -0.00014471 0.00014818 9.4641e-10 -2.103e-12 v ǁVelocityǁ 2.7414e-10 0.00016074 1.0428e-05 5.9372e-06 v Pressure -0.00069532 0.016378 0.00085178 6.6431e-20 v k 3.82e-09 0.0019532 0.001371 0.0016953 v omega 22.819 1.0313e+05 2672 506.83 v TempK 288 341.75 292.98 290.18 v Density 1.205 1.205 1.205 1.205 v TurbVisc 4.4907e-14 9.9708e-05 6.6038e-05 8.4498e-05 v CourantNb 1.6423e-09 0.00025591 1.4791e-05 7.6808e-06 v FourierNb 0.13081 0.6281 0.20727 0.17694 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9247 4.9247 0.00044549 -4.0267e-07 v volume_forces[Z] -4.9247 4.9247 -0.00044535 4.8862e-07 v ǁvolume_forcesǁ 9.7856e-09 4.9262 0.45217 0.19652 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.2 290.32 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.017459 6.0826e-05 3.4312e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.13081 0.6281 0.20729 0.17694 INSTANT 0.397719000E+00 TIME STEP NUMBER 413 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.59402E-05 0.26228E-02 Friction velocity uk : 0.59482E-05 0.26227E-02 Dimensionless distance yplus : 0.39608E-04 0.17449E-01 Friction thermal sca. tstar : -0.25013E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.27818E-04 0.12255E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.59402E-05 0.26228E-02 Friction velocity uk : 0.59482E-05 0.26227E-02 Dimensionless distance yplus : 0.39608E-04 0.17449E-01 Friction thermal sca. tstar : -0.25013E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.27818E-04 0.12255E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34781E-08 3 0.29657E-06 0.57147E-12 0.14540E+01 c Velocity[X] 0.41719E-31 c Velocity[Y] 0.28573E-12 c Velocity[Z] 0.28574E-12 c Pressure 0.19230E-13 20 0.64802E-08 0.15073E-06 0.19754E+01 c k 0.59542E-06 2 0.81560E-07 0.15510E-07 0.22836E+01 c omega 0.13153E+02 1 0.38081E-08 0.15610E+01 0.65045E-02 c TempK 0.94484E+02 1 0.21298E-06 0.50735E-01 0.25005E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.2626e-13 1.043e-13 -1.2826e-17 -3.2716e-18 v Velocity[Y] -0.00014805 0.00014458 -1.0913e-09 -4.546e-12 v Velocity[Z] -0.00014458 0.00014806 9.4609e-10 -2.1055e-12 v ǁVelocityǁ 2.776e-10 0.00016059 1.0425e-05 5.9396e-06 v Pressure -0.00069703 0.016398 0.00085317 -3.1279e-20 v k 3.7969e-09 0.0019488 0.0013678 0.0016916 v omega 22.778 1.0313e+05 2672 506.79 v TempK 288 341.75 292.98 290.18 v Density 1.205 1.205 1.205 1.205 v TurbVisc 4.4634e-14 9.969e-05 6.6003e-05 8.4461e-05 v CourantNb 1.6464e-09 0.00025562 1.4781e-05 7.6792e-06 v FourierNb 0.13072 0.6281 0.20719 0.17686 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9248 4.9248 0.00044584 -4.0328e-07 v volume_forces[Z] -4.9248 4.9248 -0.00044569 4.8931e-07 v ǁvolume_forcesǁ 9.91e-09 4.9263 0.45252 0.19676 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.2 290.33 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.017449 6.0796e-05 3.4294e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.13072 0.6281 0.2072 0.17687 INSTANT 0.398682000E+00 TIME STEP NUMBER 414 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.59880E-05 0.26212E-02 Friction velocity uk : 0.59958E-05 0.26211E-02 Dimensionless distance yplus : 0.39925E-04 0.17438E-01 Friction thermal sca. tstar : -0.23628E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.28041E-04 0.12248E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.59880E-05 0.26212E-02 Friction velocity uk : 0.59958E-05 0.26211E-02 Dimensionless distance yplus : 0.39925E-04 0.17438E-01 Friction thermal sca. tstar : -0.23628E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.28041E-04 0.12248E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34767E-08 3 0.29555E-06 0.56767E-12 0.14501E+01 c Velocity[X] 0.41358E-31 c Velocity[Y] 0.28383E-12 c Velocity[Z] 0.28384E-12 c Pressure 0.19155E-13 20 0.64629E-08 0.15014E-06 0.19705E+01 c k 0.59415E-06 2 0.81285E-07 0.15387E-07 0.22795E+01 c omega 0.13153E+02 1 0.37916E-08 0.15497E+01 0.64808E-02 c TempK 0.94485E+02 1 0.21227E-06 0.50554E-01 0.24960E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.2611e-13 1.0418e-13 -1.2812e-17 -3.2684e-18 v Velocity[Y] -0.00014793 0.00014445 -1.0915e-09 -4.534e-12 v Velocity[Z] -0.00014445 0.00014793 9.4576e-10 -2.1079e-12 v ǁVelocityǁ 2.8107e-10 0.00016044 1.0422e-05 5.942e-06 v Pressure -0.00069873 0.016418 0.00085456 -2.5788e-20 v k 3.774e-09 0.0019443 0.0013646 0.0016878 v omega 22.737 1.0313e+05 2672 506.76 v TempK 288 341.75 292.99 290.18 v Density 1.205 1.205 1.205 1.205 v TurbVisc 4.4364e-14 9.9672e-05 6.5968e-05 8.4424e-05 v CourantNb 1.6505e-09 0.00025533 1.4772e-05 7.6776e-06 v FourierNb 0.13062 0.6281 0.2071 0.17679 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9249 4.9249 0.00044618 -4.0388e-07 v volume_forces[Z] -4.9249 4.9249 -0.00044603 4.8999e-07 v ǁvolume_forcesǁ 1.0035e-08 4.9265 0.45286 0.197 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.21 290.33 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.017438 6.0766e-05 3.4277e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.13062 0.6281 0.20712 0.1768 INSTANT 0.399645000E+00 TIME STEP NUMBER 415 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.60355E-05 0.26196E-02 Friction velocity uk : 0.60432E-05 0.26195E-02 Dimensionless distance yplus : 0.40241E-04 0.17428E-01 Friction thermal sca. tstar : -0.22446E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.28263E-04 0.12240E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.60355E-05 0.26196E-02 Friction velocity uk : 0.60432E-05 0.26195E-02 Dimensionless distance yplus : 0.40241E-04 0.17428E-01 Friction thermal sca. tstar : -0.22446E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.28263E-04 0.12240E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34753E-08 3 0.29452E-06 0.56394E-12 0.14462E+01 c Velocity[X] 0.41001E-31 c Velocity[Y] 0.28196E-12 c Velocity[Z] 0.28198E-12 c Pressure 0.19058E-13 20 0.64450E-08 0.14937E-06 0.19655E+01 c k 0.59289E-06 2 0.81012E-07 0.15265E-07 0.22753E+01 c omega 0.13153E+02 1 0.37753E-08 0.15384E+01 0.64572E-02 c TempK 0.94486E+02 1 0.21156E-06 0.50375E-01 0.24915E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.2596e-13 1.0406e-13 -1.2799e-17 -3.2651e-18 v Velocity[Y] -0.00014781 0.00014432 -1.0917e-09 -4.5222e-12 v Velocity[Z] -0.00014431 0.00014781 9.4542e-10 -2.1105e-12 v ǁVelocityǁ 2.8457e-10 0.0001603 1.0419e-05 5.9444e-06 v Pressure -0.00070044 0.016438 0.00085594 7.5991e-21 v k 3.7512e-09 0.0019399 0.0013614 0.0016841 v omega 22.696 1.0313e+05 2672 506.72 v TempK 288 341.75 292.99 290.19 v Density 1.205 1.205 1.205 1.205 v TurbVisc 4.4096e-14 9.9654e-05 6.5934e-05 8.4388e-05 v CourantNb 1.6545e-09 0.00025505 1.4762e-05 7.6761e-06 v FourierNb 0.13053 0.6281 0.20702 0.17672 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.925 4.9251 0.00044652 -4.0448e-07 v volume_forces[Z] -4.925 4.9251 -0.00044637 4.9067e-07 v ǁvolume_forcesǁ 1.0161e-08 4.9266 0.4532 0.19724 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.21 290.33 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.017428 6.0737e-05 3.4259e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.13053 0.6281 0.20703 0.17672 INSTANT 0.400608000E+00 TIME STEP NUMBER 416 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.60827E-05 0.26181E-02 Friction velocity uk : 0.60903E-05 0.26180E-02 Dimensionless distance yplus : 0.40555E-04 0.17418E-01 Friction thermal sca. tstar : -0.21422E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.28483E-04 0.12233E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.60827E-05 0.26181E-02 Friction velocity uk : 0.60903E-05 0.26180E-02 Dimensionless distance yplus : 0.40555E-04 0.17418E-01 Friction thermal sca. tstar : -0.21422E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.28483E-04 0.12233E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34739E-08 3 0.29351E-06 0.56027E-12 0.14423E+01 c Velocity[X] 0.40649E-31 c Velocity[Y] 0.28013E-12 c Velocity[Z] 0.28014E-12 c Pressure 0.18991E-13 20 0.64289E-08 0.14884E-06 0.19606E+01 c k 0.59163E-06 2 0.80740E-07 0.15145E-07 0.22712E+01 c omega 0.13153E+02 1 0.37590E-08 0.15273E+01 0.64338E-02 c TempK 0.94486E+02 1 0.21086E-06 0.50197E-01 0.24871E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.2581e-13 1.0394e-13 -1.2785e-17 -3.2618e-18 v Velocity[Y] -0.00014769 0.00014418 -1.0919e-09 -4.5103e-12 v Velocity[Z] -0.00014418 0.00014769 9.4507e-10 -2.113e-12 v ǁVelocityǁ 2.8808e-10 0.00016015 1.0417e-05 5.9469e-06 v Pressure -0.00070215 0.016458 0.00085733 -4.3437e-20 v k 3.7287e-09 0.0019356 0.0013583 0.0016804 v omega 22.656 1.0313e+05 2671.9 506.68 v TempK 288 341.76 293 290.19 v Density 1.205 1.205 1.205 1.205 v TurbVisc 4.383e-14 9.9636e-05 6.5899e-05 8.4351e-05 v CourantNb 1.6586e-09 0.00025477 1.4753e-05 7.6746e-06 v FourierNb 0.13043 0.6281 0.20693 0.17664 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9252 4.9252 0.00044686 -4.0508e-07 v volume_forces[Z] -4.9252 4.9252 -0.00044671 4.9135e-07 v ǁvolume_forcesǁ 1.0287e-08 4.9267 0.45354 0.19748 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.21 290.33 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.017418 6.0708e-05 3.4241e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.13043 0.6281 0.20695 0.17665 INSTANT 0.401571000E+00 TIME STEP NUMBER 417 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.61298E-05 0.26165E-02 Friction velocity uk : 0.61372E-05 0.26164E-02 Dimensionless distance yplus : 0.40867E-04 0.17407E-01 Friction thermal sca. tstar : -0.20523E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.28702E-04 0.12226E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.61298E-05 0.26165E-02 Friction velocity uk : 0.61372E-05 0.26164E-02 Dimensionless distance yplus : 0.40867E-04 0.17407E-01 Friction thermal sca. tstar : -0.20523E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.28702E-04 0.12226E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34725E-08 3 0.29251E-06 0.55666E-12 0.14385E+01 c Velocity[X] 0.40302E-31 c Velocity[Y] 0.27833E-12 c Velocity[Z] 0.27834E-12 c Pressure 0.18904E-13 20 0.64101E-08 0.14815E-06 0.19557E+01 c k 0.59037E-06 2 0.80470E-07 0.15025E-07 0.22671E+01 c omega 0.13153E+02 1 0.37429E-08 0.15163E+01 0.64105E-02 c TempK 0.94487E+02 1 0.21016E-06 0.50020E-01 0.24827E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.2566e-13 1.0382e-13 -1.2771e-17 -3.2586e-18 v Velocity[Y] -0.00014756 0.00014405 -1.092e-09 -4.4984e-12 v Velocity[Z] -0.00014405 0.00014757 9.4471e-10 -2.1154e-12 v ǁVelocityǁ 2.9162e-10 0.00016 1.0414e-05 5.9494e-06 v Pressure -0.00070385 0.016478 0.00085871 -1.3433e-20 v k 3.7063e-09 0.0019312 0.0013551 0.0016767 v omega 22.615 1.0313e+05 2671.9 506.65 v TempK 288 341.76 293 290.19 v Density 1.205 1.205 1.205 1.205 v TurbVisc 4.3567e-14 9.9618e-05 6.5865e-05 8.4314e-05 v CourantNb 1.6626e-09 0.00025449 1.4744e-05 7.6732e-06 v FourierNb 0.13034 0.6281 0.20685 0.17657 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9253 4.9253 0.0004472 -4.0567e-07 v volume_forces[Z] -4.9253 4.9253 -0.00044705 4.9203e-07 v ǁvolume_forcesǁ 1.0414e-08 4.9268 0.45388 0.19772 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.22 290.34 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.017407 6.0678e-05 3.4224e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.13034 0.6281 0.20686 0.17658 INSTANT 0.402534000E+00 TIME STEP NUMBER 418 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.61766E-05 0.26150E-02 Friction velocity uk : 0.61839E-05 0.26149E-02 Dimensionless distance yplus : 0.41178E-04 0.17397E-01 Friction thermal sca. tstar : -0.19726E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.28921E-04 0.12218E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.61766E-05 0.26150E-02 Friction velocity uk : 0.61839E-05 0.26149E-02 Dimensionless distance yplus : 0.41178E-04 0.17397E-01 Friction thermal sca. tstar : -0.19726E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.28921E-04 0.12218E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34712E-08 3 0.29151E-06 0.55312E-12 0.14347E+01 c Velocity[X] 0.39959E-31 c Velocity[Y] 0.27655E-12 c Velocity[Z] 0.27656E-12 c Pressure 0.18830E-13 20 0.63941E-08 0.14757E-06 0.19509E+01 c k 0.58913E-06 2 0.80202E-07 0.14907E-07 0.22630E+01 c omega 0.13153E+02 1 0.37268E-08 0.15053E+01 0.63874E-02 c TempK 0.94488E+02 1 0.20946E-06 0.49844E-01 0.24783E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.2551e-13 1.0371e-13 -1.2758e-17 -3.2553e-18 v Velocity[Y] -0.00014744 0.00014392 -1.0921e-09 -4.4867e-12 v Velocity[Z] -0.00014392 0.00014745 9.4434e-10 -2.1179e-12 v ǁVelocityǁ 2.9516e-10 0.00015986 1.0411e-05 5.952e-06 v Pressure -0.00070556 0.016498 0.00086009 1.9611e-20 v k 3.6841e-09 0.0019269 0.001352 0.001673 v omega 22.575 1.0313e+05 2671.9 506.61 v TempK 288 341.76 293 290.19 v Density 1.205 1.205 1.205 1.205 v TurbVisc 4.3305e-14 9.9601e-05 6.583e-05 8.4278e-05 v CourantNb 1.6667e-09 0.00025421 1.4735e-05 7.6719e-06 v FourierNb 0.13024 0.6281 0.20676 0.1765 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9254 4.9255 0.00044754 -4.0627e-07 v volume_forces[Z] -4.9254 4.9255 -0.00044739 4.9271e-07 v ǁvolume_forcesǁ 1.0542e-08 4.927 0.45422 0.19796 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.22 290.34 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.017397 6.0649e-05 3.4206e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.13025 0.6281 0.20678 0.1765 INSTANT 0.403497000E+00 TIME STEP NUMBER 419 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.62232E-05 0.26134E-02 Friction velocity uk : 0.62304E-05 0.26133E-02 Dimensionless distance yplus : 0.41487E-04 0.17387E-01 Friction thermal sca. tstar : -0.19012E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.29138E-04 0.12211E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.62232E-05 0.26134E-02 Friction velocity uk : 0.62304E-05 0.26133E-02 Dimensionless distance yplus : 0.41487E-04 0.17387E-01 Friction thermal sca. tstar : -0.19012E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.29138E-04 0.12211E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34699E-08 3 0.29052E-06 0.54963E-12 0.14310E+01 c Velocity[X] 0.39622E-31 c Velocity[Y] 0.27481E-12 c Velocity[Z] 0.27482E-12 c Pressure 0.18758E-13 20 0.63770E-08 0.14700E-06 0.19460E+01 c k 0.58788E-06 2 0.79936E-07 0.14790E-07 0.22589E+01 c omega 0.13153E+02 1 0.37109E-08 0.14945E+01 0.63643E-02 c TempK 0.94488E+02 1 0.20877E-06 0.49668E-01 0.24739E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.2536e-13 1.0359e-13 -1.2744e-17 -3.2521e-18 v Velocity[Y] -0.00014732 0.00014379 -1.0923e-09 -4.4749e-12 v Velocity[Z] -0.00014379 0.00014733 9.4397e-10 -2.1203e-12 v ǁVelocityǁ 2.9873e-10 0.00015971 1.0409e-05 5.9546e-06 v Pressure -0.00070726 0.016517 0.00086146 6.0302e-20 v k 3.6621e-09 0.0019225 0.0013489 0.0016694 v omega 22.535 1.0313e+05 2671.8 506.57 v TempK 288 341.76 293.01 290.2 v Density 1.205 1.205 1.205 1.205 v TurbVisc 4.3046e-14 9.9583e-05 6.5796e-05 8.4241e-05 v CourantNb 1.6708e-09 0.00025393 1.4726e-05 7.6706e-06 v FourierNb 0.13015 0.6281 0.20668 0.17642 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9255 4.9256 0.00044788 -4.0686e-07 v volume_forces[Z] -4.9255 4.9256 -0.00044773 4.9338e-07 v ǁvolume_forcesǁ 1.067e-08 4.9271 0.45456 0.1982 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.23 290.34 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.017387 6.062e-05 3.4188e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.13015 0.6281 0.20669 0.17643 INSTANT 0.404460000E+00 TIME STEP NUMBER 420 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.62695E-05 0.26119E-02 Friction velocity uk : 0.62766E-05 0.26118E-02 Dimensionless distance yplus : 0.41795E-04 0.17376E-01 Friction thermal sca. tstar : -0.18369E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.29354E-04 0.12204E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.62695E-05 0.26119E-02 Friction velocity uk : 0.62766E-05 0.26118E-02 Dimensionless distance yplus : 0.41795E-04 0.17376E-01 Friction thermal sca. tstar : -0.18369E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.29354E-04 0.12204E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34686E-08 3 0.31821E-06 0.54619E-12 0.14274E+01 c Velocity[X] 0.39289E-31 c Velocity[Y] 0.27309E-12 c Velocity[Z] 0.27310E-12 c Pressure 0.18686E-13 20 0.63600E-08 0.14643E-06 0.19412E+01 c k 0.58664E-06 2 0.79671E-07 0.14674E-07 0.22549E+01 c omega 0.13153E+02 1 0.36950E-08 0.14837E+01 0.63414E-02 c TempK 0.94489E+02 1 0.20808E-06 0.49494E-01 0.24696E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.2522e-13 1.0347e-13 -1.2731e-17 -3.2488e-18 v Velocity[Y] -0.0001472 0.00014366 -1.0924e-09 -4.4632e-12 v Velocity[Z] -0.00014366 0.00014721 9.4358e-10 -2.1228e-12 v ǁVelocityǁ 3.0231e-10 0.00015957 1.0406e-05 5.9572e-06 v Pressure -0.00070897 0.016537 0.00086284 6.7166e-21 v k 3.6403e-09 0.0019182 0.0013458 0.0016657 v omega 22.494 1.0313e+05 2671.8 506.54 v TempK 288 341.76 293.01 290.2 v Density 1.205 1.205 1.205 1.205 v TurbVisc 4.2789e-14 9.9565e-05 6.5762e-05 8.4205e-05 v CourantNb 1.6748e-09 0.00025365 1.4717e-05 7.6693e-06 v FourierNb 0.13006 0.6281 0.2066 0.17635 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9257 4.9257 0.00044822 -4.0745e-07 v volume_forces[Z] -4.9257 4.9257 -0.00044807 4.9406e-07 v ǁvolume_forcesǁ 1.0799e-08 4.9272 0.4549 0.19844 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.23 290.34 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.017376 6.0591e-05 3.4171e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.13006 0.6281 0.20661 0.17636 INSTANT 0.405423000E+00 TIME STEP NUMBER 421 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.63157E-05 0.26104E-02 Friction velocity uk : 0.63226E-05 0.26103E-02 Dimensionless distance yplus : 0.42102E-04 0.17366E-01 Friction thermal sca. tstar : -0.17785E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.29569E-04 0.12197E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.63157E-05 0.26104E-02 Friction velocity uk : 0.63226E-05 0.26103E-02 Dimensionless distance yplus : 0.42102E-04 0.17366E-01 Friction thermal sca. tstar : -0.17785E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.29569E-04 0.12197E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34673E-08 3 0.28861E-06 0.54282E-12 0.14237E+01 c Velocity[X] 0.38961E-31 c Velocity[Y] 0.27140E-12 c Velocity[Z] 0.27141E-12 c Pressure 0.18635E-13 20 0.63450E-08 0.14603E-06 0.19364E+01 c k 0.58541E-06 2 0.79408E-07 0.14559E-07 0.22508E+01 c omega 0.13153E+02 1 0.36792E-08 0.14731E+01 0.63186E-02 c TempK 0.94490E+02 1 0.20740E-06 0.49321E-01 0.24652E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.2507e-13 1.0336e-13 -1.2718e-17 -3.2456e-18 v Velocity[Y] -0.00014708 0.00014353 -1.0925e-09 -4.4516e-12 v Velocity[Z] -0.00014353 0.00014709 9.4318e-10 -2.1253e-12 v ǁVelocityǁ 3.0591e-10 0.00015942 1.0403e-05 5.9599e-06 v Pressure -0.00071067 0.016557 0.00086421 1.2306e-20 v k 3.6186e-09 0.0019139 0.0013427 0.0016621 v omega 22.455 1.0313e+05 2671.8 506.5 v TempK 288 341.76 293.01 290.2 v Density 1.205 1.205 1.205 1.205 v TurbVisc 4.2534e-14 9.9548e-05 6.5728e-05 8.4168e-05 v CourantNb 1.6789e-09 0.00025338 1.4708e-05 7.6681e-06 v FourierNb 0.12996 0.6281 0.20651 0.17628 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9258 4.9258 0.00044856 -4.0804e-07 v volume_forces[Z] -4.9258 4.9258 -0.00044841 4.9473e-07 v ǁvolume_forcesǁ 1.0929e-08 4.9273 0.45524 0.19868 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.23 290.35 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.017366 6.0562e-05 3.4154e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.12996 0.6281 0.20653 0.17629 INSTANT 0.406386000E+00 TIME STEP NUMBER 422 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.63616E-05 0.26088E-02 Friction velocity uk : 0.63684E-05 0.26087E-02 Dimensionless distance yplus : 0.42407E-04 0.17356E-01 Friction thermal sca. tstar : -0.17251E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.29784E-04 0.12190E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.63616E-05 0.26088E-02 Friction velocity uk : 0.63684E-05 0.26087E-02 Dimensionless distance yplus : 0.42407E-04 0.17356E-01 Friction thermal sca. tstar : -0.17251E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.29784E-04 0.12190E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34661E-08 3 0.28764E-06 0.53949E-12 0.14202E+01 c Velocity[X] 0.38637E-31 c Velocity[Y] 0.26974E-12 c Velocity[Z] 0.26975E-12 c Pressure 0.18550E-13 20 0.63289E-08 0.14536E-06 0.19317E+01 c k 0.58418E-06 2 0.79146E-07 0.14446E-07 0.22468E+01 c omega 0.13153E+02 1 0.36636E-08 0.14625E+01 0.62959E-02 c TempK 0.94490E+02 1 0.20672E-06 0.49149E-01 0.24609E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.2493e-13 1.0324e-13 -1.2704e-17 -3.2424e-18 v Velocity[Y] -0.00014697 0.0001434 -1.0926e-09 -4.4399e-12 v Velocity[Z] -0.0001434 0.00014697 9.4277e-10 -2.1275e-12 v ǁVelocityǁ 3.0953e-10 0.00015928 1.0401e-05 5.9626e-06 v Pressure -0.00071238 0.016577 0.00086559 -1.814e-20 v k 3.5971e-09 0.0019097 0.0013396 0.0016585 v omega 22.415 1.0313e+05 2671.7 506.46 v TempK 288 341.76 293.02 290.21 v Density 1.205 1.205 1.205 1.205 v TurbVisc 4.2281e-14 9.953e-05 6.5694e-05 8.4132e-05 v CourantNb 1.6829e-09 0.0002531 1.4699e-05 7.667e-06 v FourierNb 0.12987 0.6281 0.20643 0.17621 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9259 4.926 0.00044889 -4.0863e-07 v volume_forces[Z] -4.9259 4.926 -0.00044875 4.954e-07 v ǁvolume_forcesǁ 1.1059e-08 4.9274 0.45558 0.19891 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.24 290.35 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.017356 6.0533e-05 3.4136e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.12987 0.6281 0.20645 0.17621 INSTANT 0.407349000E+00 TIME STEP NUMBER 423 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.64073E-05 0.26073E-02 Friction velocity uk : 0.64140E-05 0.26072E-02 Dimensionless distance yplus : 0.42710E-04 0.17346E-01 Friction thermal sca. tstar : -0.16761E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.29997E-04 0.12183E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.64073E-05 0.26073E-02 Friction velocity uk : 0.64140E-05 0.26072E-02 Dimensionless distance yplus : 0.42710E-04 0.17346E-01 Friction thermal sca. tstar : -0.16761E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.29997E-04 0.12183E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34649E-08 3 0.28663E-06 0.53622E-12 0.14166E+01 c Velocity[X] 0.38318E-31 c Velocity[Y] 0.26811E-12 c Velocity[Z] 0.26812E-12 c Pressure 0.18472E-13 20 0.63111E-08 0.14474E-06 0.19269E+01 c k 0.58296E-06 2 0.78887E-07 0.14333E-07 0.22428E+01 c omega 0.13153E+02 1 0.36480E-08 0.14520E+01 0.62733E-02 c TempK 0.94491E+02 1 0.20604E-06 0.48978E-01 0.24566E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.2478e-13 1.0313e-13 -1.2691e-17 -3.2392e-18 v Velocity[Y] -0.00014685 0.00014327 -1.0927e-09 -4.4283e-12 v Velocity[Z] -0.00014327 0.00014685 9.4235e-10 -2.13e-12 v ǁVelocityǁ 3.1316e-10 0.00015914 1.0399e-05 5.9653e-06 v Pressure -0.00071408 0.016597 0.00086696 -5.0399e-20 v k 3.5758e-09 0.0019054 0.0013365 0.0016549 v omega 22.375 1.0313e+05 2671.7 506.43 v TempK 288 341.77 293.02 290.21 v Density 1.205 1.205 1.205 1.205 v TurbVisc 4.203e-14 9.9512e-05 6.566e-05 8.4096e-05 v CourantNb 1.687e-09 0.00025283 1.469e-05 7.6659e-06 v FourierNb 0.12978 0.6281 0.20635 0.17613 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.926 4.9261 0.00044923 -4.0922e-07 v volume_forces[Z] -4.926 4.9261 -0.00044908 4.9606e-07 v ǁvolume_forcesǁ 1.1189e-08 4.9276 0.45592 0.19915 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.24 290.35 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.017346 6.0505e-05 3.4119e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.12978 0.6281 0.20636 0.17614 INSTANT 0.408312000E+00 TIME STEP NUMBER 424 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.64529E-05 0.26058E-02 Friction velocity uk : 0.64595E-05 0.26057E-02 Dimensionless distance yplus : 0.43013E-04 0.17336E-01 Friction thermal sca. tstar : -0.16309E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.30210E-04 0.12176E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.64529E-05 0.26058E-02 Friction velocity uk : 0.64595E-05 0.26057E-02 Dimensionless distance yplus : 0.43013E-04 0.17336E-01 Friction thermal sca. tstar : -0.16309E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.30210E-04 0.12176E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34637E-08 3 0.28569E-06 0.53301E-12 0.14132E+01 c Velocity[X] 0.38003E-31 c Velocity[Y] 0.26650E-12 c Velocity[Z] 0.26651E-12 c Pressure 0.18412E-13 20 0.62961E-08 0.14427E-06 0.19222E+01 c k 0.58174E-06 2 0.78628E-07 0.14222E-07 0.22388E+01 c omega 0.13153E+02 1 0.36325E-08 0.14417E+01 0.62509E-02 c TempK 0.94492E+02 1 0.20537E-06 0.48808E-01 0.24523E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.2464e-13 1.0302e-13 -1.2678e-17 -3.2361e-18 v Velocity[Y] -0.00014673 0.00014315 -1.0928e-09 -4.4167e-12 v Velocity[Z] -0.00014314 0.00014673 9.4193e-10 -2.1324e-12 v ǁVelocityǁ 3.1681e-10 0.000159 1.0396e-05 5.9681e-06 v Pressure -0.00071579 0.016616 0.00086833 -4.9958e-20 v k 3.5546e-09 0.0019011 0.0013335 0.0016513 v omega 22.336 1.0313e+05 2671.7 506.39 v TempK 288 341.77 293.03 290.21 v Density 1.205 1.205 1.205 1.205 v TurbVisc 4.178e-14 9.9495e-05 6.5626e-05 8.406e-05 v CourantNb 1.691e-09 0.00025256 1.4682e-05 7.6649e-06 v FourierNb 0.12968 0.6281 0.20627 0.17606 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9262 4.9262 0.00044957 -4.0981e-07 v volume_forces[Z] -4.9262 4.9262 -0.00044942 4.9673e-07 v ǁvolume_forcesǁ 1.1321e-08 4.9277 0.45625 0.19939 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.24 290.35 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.017336 6.0476e-05 3.4102e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.12969 0.6281 0.20628 0.17607 INSTANT 0.409275000E+00 TIME STEP NUMBER 425 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.64982E-05 0.26043E-02 Friction velocity uk : 0.65047E-05 0.26042E-02 Dimensionless distance yplus : 0.43314E-04 0.17326E-01 Friction thermal sca. tstar : -0.15890E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.30421E-04 0.12169E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.64982E-05 0.26043E-02 Friction velocity uk : 0.65047E-05 0.26042E-02 Dimensionless distance yplus : 0.43314E-04 0.17326E-01 Friction thermal sca. tstar : -0.15890E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.30421E-04 0.12169E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34625E-08 3 0.28472E-06 0.52985E-12 0.14097E+01 c Velocity[X] 0.37693E-31 c Velocity[Y] 0.26492E-12 c Velocity[Z] 0.26493E-12 c Pressure 0.18320E-13 20 0.62808E-08 0.14354E-06 0.19175E+01 c k 0.58052E-06 2 0.78372E-07 0.14111E-07 0.22348E+01 c omega 0.13153E+02 1 0.36171E-08 0.14314E+01 0.62285E-02 c TempK 0.94492E+02 1 0.20470E-06 0.48639E-01 0.24480E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.245e-13 1.029e-13 -1.2665e-17 -3.2329e-18 v Velocity[Y] -0.00014661 0.00014302 -1.0928e-09 -4.4052e-12 v Velocity[Z] -0.00014301 0.00014662 9.4149e-10 -2.1349e-12 v ǁVelocityǁ 3.2047e-10 0.00015885 1.0394e-05 5.9709e-06 v Pressure -0.00071749 0.016636 0.0008697 7.1088e-21 v k 3.5337e-09 0.0018969 0.0013304 0.0016477 v omega 22.296 1.0313e+05 2671.7 506.36 v TempK 288 341.77 293.03 290.21 v Density 1.205 1.205 1.205 1.205 v TurbVisc 4.1533e-14 9.9477e-05 6.5592e-05 8.4024e-05 v CourantNb 1.6951e-09 0.00025229 1.4673e-05 7.6639e-06 v FourierNb 0.12959 0.6281 0.20618 0.17599 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9263 4.9263 0.0004499 -4.1039e-07 v volume_forces[Z] -4.9263 4.9263 -0.00044975 4.9739e-07 v ǁvolume_forcesǁ 1.1453e-08 4.9278 0.45659 0.19963 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.25 290.36 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.017326 6.0447e-05 3.4084e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.12959 0.6281 0.2062 0.176 INSTANT 0.410238000E+00 TIME STEP NUMBER 426 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.65433E-05 0.26028E-02 Friction velocity uk : 0.65497E-05 0.26027E-02 Dimensionless distance yplus : 0.43614E-04 0.17316E-01 Friction thermal sca. tstar : -0.15501E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.30632E-04 0.12162E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.65433E-05 0.26028E-02 Friction velocity uk : 0.65497E-05 0.26027E-02 Dimensionless distance yplus : 0.43614E-04 0.17316E-01 Friction thermal sca. tstar : -0.15501E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.30632E-04 0.12162E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34613E-08 3 0.28377E-06 0.52673E-12 0.14063E+01 c Velocity[X] 0.37386E-31 c Velocity[Y] 0.26336E-12 c Velocity[Z] 0.26337E-12 c Pressure 0.18261E-13 20 0.62648E-08 0.14307E-06 0.19128E+01 c k 0.57931E-06 2 0.78117E-07 0.14002E-07 0.22308E+01 c omega 0.13153E+02 1 0.36018E-08 0.14212E+01 0.62063E-02 c TempK 0.94493E+02 1 0.20403E-06 0.48471E-01 0.24437E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.2435e-13 1.0279e-13 -1.2652e-17 -3.2297e-18 v Velocity[Y] -0.0001465 0.00014289 -1.0929e-09 -4.3937e-12 v Velocity[Z] -0.00014289 0.0001465 9.4104e-10 -2.1372e-12 v ǁVelocityǁ 3.2415e-10 0.00015871 1.0392e-05 5.9738e-06 v Pressure -0.0007192 0.016656 0.00087106 -1.157e-20 v k 3.5128e-09 0.0018927 0.0013274 0.0016441 v omega 22.257 1.0313e+05 2671.6 506.32 v TempK 288 341.77 293.03 290.22 v Density 1.205 1.205 1.205 1.205 v TurbVisc 4.1288e-14 9.946e-05 6.5558e-05 8.3988e-05 v CourantNb 1.6992e-09 0.00025202 1.4665e-05 7.6629e-06 v FourierNb 0.1295 0.6281 0.2061 0.17592 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9264 4.9265 0.00045024 -4.1097e-07 v volume_forces[Z] -4.9264 4.9265 -0.00045009 4.9806e-07 v ǁvolume_forcesǁ 1.1585e-08 4.9279 0.45692 0.19986 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.25 290.36 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.017316 6.0419e-05 3.4067e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.1295 0.6281 0.20612 0.17593 INSTANT 0.411201000E+00 TIME STEP NUMBER 427 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.65883E-05 0.26013E-02 Friction velocity uk : 0.65946E-05 0.26012E-02 Dimensionless distance yplus : 0.43912E-04 0.17306E-01 Friction thermal sca. tstar : -0.15138E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.30841E-04 0.12155E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.65883E-05 0.26013E-02 Friction velocity uk : 0.65946E-05 0.26012E-02 Dimensionless distance yplus : 0.43912E-04 0.17306E-01 Friction thermal sca. tstar : -0.15138E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.30841E-04 0.12155E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34602E-08 3 0.55940E-06 0.52368E-12 0.14030E+01 c Velocity[X] 0.37083E-31 c Velocity[Y] 0.26183E-12 c Velocity[Z] 0.26184E-12 c Pressure 0.18372E-13 20 0.62717E-08 0.14393E-06 0.19082E+01 c k 0.57810E-06 2 0.77864E-07 0.13894E-07 0.22269E+01 c omega 0.13153E+02 1 0.35866E-08 0.14111E+01 0.61842E-02 c TempK 0.94494E+02 1 0.20337E-06 0.48303E-01 0.24395E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.2421e-13 1.0268e-13 -1.2639e-17 -3.2266e-18 v Velocity[Y] -0.00014638 0.00014277 -1.0929e-09 -4.3828e-12 v Velocity[Z] -0.00014276 0.00014638 9.4059e-10 -2.1396e-12 v ǁVelocityǁ 3.2784e-10 0.00015857 1.039e-05 5.9767e-06 v Pressure -0.0007209 0.016676 0.00087243 -2.2895e-20 v k 3.4922e-09 0.0018885 0.0013244 0.0016406 v omega 22.218 1.0313e+05 2671.6 506.28 v TempK 288 341.77 293.04 290.22 v Density 1.205 1.205 1.205 1.205 v TurbVisc 4.1045e-14 9.9442e-05 6.5525e-05 8.3952e-05 v CourantNb 1.7032e-09 0.00025176 1.4656e-05 7.662e-06 v FourierNb 0.1294 0.6281 0.20602 0.17585 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9265 4.9266 0.00045057 -4.1155e-07 v volume_forces[Z] -4.9265 4.9266 -0.00045042 4.9872e-07 v ǁvolume_forcesǁ 1.1718e-08 4.9281 0.45726 0.2001 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.25 290.36 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.017306 6.0391e-05 3.405e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.12941 0.6281 0.20603 0.17585 INSTANT 0.412164000E+00 TIME STEP NUMBER 428 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.66330E-05 0.25998E-02 Friction velocity uk : 0.66392E-05 0.25997E-02 Dimensionless distance yplus : 0.44210E-04 0.17296E-01 Friction thermal sca. tstar : -0.14798E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.31050E-04 0.12148E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.66330E-05 0.25998E-02 Friction velocity uk : 0.66392E-05 0.25997E-02 Dimensionless distance yplus : 0.44210E-04 0.17296E-01 Friction thermal sca. tstar : -0.14798E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.31050E-04 0.12148E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34591E-08 3 0.28198E-06 0.52066E-12 0.13997E+01 c Velocity[X] 0.36785E-31 c Velocity[Y] 0.26033E-12 c Velocity[Z] 0.26034E-12 c Pressure 0.18239E-13 20 0.62431E-08 0.14289E-06 0.19035E+01 c k 0.57690E-06 2 0.77612E-07 0.13786E-07 0.22230E+01 c omega 0.13153E+02 1 0.35714E-08 0.14011E+01 0.61623E-02 c TempK 0.94494E+02 1 0.20271E-06 0.48137E-01 0.24353E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.2407e-13 1.0257e-13 -1.2625e-17 -3.2234e-18 v Velocity[Y] -0.00014627 0.00014264 -1.093e-09 -4.3714e-12 v Velocity[Z] -0.00014264 0.00014627 9.4012e-10 -2.142e-12 v ǁVelocityǁ 3.3156e-10 0.00015844 1.0388e-05 5.9796e-06 v Pressure -0.00072261 0.016695 0.00087379 -1.9905e-20 v k 3.4717e-09 0.0018843 0.0013214 0.0016371 v omega 22.179 1.0313e+05 2671.6 506.25 v TempK 288 341.77 293.04 290.22 v Density 1.205 1.205 1.205 1.205 v TurbVisc 4.0804e-14 9.9425e-05 6.5491e-05 8.3916e-05 v CourantNb 1.7072e-09 0.00025149 1.4648e-05 7.6612e-06 v FourierNb 0.12931 0.6281 0.20594 0.17578 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9267 4.9267 0.0004509 -4.1213e-07 v volume_forces[Z] -4.9267 4.9267 -0.00045076 4.9937e-07 v ǁvolume_forcesǁ 1.1852e-08 4.9282 0.45759 0.20034 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.26 290.37 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.017296 6.0362e-05 3.4033e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.12931 0.6281 0.20595 0.17578 INSTANT 0.413127000E+00 TIME STEP NUMBER 429 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.66776E-05 0.25983E-02 Friction velocity uk : 0.66836E-05 0.25982E-02 Dimensionless distance yplus : 0.44506E-04 0.17286E-01 Friction thermal sca. tstar : -0.14479E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.31258E-04 0.12141E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.66776E-05 0.25983E-02 Friction velocity uk : 0.66836E-05 0.25982E-02 Dimensionless distance yplus : 0.44506E-04 0.17286E-01 Friction thermal sca. tstar : -0.14479E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.31258E-04 0.12141E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34580E-08 3 0.28096E-06 0.51770E-12 0.13964E+01 c Velocity[X] 0.36491E-31 c Velocity[Y] 0.25884E-12 c Velocity[Z] 0.25886E-12 c Pressure 0.18045E-13 20 0.62188E-08 0.14137E-06 0.18989E+01 c k 0.57571E-06 2 0.77361E-07 0.13680E-07 0.22190E+01 c omega 0.13153E+02 1 0.35564E-08 0.13912E+01 0.61404E-02 c TempK 0.94495E+02 1 0.20206E-06 0.47972E-01 0.24311E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.2393e-13 1.0246e-13 -1.2612e-17 -3.2203e-18 v Velocity[Y] -0.00014615 0.00014252 -1.093e-09 -4.3595e-12 v Velocity[Z] -0.00014251 0.00014615 9.3965e-10 -2.1442e-12 v ǁVelocityǁ 3.3529e-10 0.0001583 1.0386e-05 5.9825e-06 v Pressure -0.00072431 0.016715 0.00087515 -1.4218e-20 v k 3.4514e-09 0.0018801 0.0013184 0.0016335 v omega 22.14 1.0313e+05 2671.5 506.21 v TempK 288 341.77 293.04 290.22 v Density 1.205 1.205 1.205 1.205 v TurbVisc 4.0564e-14 9.9408e-05 6.5458e-05 8.388e-05 v CourantNb 1.7113e-09 0.00025123 1.464e-05 7.6603e-06 v FourierNb 0.12922 0.6281 0.20586 0.17571 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9268 4.9268 0.00045124 -4.1271e-07 v volume_forces[Z] -4.9268 4.9268 -0.00045109 5.0003e-07 v ǁvolume_forcesǁ 1.1986e-08 4.9283 0.45793 0.20057 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.26 290.37 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.017286 6.0334e-05 3.4016e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.12922 0.6281 0.20587 0.17571 INSTANT 0.414090000E+00 TIME STEP NUMBER 430 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.67220E-05 0.25969E-02 Friction velocity uk : 0.67280E-05 0.25968E-02 Dimensionless distance yplus : 0.44801E-04 0.17276E-01 Friction thermal sca. tstar : -0.14178E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.31465E-04 0.12134E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.67220E-05 0.25969E-02 Friction velocity uk : 0.67280E-05 0.25968E-02 Dimensionless distance yplus : 0.44801E-04 0.17276E-01 Friction thermal sca. tstar : -0.14178E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.31465E-04 0.12134E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34569E-08 3 0.28004E-06 0.51478E-12 0.13932E+01 c Velocity[X] 0.36201E-31 c Velocity[Y] 0.25738E-12 c Velocity[Z] 0.25740E-12 c Pressure 0.17986E-13 20 0.62042E-08 0.14089E-06 0.18943E+01 c k 0.57451E-06 2 0.77112E-07 0.13575E-07 0.22151E+01 c omega 0.13153E+02 1 0.35414E-08 0.13813E+01 0.61187E-02 c TempK 0.94496E+02 1 0.20141E-06 0.47808E-01 0.24269E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.2379e-13 1.0235e-13 -1.2599e-17 -3.2172e-18 v Velocity[Y] -0.00014604 0.00014239 -1.093e-09 -4.3482e-12 v Velocity[Z] -0.00014239 0.00014604 9.3916e-10 -2.1464e-12 v ǁVelocityǁ 3.3903e-10 0.00015816 1.0384e-05 5.9855e-06 v Pressure -0.00072601 0.016734 0.00087651 8.6875e-20 v k 3.4312e-09 0.001876 0.0013154 0.00163 v omega 22.102 1.0313e+05 2671.5 506.18 v TempK 288 341.77 293.05 290.23 v Density 1.205 1.205 1.205 1.205 v TurbVisc 4.0327e-14 9.939e-05 6.5424e-05 8.3844e-05 v CourantNb 1.7153e-09 0.00025096 1.4632e-05 7.6596e-06 v FourierNb 0.12913 0.6281 0.20578 0.17563 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9269 4.9269 0.00045157 -4.1329e-07 v volume_forces[Z] -4.9269 4.9269 -0.00045142 5.0068e-07 v ǁvolume_forcesǁ 1.2121e-08 4.9284 0.45826 0.20081 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.27 290.37 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.017276 6.0306e-05 3.3999e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.12913 0.6281 0.20579 0.17564 INSTANT 0.415053000E+00 TIME STEP NUMBER 431 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.67662E-05 0.25954E-02 Friction velocity uk : 0.67721E-05 0.25953E-02 Dimensionless distance yplus : 0.45095E-04 0.17267E-01 Friction thermal sca. tstar : -0.13895E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.31672E-04 0.12127E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.67662E-05 0.25954E-02 Friction velocity uk : 0.67721E-05 0.25953E-02 Dimensionless distance yplus : 0.45095E-04 0.17267E-01 Friction thermal sca. tstar : -0.13895E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.31672E-04 0.12127E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34559E-08 3 0.28050E-06 0.51191E-12 0.13900E+01 c Velocity[X] 0.35915E-31 c Velocity[Y] 0.25595E-12 c Velocity[Z] 0.25596E-12 c Pressure 0.17908E-13 20 0.61883E-08 0.14028E-06 0.18897E+01 c k 0.57332E-06 2 0.76865E-07 0.13470E-07 0.22112E+01 c omega 0.13153E+02 1 0.35266E-08 0.13716E+01 0.60970E-02 c TempK 0.94496E+02 1 0.20076E-06 0.47644E-01 0.24227E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.2365e-13 1.0224e-13 -1.2587e-17 -3.2141e-18 v Velocity[Y] -0.00014592 0.00014227 -1.093e-09 -4.3369e-12 v Velocity[Z] -0.00014226 0.00014593 9.3867e-10 -2.1487e-12 v ǁVelocityǁ 3.4278e-10 0.00015802 1.0382e-05 5.9886e-06 v Pressure -0.00072772 0.016754 0.00087787 -1.1766e-21 v k 3.4112e-09 0.0018718 0.0013124 0.0016265 v omega 22.063 1.0313e+05 2671.5 506.14 v TempK 288 341.78 293.05 290.23 v Density 1.205 1.205 1.205 1.205 v TurbVisc 4.0091e-14 9.9373e-05 6.5391e-05 8.3809e-05 v CourantNb 1.7194e-09 0.0002507 1.4624e-05 7.6589e-06 v FourierNb 0.12904 0.6281 0.2057 0.17556 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.927 4.9271 0.0004519 -4.1386e-07 v volume_forces[Z] -4.927 4.9271 -0.00045175 5.0134e-07 v ǁvolume_forcesǁ 1.2256e-08 4.9285 0.45859 0.20105 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.27 290.37 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.017267 6.0278e-05 3.3982e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.12904 0.6281 0.20571 0.17557 INSTANT 0.416016000E+00 TIME STEP NUMBER 432 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.68102E-05 0.25939E-02 Friction velocity uk : 0.68161E-05 0.25938E-02 Dimensionless distance yplus : 0.45387E-04 0.17257E-01 Friction thermal sca. tstar : -0.13627E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.31877E-04 0.12120E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.68102E-05 0.25939E-02 Friction velocity uk : 0.68161E-05 0.25938E-02 Dimensionless distance yplus : 0.45387E-04 0.17257E-01 Friction thermal sca. tstar : -0.13627E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.31877E-04 0.12120E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34549E-08 3 0.27820E-06 0.50908E-12 0.13869E+01 c Velocity[X] 0.35633E-31 c Velocity[Y] 0.25454E-12 c Velocity[Z] 0.25455E-12 c Pressure 0.17845E-13 20 0.61376E-08 0.13978E-06 0.18852E+01 c k 0.57214E-06 2 0.76619E-07 0.13367E-07 0.22073E+01 c omega 0.13153E+02 1 0.35118E-08 0.13619E+01 0.60755E-02 c TempK 0.94497E+02 1 0.20012E-06 0.47482E-01 0.24185E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.2351e-13 1.0213e-13 -1.2574e-17 -3.211e-18 v Velocity[Y] -0.00014581 0.00014215 -1.0929e-09 -4.1873e-12 v Velocity[Z] -0.00014214 0.00014581 9.3838e-10 -1.9446e-12 v ǁVelocityǁ 3.4655e-10 0.00015788 1.038e-05 5.9916e-06 v Pressure -0.00072942 0.016774 0.00087923 2.1915e-20 v k 3.3914e-09 0.0018677 0.0013095 0.0016231 v omega 22.025 1.0313e+05 2671.5 506.11 v TempK 288 341.78 293.06 290.23 v Density 1.205 1.205 1.205 1.205 v TurbVisc 3.9858e-14 9.9356e-05 6.5358e-05 8.3773e-05 v CourantNb 1.7235e-09 0.00025044 1.4616e-05 7.6582e-06 v FourierNb 0.12894 0.6281 0.20562 0.17549 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9271 4.9272 0.00045223 -4.1443e-07 v volume_forces[Z] -4.9271 4.9272 -0.00045209 5.0199e-07 v ǁvolume_forcesǁ 1.2392e-08 4.9287 0.45892 0.20128 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.27 290.38 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.017257 6.025e-05 3.3965e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.12895 0.6281 0.20563 0.1755 INSTANT 0.416979000E+00 TIME STEP NUMBER 433 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.68541E-05 0.25924E-02 Friction velocity uk : 0.68598E-05 0.25924E-02 Dimensionless distance yplus : 0.45679E-04 0.17247E-01 Friction thermal sca. tstar : -0.13373E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.32082E-04 0.12113E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.68541E-05 0.25924E-02 Friction velocity uk : 0.68598E-05 0.25924E-02 Dimensionless distance yplus : 0.45679E-04 0.17247E-01 Friction thermal sca. tstar : -0.13373E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.32082E-04 0.12113E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34539E-08 3 0.27728E-06 0.50630E-12 0.13838E+01 c Velocity[X] 0.35353E-31 c Velocity[Y] 0.25314E-12 c Velocity[Z] 0.25316E-12 c Pressure 0.17774E-13 20 0.61233E-08 0.13923E-06 0.18807E+01 c k 0.57096E-06 2 0.76374E-07 0.13265E-07 0.22035E+01 c omega 0.13153E+02 1 0.34971E-08 0.13523E+01 0.60541E-02 c TempK 0.94497E+02 1 0.19948E-06 0.47320E-01 0.24144E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.2337e-13 1.0202e-13 -1.2561e-17 -3.2079e-18 v Velocity[Y] -0.0001457 0.00014202 -1.0929e-09 -4.1751e-12 v Velocity[Z] -0.00014202 0.0001457 9.3786e-10 -1.9469e-12 v ǁVelocityǁ 3.5035e-10 0.00015775 1.0378e-05 5.9947e-06 v Pressure -0.00073112 0.016793 0.00088058 -5.9812e-21 v k 3.3717e-09 0.0018636 0.0013065 0.0016196 v omega 21.986 1.0313e+05 2671.4 506.07 v TempK 288 341.78 293.06 290.23 v Density 1.205 1.205 1.205 1.205 v TurbVisc 3.9626e-14 9.9339e-05 6.5325e-05 8.3738e-05 v CourantNb 1.7275e-09 0.00025018 1.4608e-05 7.6575e-06 v FourierNb 0.12885 0.6281 0.20554 0.17542 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9273 4.9273 0.00045256 -4.15e-07 v volume_forces[Z] -4.9273 4.9273 -0.00045242 5.0263e-07 v ǁvolume_forcesǁ 1.2528e-08 4.9288 0.45925 0.20152 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.28 290.38 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.017247 6.0222e-05 3.3948e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.12885 0.6281 0.20555 0.17543 INSTANT 0.417942000E+00 TIME STEP NUMBER 434 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.68980E-05 0.25910E-02 Friction velocity uk : 0.69037E-05 0.25909E-02 Dimensionless distance yplus : 0.45971E-04 0.17237E-01 Friction thermal sca. tstar : -0.13132E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.32287E-04 0.12106E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.68980E-05 0.25910E-02 Friction velocity uk : 0.69037E-05 0.25909E-02 Dimensionless distance yplus : 0.45971E-04 0.17237E-01 Friction thermal sca. tstar : -0.13132E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.32287E-04 0.12106E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34529E-08 3 0.27643E-06 0.50356E-12 0.13807E+01 c Velocity[X] 0.35077E-31 c Velocity[Y] 0.25178E-12 c Velocity[Z] 0.25179E-12 c Pressure 0.17806E-13 20 0.61168E-08 0.13946E-06 0.18762E+01 c k 0.56979E-06 2 0.76131E-07 0.13164E-07 0.21996E+01 c omega 0.13153E+02 1 0.34825E-08 0.13428E+01 0.60328E-02 c TempK 0.94498E+02 1 0.19884E-06 0.47159E-01 0.24103E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.2323e-13 1.0191e-13 -1.2548e-17 -3.2048e-18 v Velocity[Y] -0.00014558 0.0001419 -1.0928e-09 -4.1651e-12 v Velocity[Z] -0.0001419 0.00014559 9.3734e-10 -1.9498e-12 v ǁVelocityǁ 3.5416e-10 0.00015761 1.0376e-05 5.9978e-06 v Pressure -0.00073283 0.016813 0.00088194 -1.5983e-20 v k 3.3521e-09 0.0018595 0.0013036 0.0016161 v omega 21.948 1.0313e+05 2671.4 506.04 v TempK 288 341.78 293.06 290.24 v Density 1.205 1.205 1.205 1.205 v TurbVisc 3.9396e-14 9.9321e-05 6.5292e-05 8.3702e-05 v CourantNb 1.7315e-09 0.00024993 1.46e-05 7.657e-06 v FourierNb 0.12876 0.6281 0.20546 0.17535 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9274 4.9274 0.00045289 -4.1557e-07 v volume_forces[Z] -4.9274 4.9274 -0.00045275 5.0328e-07 v ǁvolume_forcesǁ 1.2665e-08 4.9289 0.45959 0.20175 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.28 290.38 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.017237 6.0194e-05 3.3932e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.12876 0.6281 0.20547 0.17536 INSTANT 0.418905000E+00 TIME STEP NUMBER 435 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.69417E-05 0.25895E-02 Friction velocity uk : 0.69472E-05 0.25894E-02 Dimensionless distance yplus : 0.46261E-04 0.17228E-01 Friction thermal sca. tstar : -0.12903E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.32491E-04 0.12100E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.69417E-05 0.25895E-02 Friction velocity uk : 0.69472E-05 0.25894E-02 Dimensionless distance yplus : 0.46261E-04 0.17228E-01 Friction thermal sca. tstar : -0.12903E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.32491E-04 0.12100E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34519E-08 3 0.27549E-06 0.50087E-12 0.13777E+01 c Velocity[X] 0.34806E-31 c Velocity[Y] 0.25043E-12 c Velocity[Z] 0.25044E-12 c Pressure 0.17645E-13 20 0.60941E-08 0.13820E-06 0.18717E+01 c k 0.56862E-06 2 0.75890E-07 0.13063E-07 0.21958E+01 c omega 0.13153E+02 1 0.34680E-08 0.13334E+01 0.60116E-02 c TempK 0.94499E+02 1 0.19821E-06 0.46999E-01 0.24062E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.231e-13 1.018e-13 -1.2535e-17 -3.2017e-18 v Velocity[Y] -0.00014547 0.00014178 -1.0928e-09 -4.154e-12 v Velocity[Z] -0.00014177 0.00014548 9.3681e-10 -1.9523e-12 v ǁVelocityǁ 3.5798e-10 0.00015748 1.0374e-05 6.001e-06 v Pressure -0.00073453 0.016832 0.00088329 -1.6179e-20 v k 3.3327e-09 0.0018554 0.0013007 0.0016127 v omega 21.91 1.0313e+05 2671.4 506.01 v TempK 288 341.78 293.07 290.24 v Density 1.205 1.205 1.205 1.205 v TurbVisc 3.9167e-14 9.9304e-05 6.5259e-05 8.3667e-05 v CourantNb 1.7356e-09 0.00024967 1.4592e-05 7.6564e-06 v FourierNb 0.12867 0.6281 0.20538 0.17528 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9275 4.9275 0.00045322 -4.1614e-07 v volume_forces[Z] -4.9275 4.9275 -0.00045308 5.0393e-07 v ǁvolume_forcesǁ 1.2803e-08 4.929 0.45992 0.20199 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.28 290.38 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.017228 6.0166e-05 3.3915e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.12867 0.6281 0.20539 0.17529 INSTANT 0.419868000E+00 TIME STEP NUMBER 436 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.69851E-05 0.25881E-02 Friction velocity uk : 0.69906E-05 0.25880E-02 Dimensionless distance yplus : 0.46550E-04 0.17218E-01 Friction thermal sca. tstar : -0.12685E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.32693E-04 0.12093E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.69851E-05 0.25881E-02 Friction velocity uk : 0.69906E-05 0.25880E-02 Dimensionless distance yplus : 0.46550E-04 0.17218E-01 Friction thermal sca. tstar : -0.12685E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.32693E-04 0.12093E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34509E-08 3 0.27460E-06 0.49822E-12 0.13747E+01 c Velocity[X] 0.34538E-31 c Velocity[Y] 0.24910E-12 c Velocity[Z] 0.24911E-12 c Pressure 0.17580E-13 20 0.60680E-08 0.13769E-06 0.18672E+01 c k 0.56745E-06 2 0.75650E-07 0.12964E-07 0.21919E+01 c omega 0.13153E+02 1 0.34536E-08 0.13241E+01 0.59905E-02 c TempK 0.94499E+02 1 0.19758E-06 0.46841E-01 0.24021E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.2296e-13 1.0169e-13 -1.2523e-17 -3.1987e-18 v Velocity[Y] -0.00014536 0.00014166 -1.0927e-09 -4.1149e-12 v Velocity[Z] -0.00014165 0.00014537 9.3634e-10 -1.8836e-12 v ǁVelocityǁ 3.6177e-10 0.00015734 1.0373e-05 6.0042e-06 v Pressure -0.00073624 0.016852 0.00088464 -2.7357e-20 v k 3.3135e-09 0.0018513 0.0012977 0.0016093 v omega 21.872 1.0313e+05 2671.3 505.97 v TempK 288 341.78 293.07 290.24 v Density 1.205 1.205 1.205 1.205 v TurbVisc 3.8941e-14 9.9287e-05 6.5226e-05 8.3632e-05 v CourantNb 1.7396e-09 0.00024941 1.4585e-05 7.6559e-06 v FourierNb 0.12858 0.6281 0.2053 0.17521 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9276 4.9277 0.00045355 -4.1671e-07 v volume_forces[Z] -4.9276 4.9277 -0.0004534 5.0457e-07 v ǁvolume_forcesǁ 1.2941e-08 4.9291 0.46024 0.20222 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.29 290.39 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.017218 6.0139e-05 3.3898e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.12858 0.6281 0.20531 0.17522 INSTANT 0.420831000E+00 TIME STEP NUMBER 437 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.70279E-05 0.25866E-02 Friction velocity uk : 0.70332E-05 0.25865E-02 Dimensionless distance yplus : 0.46834E-04 0.17208E-01 Friction thermal sca. tstar : -0.12477E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.32893E-04 0.12086E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.70279E-05 0.25866E-02 Friction velocity uk : 0.70332E-05 0.25865E-02 Dimensionless distance yplus : 0.46834E-04 0.17208E-01 Friction thermal sca. tstar : -0.12477E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.32893E-04 0.12086E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34500E-08 3 0.27376E-06 0.49560E-12 0.13718E+01 c Velocity[X] 0.34273E-31 c Velocity[Y] 0.24780E-12 c Velocity[Z] 0.24781E-12 c Pressure 0.17575E-13 20 0.60673E-08 0.13764E-06 0.18628E+01 c k 0.56629E-06 2 0.75411E-07 0.12865E-07 0.21881E+01 c omega 0.13153E+02 1 0.34392E-08 0.13148E+01 0.59696E-02 c TempK 0.94500E+02 1 0.19695E-06 0.46683E-01 0.23980E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.2282e-13 1.0159e-13 -1.251e-17 -3.1956e-18 v Velocity[Y] -0.00014525 0.00014154 -1.0927e-09 -4.1038e-12 v Velocity[Z] -0.00014153 0.00014525 9.3579e-10 -1.886e-12 v ǁVelocityǁ 3.6562e-10 0.00015721 1.0371e-05 6.0074e-06 v Pressure -0.00073794 0.016871 0.00088599 -6.3979e-20 v k 3.2944e-09 0.0018473 0.0012949 0.0016059 v omega 21.835 1.0313e+05 2671.3 505.94 v TempK 288 341.78 293.07 290.24 v Density 1.205 1.205 1.205 1.205 v TurbVisc 3.8716e-14 9.927e-05 6.5193e-05 8.3596e-05 v CourantNb 1.7437e-09 0.00024916 1.4577e-05 7.6554e-06 v FourierNb 0.12849 0.6281 0.20522 0.17514 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9277 4.9278 0.00045388 -4.1727e-07 v volume_forces[Z] -4.9277 4.9278 -0.00045373 5.0521e-07 v ǁvolume_forcesǁ 1.3078e-08 4.9292 0.46057 0.20246 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.29 290.39 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.017208 6.0111e-05 3.3882e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.12849 0.6281 0.20523 0.17515 INSTANT 0.421794000E+00 TIME STEP NUMBER 438 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.70711E-05 0.25852E-02 Friction velocity uk : 0.70763E-05 0.25851E-02 Dimensionless distance yplus : 0.47121E-04 0.17199E-01 Friction thermal sca. tstar : -0.12278E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.33095E-04 0.12079E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.70711E-05 0.25852E-02 Friction velocity uk : 0.70763E-05 0.25851E-02 Dimensionless distance yplus : 0.47121E-04 0.17199E-01 Friction thermal sca. tstar : -0.12278E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.33095E-04 0.12079E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34491E-08 3 0.27283E-06 0.49303E-12 0.13689E+01 c Velocity[X] 0.34011E-31 c Velocity[Y] 0.24651E-12 c Velocity[Z] 0.24652E-12 c Pressure 0.17461E-13 20 0.60564E-08 0.13675E-06 0.18583E+01 c k 0.56513E-06 2 0.75174E-07 0.12768E-07 0.21843E+01 c omega 0.13153E+02 1 0.34249E-08 0.13057E+01 0.59487E-02 c TempK 0.94501E+02 1 0.19632E-06 0.46525E-01 0.23939E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.2269e-13 1.0148e-13 -1.2497e-17 -3.1926e-18 v Velocity[Y] -0.00014514 0.00014142 -1.0928e-09 -4.2948e-12 v Velocity[Z] -0.00014141 0.00014514 9.352e-10 -1.9101e-12 v ǁVelocityǁ 3.6949e-10 0.00015708 1.037e-05 6.0106e-06 v Pressure -0.00073965 0.01689 0.00088734 8.0796e-20 v k 3.2755e-09 0.0018432 0.001292 0.0016025 v omega 21.797 1.0313e+05 2671.3 505.9 v TempK 288 341.79 293.08 290.25 v Density 1.205 1.205 1.205 1.205 v TurbVisc 3.8493e-14 9.9253e-05 6.516e-05 8.3561e-05 v CourantNb 1.7477e-09 0.00024891 1.457e-05 7.655e-06 v FourierNb 0.12839 0.6281 0.20514 0.17507 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9279 4.9279 0.00045421 -4.1783e-07 v volume_forces[Z] -4.9279 4.9279 -0.00045406 5.0585e-07 v ǁvolume_forcesǁ 1.3217e-08 4.9294 0.4609 0.20269 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.3 290.39 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.017199 6.0084e-05 3.3865e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.1284 0.6281 0.20515 0.17508 INSTANT 0.422757000E+00 TIME STEP NUMBER 439 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.71141E-05 0.25838E-02 Friction velocity uk : 0.71193E-05 0.25837E-02 Dimensionless distance yplus : 0.47407E-04 0.17189E-01 Friction thermal sca. tstar : -0.12088E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.33295E-04 0.12073E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.71141E-05 0.25838E-02 Friction velocity uk : 0.71193E-05 0.25837E-02 Dimensionless distance yplus : 0.47407E-04 0.17189E-01 Friction thermal sca. tstar : -0.12088E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.33295E-04 0.12073E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34482E-08 3 0.27205E-06 0.49050E-12 0.13660E+01 c Velocity[X] 0.33754E-31 c Velocity[Y] 0.24525E-12 c Velocity[Z] 0.24526E-12 c Pressure 0.17547E-13 20 0.60539E-08 0.13742E-06 0.18539E+01 c k 0.56398E-06 2 0.74939E-07 0.12671E-07 0.21805E+01 c omega 0.13153E+02 1 0.34108E-08 0.12966E+01 0.59279E-02 c TempK 0.94501E+02 1 0.19570E-06 0.46369E-01 0.23899E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.2255e-13 1.0137e-13 -1.2485e-17 -3.1895e-18 v Velocity[Y] -0.00014503 0.0001413 -1.0928e-09 -4.2851e-12 v Velocity[Z] -0.00014129 0.00014503 9.3463e-10 -1.912e-12 v ǁVelocityǁ 3.7353e-10 0.00015694 1.0368e-05 6.0139e-06 v Pressure -0.00074135 0.01691 0.00088868 -6.8637e-21 v k 3.2567e-09 0.0018392 0.0012891 0.0015991 v omega 21.76 1.0313e+05 2671.3 505.87 v TempK 288 341.79 293.08 290.25 v Density 1.205 1.205 1.205 1.205 v TurbVisc 3.8272e-14 9.9236e-05 6.5127e-05 8.3526e-05 v CourantNb 1.7518e-09 0.00024866 1.4562e-05 7.6546e-06 v FourierNb 0.1283 0.6281 0.20506 0.175 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.928 4.928 0.00045454 -4.184e-07 v volume_forces[Z] -4.928 4.928 -0.00045439 5.065e-07 v ǁvolume_forcesǁ 1.3357e-08 4.9295 0.46123 0.20292 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.3 290.39 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.017189 6.0056e-05 3.3848e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.12831 0.6281 0.20507 0.17501 INSTANT 0.423720000E+00 TIME STEP NUMBER 440 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.71587E-05 0.25823E-02 Friction velocity uk : 0.71638E-05 0.25823E-02 Dimensionless distance yplus : 0.47703E-04 0.17180E-01 Friction thermal sca. tstar : -0.11905E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.33504E-04 0.12066E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.71587E-05 0.25823E-02 Friction velocity uk : 0.71638E-05 0.25823E-02 Dimensionless distance yplus : 0.47703E-04 0.17180E-01 Friction thermal sca. tstar : -0.11905E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.33504E-04 0.12066E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34473E-08 3 0.27110E-06 0.48801E-12 0.13632E+01 c Velocity[X] 0.33500E-31 c Velocity[Y] 0.24400E-12 c Velocity[Z] 0.24401E-12 c Pressure 0.17329E-13 20 0.60278E-08 0.13570E-06 0.18496E+01 c k 0.56283E-06 2 0.74704E-07 0.12575E-07 0.21768E+01 c omega 0.13153E+02 1 0.33967E-08 0.12876E+01 0.59073E-02 c TempK 0.94502E+02 1 0.19509E-06 0.46214E-01 0.23859E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.2242e-13 1.0127e-13 -1.2472e-17 -3.1865e-18 v Velocity[Y] -0.00014492 0.00014118 -1.0927e-09 -4.2732e-12 v Velocity[Z] -0.00014117 0.00014493 9.3405e-10 -1.9152e-12 v ǁVelocityǁ 3.7751e-10 0.00015681 1.0367e-05 6.0172e-06 v Pressure -0.00074305 0.016929 0.00089003 -6.6088e-20 v k 3.238e-09 0.0018352 0.0012862 0.0015957 v omega 21.722 1.0313e+05 2671.2 505.83 v TempK 288 341.79 293.08 290.25 v Density 1.205 1.205 1.205 1.205 v TurbVisc 3.8052e-14 9.9219e-05 6.5095e-05 8.3491e-05 v CourantNb 1.7558e-09 0.00024841 1.4555e-05 7.6543e-06 v FourierNb 0.12821 0.6281 0.20498 0.17494 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9281 4.9281 0.00045486 -4.1896e-07 v volume_forces[Z] -4.9281 4.9281 -0.00045471 5.0714e-07 v ǁvolume_forcesǁ 1.3503e-08 4.9296 0.46156 0.20316 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.3 290.4 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.01718 6.0029e-05 3.3832e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.12821 0.6281 0.205 0.17494 INSTANT 0.424683000E+00 TIME STEP NUMBER 441 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.72024E-05 0.25809E-02 Friction velocity uk : 0.72074E-05 0.25808E-02 Dimensionless distance yplus : 0.47994E-04 0.17170E-01 Friction thermal sca. tstar : -0.11731E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.33708E-04 0.12059E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.72024E-05 0.25809E-02 Friction velocity uk : 0.72074E-05 0.25808E-02 Dimensionless distance yplus : 0.47994E-04 0.17170E-01 Friction thermal sca. tstar : -0.11731E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.33708E-04 0.12059E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34465E-08 3 0.27023E-06 0.48556E-12 0.13604E+01 c Velocity[X] 0.33248E-31 c Velocity[Y] 0.24277E-12 c Velocity[Z] 0.24278E-12 c Pressure 0.17267E-13 20 0.60173E-08 0.13521E-06 0.18452E+01 c k 0.56169E-06 2 0.74472E-07 0.12480E-07 0.21730E+01 c omega 0.13153E+02 1 0.33826E-08 0.12786E+01 0.58868E-02 c TempK 0.94503E+02 1 0.19447E-06 0.46059E-01 0.23818E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.2229e-13 1.0116e-13 -1.246e-17 -3.1835e-18 v Velocity[Y] -0.00014481 0.00014106 -1.0926e-09 -4.2686e-12 v Velocity[Z] -0.00014106 0.00014482 9.3346e-10 -1.9265e-12 v ǁVelocityǁ 3.8147e-10 0.00015668 1.0365e-05 6.0206e-06 v Pressure -0.00074476 0.016948 0.00089137 1.0041e-19 v k 3.2195e-09 0.0018312 0.0012834 0.0015923 v omega 21.685 1.0313e+05 2671.2 505.8 v TempK 288 341.79 293.09 290.26 v Density 1.205 1.205 1.205 1.205 v TurbVisc 3.7834e-14 9.9202e-05 6.5062e-05 8.3456e-05 v CourantNb 1.7598e-09 0.00024816 1.4547e-05 7.654e-06 v FourierNb 0.12812 0.6281 0.2049 0.17487 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9282 4.9283 0.00045519 -4.1952e-07 v volume_forces[Z] -4.9282 4.9283 -0.00045504 5.0777e-07 v ǁvolume_forcesǁ 1.3647e-08 4.9297 0.46188 0.20339 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.31 290.4 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.01717 6.0002e-05 3.3816e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.12812 0.6281 0.20492 0.17487 INSTANT 0.425646000E+00 TIME STEP NUMBER 442 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.72456E-05 0.25795E-02 Friction velocity uk : 0.72506E-05 0.25794E-02 Dimensionless distance yplus : 0.48281E-04 0.17161E-01 Friction thermal sca. tstar : -0.11563E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.33909E-04 0.12053E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.72456E-05 0.25795E-02 Friction velocity uk : 0.72506E-05 0.25794E-02 Dimensionless distance yplus : 0.48281E-04 0.17161E-01 Friction thermal sca. tstar : -0.11563E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.33909E-04 0.12053E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34456E-08 3 0.26937E-06 0.48314E-12 0.13576E+01 c Velocity[X] 0.33000E-31 c Velocity[Y] 0.24156E-12 c Velocity[Z] 0.24157E-12 c Pressure 0.17209E-13 20 0.60041E-08 0.13476E-06 0.18409E+01 c k 0.56055E-06 2 0.74240E-07 0.12386E-07 0.21693E+01 c omega 0.13153E+02 1 0.33687E-08 0.12698E+01 0.58663E-02 c TempK 0.94503E+02 1 0.19386E-06 0.45906E-01 0.23778E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.2215e-13 1.0106e-13 -1.2447e-17 -3.1805e-18 v Velocity[Y] -0.0001447 0.00014094 -1.0925e-09 -4.2577e-12 v Velocity[Z] -0.00014094 0.00014471 9.3286e-10 -1.9292e-12 v ǁVelocityǁ 3.8543e-10 0.00015655 1.0364e-05 6.0239e-06 v Pressure -0.00074646 0.016968 0.00089271 1.51e-20 v k 3.2012e-09 0.0018272 0.0012805 0.001589 v omega 21.648 1.0313e+05 2671.2 505.77 v TempK 288 341.79 293.09 290.26 v Density 1.205 1.205 1.205 1.205 v TurbVisc 3.7618e-14 9.9185e-05 6.503e-05 8.3421e-05 v CourantNb 1.7639e-09 0.00024791 1.454e-05 7.6538e-06 v FourierNb 0.12803 0.6281 0.20483 0.1748 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9283 4.9284 0.00045551 -4.2008e-07 v volume_forces[Z] -4.9283 4.9284 -0.00045537 5.0841e-07 v ǁvolume_forcesǁ 1.379e-08 4.9298 0.46221 0.20362 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.31 290.4 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.017161 5.9974e-05 3.3799e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.12803 0.6281 0.20484 0.17481 INSTANT 0.426609000E+00 TIME STEP NUMBER 443 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.72883E-05 0.25781E-02 Friction velocity uk : 0.72932E-05 0.25780E-02 Dimensionless distance yplus : 0.48565E-04 0.17152E-01 Friction thermal sca. tstar : -0.11401E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.34109E-04 0.12046E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.72883E-05 0.25781E-02 Friction velocity uk : 0.72932E-05 0.25780E-02 Dimensionless distance yplus : 0.48565E-04 0.17152E-01 Friction thermal sca. tstar : -0.11401E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.34109E-04 0.12046E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34448E-08 3 0.26851E-06 0.48075E-12 0.13549E+01 c Velocity[X] 0.32755E-31 c Velocity[Y] 0.24037E-12 c Velocity[Z] 0.24038E-12 c Pressure 0.17144E-13 20 0.59896E-08 0.13424E-06 0.18365E+01 c k 0.55941E-06 2 0.74010E-07 0.12293E-07 0.21655E+01 c omega 0.13153E+02 1 0.33549E-08 0.12610E+01 0.58460E-02 c TempK 0.94504E+02 1 0.19326E-06 0.45753E-01 0.23739E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.2202e-13 1.0095e-13 -1.2435e-17 -3.1775e-18 v Velocity[Y] -0.0001446 0.00014083 -1.0924e-09 -4.2467e-12 v Velocity[Z] -0.00014082 0.0001446 9.3225e-10 -1.9318e-12 v ǁVelocityǁ 3.8938e-10 0.00015642 1.0362e-05 6.0273e-06 v Pressure -0.00074817 0.016987 0.00089405 3.6083e-20 v k 3.183e-09 0.0018232 0.0012777 0.0015856 v omega 21.611 1.0313e+05 2671.2 505.73 v TempK 288 341.79 293.1 290.26 v Density 1.205 1.205 1.205 1.205 v TurbVisc 3.7403e-14 9.9168e-05 6.4997e-05 8.3386e-05 v CourantNb 1.7679e-09 0.00024766 1.4533e-05 7.6535e-06 v FourierNb 0.12794 0.6281 0.20475 0.17473 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9285 4.9285 0.00045584 -4.2063e-07 v volume_forces[Z] -4.9285 4.9285 -0.00045569 5.0904e-07 v ǁvolume_forcesǁ 1.3933e-08 4.9299 0.46253 0.20386 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.31 290.4 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.017152 5.9947e-05 3.3783e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.12794 0.6281 0.20476 0.17474 INSTANT 0.427572000E+00 TIME STEP NUMBER 444 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.73308E-05 0.25767E-02 Friction velocity uk : 0.73356E-05 0.25766E-02 Dimensionless distance yplus : 0.48847E-04 0.17142E-01 Friction thermal sca. tstar : -0.11246E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.34307E-04 0.12040E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.73308E-05 0.25767E-02 Friction velocity uk : 0.73356E-05 0.25766E-02 Dimensionless distance yplus : 0.48847E-04 0.17142E-01 Friction thermal sca. tstar : -0.11246E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.34307E-04 0.12040E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34440E-08 3 0.26779E-06 0.47841E-12 0.13522E+01 c Velocity[X] 0.32513E-31 c Velocity[Y] 0.23920E-12 c Velocity[Z] 0.23921E-12 c Pressure 0.17230E-13 20 0.59863E-08 0.13491E-06 0.18322E+01 c k 0.55828E-06 2 0.73781E-07 0.12201E-07 0.21618E+01 c omega 0.13153E+02 1 0.33411E-08 0.12523E+01 0.58258E-02 c TempK 0.94505E+02 1 0.19265E-06 0.45601E-01 0.23699E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.2189e-13 1.0085e-13 -1.2422e-17 -3.1745e-18 v Velocity[Y] -0.00014449 0.00014071 -1.0923e-09 -4.2362e-12 v Velocity[Z] -0.0001407 0.00014449 9.3163e-10 -1.9345e-12 v ǁVelocityǁ 3.9333e-10 0.00015629 1.0361e-05 6.0308e-06 v Pressure -0.00074987 0.017006 0.00089539 -5.4027e-20 v k 3.1649e-09 0.0018193 0.0012749 0.0015823 v omega 21.574 1.0313e+05 2671.1 505.7 v TempK 288 341.79 293.1 290.26 v Density 1.205 1.205 1.205 1.205 v TurbVisc 3.7191e-14 9.9151e-05 6.4965e-05 8.3351e-05 v CourantNb 1.7719e-09 0.00024742 1.4526e-05 7.6534e-06 v FourierNb 0.12785 0.6281 0.20467 0.17466 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9286 4.9286 0.00045616 -4.2119e-07 v volume_forces[Z] -4.9286 4.9286 -0.00045602 5.0967e-07 v ǁvolume_forcesǁ 1.4076e-08 4.9301 0.46286 0.20409 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.32 290.41 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.017142 5.992e-05 3.3766e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.12785 0.6281 0.20469 0.17467 INSTANT 0.428535000E+00 TIME STEP NUMBER 445 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.73730E-05 0.25753E-02 Friction velocity uk : 0.73777E-05 0.25752E-02 Dimensionless distance yplus : 0.49127E-04 0.17133E-01 Friction thermal sca. tstar : -0.11096E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.34504E-04 0.12033E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.73730E-05 0.25753E-02 Friction velocity uk : 0.73777E-05 0.25752E-02 Dimensionless distance yplus : 0.49127E-04 0.17133E-01 Friction thermal sca. tstar : -0.11096E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.34504E-04 0.12033E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34432E-08 3 0.26682E-06 0.47610E-12 0.13495E+01 c Velocity[X] 0.32274E-31 c Velocity[Y] 0.23804E-12 c Velocity[Z] 0.23806E-12 c Pressure 0.17025E-13 20 0.59622E-08 0.13330E-06 0.18279E+01 c k 0.55715E-06 2 0.73554E-07 0.12109E-07 0.21581E+01 c omega 0.13153E+02 1 0.33274E-08 0.12436E+01 0.58056E-02 c TempK 0.94505E+02 1 0.19205E-06 0.45450E-01 0.23659E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.2175e-13 1.0074e-13 -1.241e-17 -3.1715e-18 v Velocity[Y] -0.00014438 0.00014059 -1.0921e-09 -4.225e-12 v Velocity[Z] -0.00014059 0.00014439 9.31e-10 -1.9372e-12 v ǁVelocityǁ 3.973e-10 0.00015616 1.036e-05 6.0342e-06 v Pressure -0.00075157 0.017026 0.00089673 -2.2944e-20 v k 3.1469e-09 0.0018155 0.0012721 0.001579 v omega 21.537 1.0313e+05 2671.1 505.67 v TempK 288 341.79 293.1 290.27 v Density 1.205 1.205 1.205 1.205 v TurbVisc 3.6979e-14 9.9134e-05 6.4933e-05 8.3317e-05 v CourantNb 1.776e-09 0.00024717 1.4519e-05 7.6532e-06 v FourierNb 0.12776 0.6281 0.20459 0.17459 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9287 4.9287 0.00045649 -4.2174e-07 v volume_forces[Z] -4.9287 4.9287 -0.00045634 5.103e-07 v ǁvolume_forcesǁ 1.4219e-08 4.9302 0.46318 0.20432 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.32 290.41 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.017133 5.9893e-05 3.375e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.12776 0.6281 0.20461 0.1746 INSTANT 0.429498000E+00 TIME STEP NUMBER 446 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.74151E-05 0.25739E-02 Friction velocity uk : 0.74197E-05 0.25738E-02 Dimensionless distance yplus : 0.49407E-04 0.17124E-01 Friction thermal sca. tstar : -0.10952E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.34700E-04 0.12027E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.74151E-05 0.25739E-02 Friction velocity uk : 0.74197E-05 0.25738E-02 Dimensionless distance yplus : 0.49407E-04 0.17124E-01 Friction thermal sca. tstar : -0.10952E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.34700E-04 0.12027E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34425E-08 3 0.26598E-06 0.47382E-12 0.13469E+01 c Velocity[X] 0.32038E-31 c Velocity[Y] 0.23691E-12 c Velocity[Z] 0.23692E-12 c Pressure 0.16965E-13 20 0.59493E-08 0.13283E-06 0.18237E+01 c k 0.55603E-06 2 0.73328E-07 0.12019E-07 0.21544E+01 c omega 0.13153E+02 1 0.33138E-08 0.12351E+01 0.57856E-02 c TempK 0.94506E+02 1 0.19145E-06 0.45299E-01 0.23620E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.2162e-13 1.0064e-13 -1.2398e-17 -3.1686e-18 v Velocity[Y] -0.00014428 0.00014048 -1.092e-09 -4.2143e-12 v Velocity[Z] -0.00014047 0.00014428 9.3037e-10 -1.9399e-12 v ǁVelocityǁ 4.0128e-10 0.00015603 1.0359e-05 6.0377e-06 v Pressure -0.00075328 0.017045 0.00089806 -4.3143e-20 v k 3.1291e-09 0.0018117 0.0012693 0.0015757 v omega 21.501 1.0313e+05 2671.1 505.63 v TempK 288 341.8 293.11 290.27 v Density 1.205 1.205 1.205 1.205 v TurbVisc 3.677e-14 9.9117e-05 6.4901e-05 8.3282e-05 v CourantNb 1.78e-09 0.00024693 1.4512e-05 7.6531e-06 v FourierNb 0.12767 0.6281 0.20452 0.17452 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9288 4.9288 0.00045681 -4.223e-07 v volume_forces[Z] -4.9288 4.9288 -0.00045666 5.1092e-07 v ǁvolume_forcesǁ 1.4363e-08 4.9303 0.46351 0.20455 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.32 290.41 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.017124 5.9866e-05 3.3734e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.12767 0.6281 0.20453 0.17453 INSTANT 0.430461000E+00 TIME STEP NUMBER 447 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.74569E-05 0.25725E-02 Friction velocity uk : 0.74615E-05 0.25724E-02 Dimensionless distance yplus : 0.49686E-04 0.17114E-01 Friction thermal sca. tstar : -0.10813E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.34896E-04 0.12020E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.74569E-05 0.25725E-02 Friction velocity uk : 0.74615E-05 0.25724E-02 Dimensionless distance yplus : 0.49686E-04 0.17114E-01 Friction thermal sca. tstar : -0.10813E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.34896E-04 0.12020E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34417E-08 3 0.41386E-06 0.47158E-12 0.13443E+01 c Velocity[X] 0.31805E-31 c Velocity[Y] 0.23578E-12 c Velocity[Z] 0.23580E-12 c Pressure 0.16975E-13 20 0.59356E-08 0.13291E-06 0.18194E+01 c k 0.55491E-06 2 0.73103E-07 0.11929E-07 0.21507E+01 c omega 0.13153E+02 1 0.33002E-08 0.12266E+01 0.57657E-02 c TempK 0.94507E+02 1 0.19086E-06 0.45150E-01 0.23581E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.2149e-13 1.0054e-13 -1.2385e-17 -3.1656e-18 v Velocity[Y] -0.00014417 0.00014036 -1.0918e-09 -4.2038e-12 v Velocity[Z] -0.00014036 0.00014417 9.2973e-10 -1.9424e-12 v ǁVelocityǁ 4.0527e-10 0.0001559 1.0357e-05 6.0412e-06 v Pressure -0.00075498 0.017064 0.0008994 -5.4861e-20 v k 3.1115e-09 0.001808 0.0012665 0.0015724 v omega 21.464 1.0313e+05 2671 505.6 v TempK 288 341.8 293.11 290.27 v Density 1.205 1.205 1.205 1.205 v TurbVisc 3.6562e-14 9.91e-05 6.4868e-05 8.3247e-05 v CourantNb 1.784e-09 0.00024668 1.4505e-05 7.653e-06 v FourierNb 0.12758 0.6281 0.20444 0.17446 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9289 4.9289 0.00045713 -4.2285e-07 v volume_forces[Z] -4.9289 4.9289 -0.00045699 5.1155e-07 v ǁvolume_forcesǁ 1.4506e-08 4.9304 0.46383 0.20478 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.33 290.41 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.017114 5.984e-05 3.3718e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.12758 0.6281 0.20445 0.17446 INSTANT 0.431424000E+00 TIME STEP NUMBER 448 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.74986E-05 0.25711E-02 Friction velocity uk : 0.75032E-05 0.25710E-02 Dimensionless distance yplus : 0.49963E-04 0.17105E-01 Friction thermal sca. tstar : -0.10678E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.35091E-04 0.12013E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.74986E-05 0.25711E-02 Friction velocity uk : 0.75032E-05 0.25710E-02 Dimensionless distance yplus : 0.49963E-04 0.17105E-01 Friction thermal sca. tstar : -0.10678E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.35091E-04 0.12013E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34410E-08 3 0.26438E-06 0.46937E-12 0.13417E+01 c Velocity[X] 0.31574E-31 c Velocity[Y] 0.23468E-12 c Velocity[Z] 0.23469E-12 c Pressure 0.16945E-13 20 0.59280E-08 0.13267E-06 0.18152E+01 c k 0.55380E-06 2 0.72880E-07 0.11840E-07 0.21470E+01 c omega 0.13153E+02 1 0.32868E-08 0.12182E+01 0.57459E-02 c TempK 0.94507E+02 1 0.19027E-06 0.45001E-01 0.23542E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.2136e-13 1.0044e-13 -1.2373e-17 -3.1627e-18 v Velocity[Y] -0.00014406 0.00014025 -1.0917e-09 -4.1931e-12 v Velocity[Z] -0.00014024 0.00014407 9.2907e-10 -1.9449e-12 v ǁVelocityǁ 4.0927e-10 0.00015578 1.0356e-05 6.0448e-06 v Pressure -0.00075668 0.017083 0.00090073 1.2041e-19 v k 3.0939e-09 0.0018042 0.0012637 0.0015691 v omega 21.428 1.0313e+05 2671 505.57 v TempK 288 341.8 293.11 290.27 v Density 1.205 1.205 1.205 1.205 v TurbVisc 3.6355e-14 9.9083e-05 6.4836e-05 8.3213e-05 v CourantNb 1.7881e-09 0.00024644 1.4498e-05 7.653e-06 v FourierNb 0.12749 0.6281 0.20436 0.17439 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.929 4.9291 0.00045746 -4.234e-07 v volume_forces[Z] -4.929 4.9291 -0.00045731 5.1217e-07 v ǁvolume_forcesǁ 1.465e-08 4.9305 0.46415 0.20501 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.33 290.42 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.017105 5.9813e-05 3.3702e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.12749 0.6281 0.20438 0.1744 INSTANT 0.432387000E+00 TIME STEP NUMBER 449 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.75402E-05 0.25697E-02 Friction velocity uk : 0.75447E-05 0.25696E-02 Dimensionless distance yplus : 0.50239E-04 0.17096E-01 Friction thermal sca. tstar : -0.10548E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.35285E-04 0.12007E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.75402E-05 0.25697E-02 Friction velocity uk : 0.75447E-05 0.25696E-02 Dimensionless distance yplus : 0.50239E-04 0.17096E-01 Friction thermal sca. tstar : -0.10548E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.35285E-04 0.12007E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34403E-08 3 0.26349E-06 0.46720E-12 0.13392E+01 c Velocity[X] 0.31347E-31 c Velocity[Y] 0.23359E-12 c Velocity[Z] 0.23360E-12 c Pressure 0.16807E-13 20 0.59086E-08 0.13158E-06 0.18110E+01 c k 0.55269E-06 2 0.72658E-07 0.11752E-07 0.21434E+01 c omega 0.13153E+02 1 0.32734E-08 0.12098E+01 0.57262E-02 c TempK 0.94508E+02 1 0.18968E-06 0.44853E-01 0.23503E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.2123e-13 1.0033e-13 -1.2361e-17 -3.1597e-18 v Velocity[Y] -0.00014396 0.00014013 -1.0915e-09 -4.1823e-12 v Velocity[Z] -0.00014013 0.00014396 9.2841e-10 -1.9477e-12 v ǁVelocityǁ 4.1328e-10 0.00015565 1.0355e-05 6.0483e-06 v Pressure -0.00075839 0.017102 0.00090206 7.7462e-21 v k 3.0765e-09 0.0018005 0.0012609 0.0015659 v omega 21.392 1.0313e+05 2671 505.54 v TempK 288 341.8 293.12 290.28 v Density 1.205 1.205 1.205 1.205 v TurbVisc 3.615e-14 9.9067e-05 6.4804e-05 8.3178e-05 v CourantNb 1.7921e-09 0.0002462 1.4491e-05 7.653e-06 v FourierNb 0.1274 0.6281 0.20429 0.17432 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9291 4.9292 0.00045778 -4.2395e-07 v volume_forces[Z] -4.9291 4.9292 -0.00045763 5.128e-07 v ǁvolume_forcesǁ 1.4795e-08 4.9306 0.46447 0.20524 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.33 290.42 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.017096 5.9786e-05 3.3686e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.1274 0.6281 0.2043 0.17433 INSTANT 0.433350000E+00 TIME STEP NUMBER 450 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.75817E-05 0.25683E-02 Friction velocity uk : 0.75861E-05 0.25682E-02 Dimensionless distance yplus : 0.50515E-04 0.17087E-01 Friction thermal sca. tstar : -0.10423E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.35479E-04 0.12001E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.75817E-05 0.25683E-02 Friction velocity uk : 0.75861E-05 0.25682E-02 Dimensionless distance yplus : 0.50515E-04 0.17087E-01 Friction thermal sca. tstar : -0.10423E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.35479E-04 0.12001E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34396E-08 3 0.26267E-06 0.46505E-12 0.13367E+01 c Velocity[X] 0.31123E-31 c Velocity[Y] 0.23252E-12 c Velocity[Z] 0.23253E-12 c Pressure 0.16747E-13 20 0.58935E-08 0.13110E-06 0.18068E+01 c k 0.55158E-06 2 0.72437E-07 0.11665E-07 0.21397E+01 c omega 0.13153E+02 1 0.32601E-08 0.12015E+01 0.57066E-02 c TempK 0.94508E+02 1 0.18909E-06 0.44706E-01 0.23464E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.211e-13 1.0023e-13 -1.2349e-17 -3.1568e-18 v Velocity[Y] -0.00014385 0.00014002 -1.0913e-09 -4.1718e-12 v Velocity[Z] -0.00014001 0.00014386 9.2774e-10 -1.9503e-12 v ǁVelocityǁ 4.1731e-10 0.00015552 1.0354e-05 6.0519e-06 v Pressure -0.00076009 0.017121 0.00090339 3.8143e-20 v k 3.0592e-09 0.0017968 0.0012582 0.0015626 v omega 21.356 1.0313e+05 2671 505.5 v TempK 288 341.8 293.12 290.28 v Density 1.205 1.205 1.205 1.205 v TurbVisc 3.5947e-14 9.905e-05 6.4772e-05 8.3144e-05 v CourantNb 1.7961e-09 0.00024596 1.4484e-05 7.6531e-06 v FourierNb 0.12731 0.6281 0.20421 0.17425 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9293 4.9293 0.0004581 -4.245e-07 v volume_forces[Z] -4.9293 4.9293 -0.00045795 5.1342e-07 v ǁvolume_forcesǁ 1.494e-08 4.9307 0.46479 0.20548 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.34 290.42 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.017087 5.976e-05 3.367e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.12731 0.6281 0.20422 0.17426 INSTANT 0.434313000E+00 TIME STEP NUMBER 451 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.76230E-05 0.25669E-02 Friction velocity uk : 0.76273E-05 0.25669E-02 Dimensionless distance yplus : 0.50790E-04 0.17077E-01 Friction thermal sca. tstar : -0.10301E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.35671E-04 0.11994E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.76230E-05 0.25669E-02 Friction velocity uk : 0.76273E-05 0.25669E-02 Dimensionless distance yplus : 0.50790E-04 0.17077E-01 Friction thermal sca. tstar : -0.10301E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.35671E-04 0.11994E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34389E-08 3 0.26184E-06 0.46294E-12 0.13342E+01 c Velocity[X] 0.30900E-31 c Velocity[Y] 0.23146E-12 c Velocity[Z] 0.23147E-12 c Pressure 0.16675E-13 20 0.58828E-08 0.13054E-06 0.18026E+01 c k 0.55048E-06 2 0.72217E-07 0.11578E-07 0.21361E+01 c omega 0.13153E+02 1 0.32468E-08 0.11933E+01 0.56870E-02 c TempK 0.94509E+02 1 0.18851E-06 0.44560E-01 0.23425E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.2097e-13 1.0013e-13 -1.2337e-17 -3.1539e-18 v Velocity[Y] -0.00014375 0.0001399 -1.0911e-09 -4.1611e-12 v Velocity[Z] -0.0001399 0.00014375 9.2706e-10 -1.9528e-12 v ǁVelocityǁ 4.2134e-10 0.0001554 1.0353e-05 6.0556e-06 v Pressure -0.00076179 0.01714 0.00090472 -2.4121e-20 v k 3.0421e-09 0.001793 0.0012554 0.0015594 v omega 21.32 1.0313e+05 2670.9 505.47 v TempK 288 341.8 293.12 290.28 v Density 1.205 1.205 1.205 1.205 v TurbVisc 3.5745e-14 9.9033e-05 6.4741e-05 8.311e-05 v CourantNb 1.8001e-09 0.00024573 1.4478e-05 7.6532e-06 v FourierNb 0.12722 0.6281 0.20413 0.17419 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9294 4.9294 0.00045842 -4.2504e-07 v volume_forces[Z] -4.9294 4.9294 -0.00045827 5.1404e-07 v ǁvolume_forcesǁ 1.5086e-08 4.9308 0.46512 0.20571 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.34 290.43 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.017077 5.9733e-05 3.3654e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.12723 0.6281 0.20415 0.17419 INSTANT 0.435276000E+00 TIME STEP NUMBER 452 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.76642E-05 0.25656E-02 Friction velocity uk : 0.76685E-05 0.25655E-02 Dimensionless distance yplus : 0.51064E-04 0.17068E-01 Friction thermal sca. tstar : -0.10183E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.35864E-04 0.11988E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.76642E-05 0.25656E-02 Friction velocity uk : 0.76685E-05 0.25655E-02 Dimensionless distance yplus : 0.51064E-04 0.17068E-01 Friction thermal sca. tstar : -0.10183E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.35864E-04 0.11988E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34382E-08 3 0.29742E-06 0.46085E-12 0.13318E+01 c Velocity[X] 0.30681E-31 c Velocity[Y] 0.23042E-12 c Velocity[Z] 0.23043E-12 c Pressure 0.16684E-13 20 0.58722E-08 0.13061E-06 0.17985E+01 c k 0.54938E-06 2 0.71999E-07 0.11492E-07 0.21325E+01 c omega 0.13153E+02 1 0.32337E-08 0.11852E+01 0.56676E-02 c TempK 0.94510E+02 1 0.18793E-06 0.44414E-01 0.23387E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.2085e-13 1.0003e-13 -1.2325e-17 -3.151e-18 v Velocity[Y] -0.00014364 0.00013979 -1.0909e-09 -4.1509e-12 v Velocity[Z] -0.00013978 0.00014365 9.2637e-10 -1.9555e-12 v ǁVelocityǁ 4.2539e-10 0.00015527 1.0352e-05 6.0592e-06 v Pressure -0.00076349 0.01716 0.00090604 -3.8143e-20 v k 3.0251e-09 0.0017893 0.0012527 0.0015562 v omega 21.284 1.0313e+05 2670.9 505.44 v TempK 288 341.8 293.13 290.28 v Density 1.205 1.205 1.205 1.205 v TurbVisc 3.5545e-14 9.9016e-05 6.4709e-05 8.3075e-05 v CourantNb 1.8042e-09 0.00024549 1.4471e-05 7.6533e-06 v FourierNb 0.12713 0.6281 0.20406 0.17412 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9295 4.9295 0.00045874 -4.2559e-07 v volume_forces[Z] -4.9295 4.9295 -0.00045859 5.1465e-07 v ǁvolume_forcesǁ 1.5232e-08 4.931 0.46544 0.20594 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.35 290.43 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.017068 5.9707e-05 3.3638e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.12714 0.6281 0.20407 0.17413 INSTANT 0.436239000E+00 TIME STEP NUMBER 453 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.77052E-05 0.25642E-02 Friction velocity uk : 0.77094E-05 0.25641E-02 Dimensionless distance yplus : 0.51336E-04 0.17059E-01 Friction thermal sca. tstar : -0.10069E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.36055E-04 0.11981E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.77052E-05 0.25642E-02 Friction velocity uk : 0.77094E-05 0.25641E-02 Dimensionless distance yplus : 0.51336E-04 0.17059E-01 Friction thermal sca. tstar : -0.10069E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.36055E-04 0.11981E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34376E-08 3 0.26034E-06 0.45880E-12 0.13294E+01 c Velocity[X] 0.30465E-31 c Velocity[Y] 0.22939E-12 c Velocity[Z] 0.22941E-12 c Pressure 0.16630E-13 20 0.58565E-08 0.13018E-06 0.17944E+01 c k 0.54828E-06 2 0.71782E-07 0.11407E-07 0.21289E+01 c omega 0.13153E+02 1 0.32206E-08 0.11771E+01 0.56483E-02 c TempK 0.94510E+02 1 0.18735E-06 0.44269E-01 0.23348E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.2072e-13 9.9931e-14 -1.2312e-17 -3.1481e-18 v Velocity[Y] -0.00014354 0.00013968 -1.0907e-09 -4.1405e-12 v Velocity[Z] -0.00013967 0.00014354 9.2567e-10 -1.958e-12 v ǁVelocityǁ 4.2945e-10 0.00015514 1.0351e-05 6.0629e-06 v Pressure -0.0007652 0.017179 0.00090737 -3.1328e-20 v k 3.0082e-09 0.0017857 0.00125 0.001553 v omega 21.248 1.0313e+05 2670.9 505.4 v TempK 288 341.8 293.13 290.29 v Density 1.205 1.205 1.205 1.205 v TurbVisc 3.5346e-14 9.9e-05 6.4677e-05 8.3041e-05 v CourantNb 1.8082e-09 0.00024525 1.4465e-05 7.6534e-06 v FourierNb 0.12704 0.6281 0.20398 0.17405 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9296 4.9296 0.00045906 -4.2613e-07 v volume_forces[Z] -4.9296 4.9296 -0.00045891 5.1527e-07 v ǁvolume_forcesǁ 1.5378e-08 4.9311 0.46576 0.20617 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.35 290.43 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.017059 5.968e-05 3.3622e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.12705 0.6281 0.204 0.17406 INSTANT 0.437202000E+00 TIME STEP NUMBER 454 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.77462E-05 0.25628E-02 Friction velocity uk : 0.77503E-05 0.25628E-02 Dimensionless distance yplus : 0.51609E-04 0.17050E-01 Friction thermal sca. tstar : -0.10023E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.36247E-04 0.11975E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.77462E-05 0.25628E-02 Friction velocity uk : 0.77503E-05 0.25628E-02 Dimensionless distance yplus : 0.51609E-04 0.17050E-01 Friction thermal sca. tstar : -0.10023E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.36247E-04 0.11975E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34369E-08 3 0.25942E-06 0.45678E-12 0.13270E+01 c Velocity[X] 0.30251E-31 c Velocity[Y] 0.22838E-12 c Velocity[Z] 0.22839E-12 c Pressure 0.16518E-13 20 0.58418E-08 0.12929E-06 0.17903E+01 c k 0.54719E-06 2 0.71566E-07 0.11323E-07 0.21253E+01 c omega 0.13153E+02 1 0.32076E-08 0.11691E+01 0.56291E-02 c TempK 0.94511E+02 1 0.18678E-06 0.44125E-01 0.23310E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.2059e-13 9.9831e-14 -1.23e-17 -3.1452e-18 v Velocity[Y] -0.00014344 0.00013957 -1.0905e-09 -4.1299e-12 v Velocity[Z] -0.00013956 0.00014344 9.2496e-10 -1.9607e-12 v ǁVelocityǁ 4.3353e-10 0.00015502 1.0351e-05 6.0666e-06 v Pressure -0.0007669 0.017198 0.00090869 -3.5103e-20 v k 2.9915e-09 0.001782 0.0012473 0.0015498 v omega 21.213 1.0313e+05 2670.9 505.37 v TempK 288 341.81 293.13 290.29 v Density 1.205 1.205 1.205 1.205 v TurbVisc 3.5149e-14 9.8983e-05 6.4645e-05 8.3007e-05 v CourantNb 1.8122e-09 0.00024502 1.4458e-05 7.6536e-06 v FourierNb 0.12696 0.6281 0.20391 0.17399 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9297 4.9297 0.00045938 -4.2667e-07 v volume_forces[Z] -4.9297 4.9297 -0.00045923 5.1588e-07 v ǁvolume_forcesǁ 1.5525e-08 4.9312 0.46607 0.2064 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.35 290.43 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.01705 5.9654e-05 3.3606e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.12696 0.6281 0.20392 0.17399 INSTANT 0.438165000E+00 TIME STEP NUMBER 455 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.77870E-05 0.25615E-02 Friction velocity uk : 0.77911E-05 0.25614E-02 Dimensionless distance yplus : 0.51880E-04 0.17041E-01 Friction thermal sca. tstar : -0.10092E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.36437E-04 0.11969E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.77870E-05 0.25615E-02 Friction velocity uk : 0.77911E-05 0.25614E-02 Dimensionless distance yplus : 0.51880E-04 0.17041E-01 Friction thermal sca. tstar : -0.10092E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.36437E-04 0.11969E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34363E-08 3 0.25862E-06 0.45478E-12 0.13246E+01 c Velocity[X] 0.30039E-31 c Velocity[Y] 0.22738E-12 c Velocity[Z] 0.22740E-12 c Pressure 0.16451E-13 20 0.58310E-08 0.12876E-06 0.17862E+01 c k 0.54610E-06 2 0.71351E-07 0.11240E-07 0.21217E+01 c omega 0.13153E+02 1 0.31946E-08 0.11612E+01 0.56100E-02 c TempK 0.94512E+02 1 0.18621E-06 0.43982E-01 0.23272E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.2046e-13 9.9731e-14 -1.2288e-17 -3.1423e-18 v Velocity[Y] -0.00014333 0.00013945 -1.0903e-09 -4.1194e-12 v Velocity[Z] -0.00013945 0.00014334 9.2425e-10 -1.9633e-12 v ǁVelocityǁ 4.3761e-10 0.0001549 1.035e-05 6.0703e-06 v Pressure -0.0007686 0.017217 0.00091001 1.1766e-21 v k 2.9748e-09 0.0017783 0.0012446 0.0015466 v omega 21.177 1.0313e+05 2670.8 505.34 v TempK 288 341.81 293.14 290.29 v Density 1.205 1.205 1.205 1.205 v TurbVisc 3.4953e-14 9.8967e-05 6.4614e-05 8.2973e-05 v CourantNb 1.8162e-09 0.00024478 1.4452e-05 7.6538e-06 v FourierNb 0.12687 0.6281 0.20383 0.17392 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9298 4.9299 0.0004597 -4.2721e-07 v volume_forces[Z] -4.9298 4.9299 -0.00045955 5.165e-07 v ǁvolume_forcesǁ 1.5672e-08 4.9313 0.46639 0.20662 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.36 290.44 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.017041 5.9628e-05 3.359e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.12687 0.6281 0.20385 0.17393 INSTANT 0.439128000E+00 TIME STEP NUMBER 456 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.78277E-05 0.25601E-02 Friction velocity uk : 0.78317E-05 0.25600E-02 Dimensionless distance yplus : 0.52150E-04 0.17032E-01 Friction thermal sca. tstar : -0.10162E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.36627E-04 0.11962E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.78277E-05 0.25601E-02 Friction velocity uk : 0.78317E-05 0.25600E-02 Dimensionless distance yplus : 0.52150E-04 0.17032E-01 Friction thermal sca. tstar : -0.10162E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.36627E-04 0.11962E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34357E-08 3 0.25783E-06 0.45281E-12 0.13223E+01 c Velocity[X] 0.29831E-31 c Velocity[Y] 0.22640E-12 c Velocity[Z] 0.22641E-12 c Pressure 0.16401E-13 20 0.58173E-08 0.12837E-06 0.17821E+01 c k 0.54502E-06 2 0.71138E-07 0.11157E-07 0.21182E+01 c omega 0.13153E+02 1 0.31818E-08 0.11533E+01 0.55909E-02 c TempK 0.94512E+02 1 0.18564E-06 0.43840E-01 0.23234E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.2034e-13 9.9632e-14 -1.2277e-17 -3.1394e-18 v Velocity[Y] -0.00014323 0.00013934 -1.09e-09 -4.1091e-12 v Velocity[Z] -0.00013934 0.00014324 9.2352e-10 -1.9658e-12 v ǁVelocityǁ 4.4171e-10 0.00015477 1.0349e-05 6.0741e-06 v Pressure -0.0007703 0.017236 0.00091133 -4.1869e-20 v k 2.9583e-09 0.0017747 0.0012419 0.0015434 v omega 21.142 1.0313e+05 2670.8 505.31 v TempK 288 341.81 293.14 290.29 v Density 1.205 1.205 1.205 1.205 v TurbVisc 3.4759e-14 9.895e-05 6.4582e-05 8.2939e-05 v CourantNb 1.8202e-09 0.00024455 1.4445e-05 7.6541e-06 v FourierNb 0.12678 0.6281 0.20376 0.17385 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9299 4.93 0.00046001 -4.2775e-07 v volume_forces[Z] -4.9299 4.93 -0.00045987 5.1711e-07 v ǁvolume_forcesǁ 1.582e-08 4.9314 0.46671 0.20685 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.36 290.44 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.017032 5.9601e-05 3.3574e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.12678 0.6281 0.20377 0.17386 INSTANT 0.440091000E+00 TIME STEP NUMBER 457 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.78682E-05 0.25588E-02 Friction velocity uk : 0.78722E-05 0.25587E-02 Dimensionless distance yplus : 0.52420E-04 0.17023E-01 Friction thermal sca. tstar : -0.10233E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.36817E-04 0.11956E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.78682E-05 0.25588E-02 Friction velocity uk : 0.78722E-05 0.25587E-02 Dimensionless distance yplus : 0.52420E-04 0.17023E-01 Friction thermal sca. tstar : -0.10233E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.36817E-04 0.11956E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34351E-08 3 0.25704E-06 0.45087E-12 0.13200E+01 c Velocity[X] 0.29624E-31 c Velocity[Y] 0.22543E-12 c Velocity[Z] 0.22544E-12 c Pressure 0.16349E-13 20 0.58046E-08 0.12796E-06 0.17780E+01 c k 0.54394E-06 2 0.70926E-07 0.11075E-07 0.21146E+01 c omega 0.13153E+02 1 0.31690E-08 0.11455E+01 0.55720E-02 c TempK 0.94513E+02 1 0.18508E-06 0.43698E-01 0.23196E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.2021e-13 9.9533e-14 -1.2265e-17 -3.1365e-18 v Velocity[Y] -0.00014313 0.00013923 -1.0898e-09 -4.0987e-12 v Velocity[Z] -0.00013923 0.00014313 9.2279e-10 -1.9683e-12 v ǁVelocityǁ 4.4582e-10 0.00015465 1.0348e-05 6.0779e-06 v Pressure -0.000772 0.017255 0.00091265 -3.9025e-20 v k 2.9419e-09 0.001771 0.0012392 0.0015402 v omega 21.106 1.0313e+05 2670.8 505.28 v TempK 288 341.81 293.15 290.3 v Density 1.205 1.205 1.205 1.205 v TurbVisc 3.4566e-14 9.8933e-05 6.4551e-05 8.2905e-05 v CourantNb 1.8243e-09 0.00024432 1.4439e-05 7.6544e-06 v FourierNb 0.12669 0.6281 0.20368 0.17379 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.93 4.9301 0.00046033 -4.2829e-07 v volume_forces[Z] -4.93 4.9301 -0.00046018 5.1772e-07 v ǁvolume_forcesǁ 1.5968e-08 4.9315 0.46703 0.20708 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.36 290.44 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.017023 5.9575e-05 3.3558e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.12669 0.6281 0.2037 0.17379 INSTANT 0.441054000E+00 TIME STEP NUMBER 458 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.79087E-05 0.25574E-02 Friction velocity uk : 0.79126E-05 0.25573E-02 Dimensionless distance yplus : 0.52689E-04 0.17014E-01 Friction thermal sca. tstar : -0.10306E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.37006E-04 0.11950E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.79087E-05 0.25574E-02 Friction velocity uk : 0.79126E-05 0.25573E-02 Dimensionless distance yplus : 0.52689E-04 0.17014E-01 Friction thermal sca. tstar : -0.10306E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.37006E-04 0.11950E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34346E-08 3 0.25626E-06 0.44896E-12 0.13177E+01 c Velocity[X] 0.29420E-31 c Velocity[Y] 0.22447E-12 c Velocity[Z] 0.22448E-12 c Pressure 0.16323E-13 20 0.57893E-08 0.12776E-06 0.17740E+01 c k 0.54287E-06 2 0.70715E-07 0.10994E-07 0.21111E+01 c omega 0.13153E+02 1 0.31562E-08 0.11378E+01 0.55532E-02 c TempK 0.94514E+02 1 0.18451E-06 0.43557E-01 0.23159E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.2009e-13 9.9434e-14 -1.2253e-17 -3.1337e-18 v Velocity[Y] -0.00014303 0.00013912 -1.0895e-09 -4.0884e-12 v Velocity[Z] -0.00013912 0.00014303 9.2205e-10 -1.9709e-12 v ǁVelocityǁ 4.4994e-10 0.00015453 1.0347e-05 6.0817e-06 v Pressure -0.00077371 0.017274 0.00091397 -4.2359e-20 v k 2.9257e-09 0.0017674 0.0012365 0.0015371 v omega 21.071 1.0313e+05 2670.8 505.24 v TempK 288 341.81 293.15 290.3 v Density 1.205 1.205 1.205 1.205 v TurbVisc 3.4374e-14 9.8917e-05 6.452e-05 8.2871e-05 v CourantNb 1.8283e-09 0.00024409 1.4433e-05 7.6547e-06 v FourierNb 0.1266 0.6281 0.20361 0.17372 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9302 4.9302 0.00046065 -4.2883e-07 v volume_forces[Z] -4.9302 4.9302 -0.0004605 5.1832e-07 v ǁvolume_forcesǁ 1.6116e-08 4.9316 0.46735 0.20731 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.37 290.44 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.017014 5.9549e-05 3.3543e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.1266 0.6281 0.20362 0.17373 INSTANT 0.442017000E+00 TIME STEP NUMBER 459 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.79490E-05 0.25561E-02 Friction velocity uk : 0.79529E-05 0.25560E-02 Dimensionless distance yplus : 0.52958E-04 0.17005E-01 Friction thermal sca. tstar : -0.10380E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.37194E-04 0.11943E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.79490E-05 0.25561E-02 Friction velocity uk : 0.79529E-05 0.25560E-02 Dimensionless distance yplus : 0.52958E-04 0.17005E-01 Friction thermal sca. tstar : -0.10380E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.37194E-04 0.11943E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34340E-08 3 0.25560E-06 0.44707E-12 0.13155E+01 c Velocity[X] 0.29218E-31 c Velocity[Y] 0.22353E-12 c Velocity[Z] 0.22354E-12 c Pressure 0.16418E-13 20 0.58018E-08 0.12849E-06 0.17700E+01 c k 0.54180E-06 2 0.70505E-07 0.10914E-07 0.21075E+01 c omega 0.13153E+02 1 0.31436E-08 0.11301E+01 0.55344E-02 c TempK 0.94514E+02 1 0.18395E-06 0.43417E-01 0.23121E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.1996e-13 9.9336e-14 -1.2241e-17 -3.1308e-18 v Velocity[Y] -0.00014293 0.00013901 -1.0893e-09 -4.0785e-12 v Velocity[Z] -0.00013901 0.00014293 9.213e-10 -1.9733e-12 v ǁVelocityǁ 4.5408e-10 0.0001544 1.0347e-05 6.0855e-06 v Pressure -0.00077541 0.017292 0.00091528 2.618e-20 v k 2.9095e-09 0.0017638 0.0012339 0.0015339 v omega 21.036 1.0313e+05 2670.7 505.21 v TempK 288 341.81 293.15 290.3 v Density 1.205 1.205 1.205 1.205 v TurbVisc 3.4184e-14 9.89e-05 6.4488e-05 8.2837e-05 v CourantNb 1.8323e-09 0.00024386 1.4426e-05 7.655e-06 v FourierNb 0.12651 0.6281 0.20354 0.17365 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9303 4.9303 0.00046096 -4.2936e-07 v volume_forces[Z] -4.9303 4.9303 -0.00046082 5.1893e-07 v ǁvolume_forcesǁ 1.6266e-08 4.9317 0.46766 0.20754 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.37 290.45 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.017005 5.9523e-05 3.3527e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.12652 0.6281 0.20355 0.17366 INSTANT 0.442980000E+00 TIME STEP NUMBER 460 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.79892E-05 0.25548E-02 Friction velocity uk : 0.79930E-05 0.25547E-02 Dimensionless distance yplus : 0.53225E-04 0.16996E-01 Friction thermal sca. tstar : -0.10457E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.37382E-04 0.11937E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.79892E-05 0.25548E-02 Friction velocity uk : 0.79930E-05 0.25547E-02 Dimensionless distance yplus : 0.53225E-04 0.16996E-01 Friction thermal sca. tstar : -0.10457E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.37382E-04 0.11937E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34335E-08 3 0.25468E-06 0.44521E-12 0.13132E+01 c Velocity[X] 0.29019E-31 c Velocity[Y] 0.22260E-12 c Velocity[Z] 0.22261E-12 c Pressure 0.16184E-13 20 0.57676E-08 0.12666E-06 0.17659E+01 c k 0.54073E-06 2 0.70296E-07 0.10834E-07 0.21040E+01 c omega 0.13153E+02 1 0.31310E-08 0.11225E+01 0.55158E-02 c TempK 0.94515E+02 1 0.18340E-06 0.43278E-01 0.23084E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.1984e-13 9.9238e-14 -1.2229e-17 -3.128e-18 v Velocity[Y] -0.00014283 0.0001389 -1.089e-09 -4.0679e-12 v Velocity[Z] -0.0001389 0.00014283 9.2054e-10 -1.9758e-12 v ǁVelocityǁ 4.5823e-10 0.00015428 1.0346e-05 6.0894e-06 v Pressure -0.00077711 0.017311 0.0009166 -6.8637e-22 v k 2.8935e-09 0.0017602 0.0012312 0.0015308 v omega 21.001 1.0313e+05 2670.7 505.18 v TempK 288 341.81 293.16 290.3 v Density 1.205 1.205 1.205 1.205 v TurbVisc 3.3996e-14 9.8884e-05 6.4457e-05 8.2803e-05 v CourantNb 1.8363e-09 0.00024363 1.442e-05 7.6554e-06 v FourierNb 0.12643 0.6281 0.20346 0.17359 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9304 4.9304 0.00046128 -4.2989e-07 v volume_forces[Z] -4.9304 4.9304 -0.00046113 5.1954e-07 v ǁvolume_forcesǁ 1.6415e-08 4.9318 0.46798 0.20777 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.37 290.45 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.016996 5.9497e-05 3.3511e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.12643 0.6281 0.20348 0.1736 INSTANT 0.443943000E+00 TIME STEP NUMBER 461 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.80294E-05 0.25534E-02 Friction velocity uk : 0.80332E-05 0.25533E-02 Dimensionless distance yplus : 0.53492E-04 0.16988E-01 Friction thermal sca. tstar : -0.10536E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.37569E-04 0.11931E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.80294E-05 0.25534E-02 Friction velocity uk : 0.80332E-05 0.25533E-02 Dimensionless distance yplus : 0.53492E-04 0.16988E-01 Friction thermal sca. tstar : -0.10536E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.37569E-04 0.11931E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34329E-08 3 0.25392E-06 0.44338E-12 0.13110E+01 c Velocity[X] 0.28822E-31 c Velocity[Y] 0.22168E-12 c Velocity[Z] 0.22169E-12 c Pressure 0.16142E-13 20 0.57532E-08 0.12633E-06 0.17620E+01 c k 0.53966E-06 2 0.70089E-07 0.10755E-07 0.21005E+01 c omega 0.13153E+02 1 0.31185E-08 0.11150E+01 0.54972E-02 c TempK 0.94516E+02 1 0.18284E-06 0.43139E-01 0.23047E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.1971e-13 9.9141e-14 -1.2217e-17 -3.1252e-18 v Velocity[Y] -0.00014273 0.00013879 -1.0887e-09 -4.0577e-12 v Velocity[Z] -0.00013879 0.00014273 9.1977e-10 -1.9782e-12 v ǁVelocityǁ 4.6239e-10 0.00015416 1.0346e-05 6.0932e-06 v Pressure -0.00077881 0.01733 0.00091791 -6.7558e-20 v k 2.8776e-09 0.0017566 0.0012286 0.0015277 v omega 20.967 1.0313e+05 2670.7 505.15 v TempK 288 341.81 293.16 290.31 v Density 1.205 1.205 1.205 1.205 v TurbVisc 3.3809e-14 9.8868e-05 6.4426e-05 8.277e-05 v CourantNb 1.8403e-09 0.0002434 1.4414e-05 7.6558e-06 v FourierNb 0.12634 0.6281 0.20339 0.17352 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9305 4.9305 0.00046159 -4.3043e-07 v volume_forces[Z] -4.9305 4.9305 -0.00046145 5.2014e-07 v ǁvolume_forcesǁ 1.6565e-08 4.9319 0.46829 0.208 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.38 290.45 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.016988 5.9472e-05 3.3496e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.12634 0.6281 0.2034 0.17353 INSTANT 0.444906000E+00 TIME STEP NUMBER 462 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.80694E-05 0.25521E-02 Friction velocity uk : 0.80731E-05 0.25520E-02 Dimensionless distance yplus : 0.53758E-04 0.16979E-01 Friction thermal sca. tstar : -0.10616E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.37756E-04 0.11925E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.80694E-05 0.25521E-02 Friction velocity uk : 0.80731E-05 0.25520E-02 Dimensionless distance yplus : 0.53758E-04 0.16979E-01 Friction thermal sca. tstar : -0.10616E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.37756E-04 0.11925E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34324E-08 3 0.25313E-06 0.44157E-12 0.13088E+01 c Velocity[X] 0.28627E-31 c Velocity[Y] 0.22078E-12 c Velocity[Z] 0.22079E-12 c Pressure 0.16074E-13 20 0.57435E-08 0.12579E-06 0.17580E+01 c k 0.53860E-06 2 0.69883E-07 0.10677E-07 0.20970E+01 c omega 0.13153E+02 1 0.31061E-08 0.11075E+01 0.54787E-02 c TempK 0.94516E+02 1 0.18229E-06 0.43001E-01 0.23010E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.1959e-13 9.9044e-14 -1.2206e-17 -3.1223e-18 v Velocity[Y] -0.00014263 0.00013868 -1.0884e-09 -4.0475e-12 v Velocity[Z] -0.00013868 0.00014263 9.1899e-10 -1.9807e-12 v ǁVelocityǁ 4.6656e-10 0.00015404 1.0345e-05 6.0972e-06 v Pressure -0.00078051 0.017349 0.00091922 3.2259e-20 v k 2.8618e-09 0.001753 0.001226 0.0015246 v omega 20.932 1.0313e+05 2670.7 505.12 v TempK 288 341.81 293.16 290.31 v Density 1.205 1.205 1.205 1.205 v TurbVisc 3.3623e-14 9.8851e-05 6.4395e-05 8.2736e-05 v CourantNb 1.8443e-09 0.00024317 1.4408e-05 7.6562e-06 v FourierNb 0.12625 0.6281 0.20331 0.17346 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9306 4.9306 0.00046191 -4.3096e-07 v volume_forces[Z] -4.9306 4.9306 -0.00046176 5.2074e-07 v ǁvolume_forcesǁ 1.6715e-08 4.9321 0.46861 0.20822 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.38 290.45 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.016979 5.9446e-05 3.348e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.12625 0.6281 0.20333 0.17346 INSTANT 0.445869000E+00 TIME STEP NUMBER 463 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.81093E-05 0.25508E-02 Friction velocity uk : 0.81130E-05 0.25507E-02 Dimensionless distance yplus : 0.54024E-04 0.16970E-01 Friction thermal sca. tstar : -0.10699E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.37943E-04 0.11919E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.81093E-05 0.25508E-02 Friction velocity uk : 0.81130E-05 0.25507E-02 Dimensionless distance yplus : 0.54024E-04 0.16970E-01 Friction thermal sca. tstar : -0.10699E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.37943E-04 0.11919E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34319E-08 3 0.25237E-06 0.43978E-12 0.13067E+01 c Velocity[X] 0.28434E-31 c Velocity[Y] 0.21988E-12 c Velocity[Z] 0.21990E-12 c Pressure 0.16028E-13 20 0.57304E-08 0.12542E-06 0.17540E+01 c k 0.53755E-06 2 0.69677E-07 0.10599E-07 0.20935E+01 c omega 0.13153E+02 1 0.30937E-08 0.11001E+01 0.54603E-02 c TempK 0.94517E+02 1 0.18175E-06 0.42864E-01 0.22973E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.1947e-13 9.8947e-14 -1.2194e-17 -3.1195e-18 v Velocity[Y] -0.00014253 0.00013858 -1.0881e-09 -4.0373e-12 v Velocity[Z] -0.00013857 0.00014253 9.182e-10 -1.9831e-12 v ǁVelocityǁ 4.7074e-10 0.00015392 1.0345e-05 6.1011e-06 v Pressure -0.00078221 0.017368 0.00092053 -2.0591e-20 v k 2.8462e-09 0.0017495 0.0012233 0.0015215 v omega 20.897 1.0313e+05 2670.6 505.09 v TempK 288 341.82 293.17 290.31 v Density 1.205 1.205 1.205 1.205 v TurbVisc 3.3438e-14 9.8835e-05 6.4364e-05 8.2702e-05 v CourantNb 1.8483e-09 0.00024295 1.4402e-05 7.6567e-06 v FourierNb 0.12616 0.6281 0.20324 0.17339 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9307 4.9307 0.00046222 -4.3149e-07 v volume_forces[Z] -4.9307 4.9307 -0.00046207 5.2134e-07 v ǁvolume_forcesǁ 1.6866e-08 4.9322 0.46892 0.20845 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.38 290.46 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.01697 5.942e-05 3.3465e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.12616 0.6281 0.20326 0.1734 INSTANT 0.446832000E+00 TIME STEP NUMBER 464 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.81491E-05 0.25494E-02 Friction velocity uk : 0.81527E-05 0.25494E-02 Dimensionless distance yplus : 0.54288E-04 0.16961E-01 Friction thermal sca. tstar : -0.10784E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.38129E-04 0.11912E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.81491E-05 0.25494E-02 Friction velocity uk : 0.81527E-05 0.25494E-02 Dimensionless distance yplus : 0.54288E-04 0.16961E-01 Friction thermal sca. tstar : -0.10784E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.38129E-04 0.11912E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34314E-08 3 0.25161E-06 0.43802E-12 0.13046E+01 c Velocity[X] 0.28244E-31 c Velocity[Y] 0.21900E-12 c Velocity[Z] 0.21901E-12 c Pressure 0.15983E-13 20 0.57171E-08 0.12507E-06 0.17501E+01 c k 0.53650E-06 2 0.69473E-07 0.10522E-07 0.20901E+01 c omega 0.13153E+02 1 0.30814E-08 0.10927E+01 0.54421E-02 c TempK 0.94517E+02 1 0.18120E-06 0.42727E-01 0.22936E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.1934e-13 9.8851e-14 -1.2182e-17 -3.1167e-18 v Velocity[Y] -0.00014243 0.00013847 -1.0878e-09 -4.0272e-12 v Velocity[Z] -0.00013846 0.00014243 9.1741e-10 -1.9855e-12 v ǁVelocityǁ 4.7493e-10 0.0001538 1.0344e-05 6.105e-06 v Pressure -0.00078391 0.017387 0.00092184 -1.2747e-21 v k 2.8306e-09 0.0017459 0.0012207 0.0015184 v omega 20.863 1.0313e+05 2670.6 505.06 v TempK 288 341.82 293.17 290.31 v Density 1.205 1.205 1.205 1.205 v TurbVisc 3.3255e-14 9.8818e-05 6.4333e-05 8.2669e-05 v CourantNb 1.8523e-09 0.00024272 1.4396e-05 7.6572e-06 v FourierNb 0.12607 0.6281 0.20317 0.17333 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9308 4.9308 0.00046254 -4.3202e-07 v volume_forces[Z] -4.9308 4.9308 -0.00046239 5.2194e-07 v ǁvolume_forcesǁ 1.7017e-08 4.9323 0.46924 0.20868 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.39 290.46 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.016961 5.9395e-05 3.3449e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.12608 0.6281 0.20318 0.17333 INSTANT 0.447795000E+00 TIME STEP NUMBER 465 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.81889E-05 0.25481E-02 Friction velocity uk : 0.81924E-05 0.25480E-02 Dimensionless distance yplus : 0.54552E-04 0.16952E-01 Friction thermal sca. tstar : -0.10871E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.38314E-04 0.11906E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.81889E-05 0.25481E-02 Friction velocity uk : 0.81924E-05 0.25480E-02 Dimensionless distance yplus : 0.54552E-04 0.16952E-01 Friction thermal sca. tstar : -0.10871E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.38314E-04 0.11906E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34310E-08 3 0.25084E-06 0.43628E-12 0.13025E+01 c Velocity[X] 0.28055E-31 c Velocity[Y] 0.21813E-12 c Velocity[Z] 0.21815E-12 c Pressure 0.15919E-13 20 0.57075E-08 0.12457E-06 0.17462E+01 c k 0.53545E-06 2 0.69270E-07 0.10446E-07 0.20866E+01 c omega 0.13153E+02 1 0.30692E-08 0.10854E+01 0.54239E-02 c TempK 0.94518E+02 1 0.18066E-06 0.42592E-01 0.22899E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.1922e-13 9.8755e-14 -1.2171e-17 -3.1139e-18 v Velocity[Y] -0.00014233 0.00013836 -1.0875e-09 -4.0171e-12 v Velocity[Z] -0.00013835 0.00014233 9.166e-10 -1.9879e-12 v ǁVelocityǁ 4.7914e-10 0.00015368 1.0344e-05 6.109e-06 v Pressure -0.00078561 0.017405 0.00092315 1.033e-19 v k 2.8152e-09 0.0017424 0.0012181 0.0015153 v omega 20.829 1.0313e+05 2670.6 505.02 v TempK 288 341.82 293.17 290.32 v Density 1.205 1.205 1.205 1.205 v TurbVisc 3.3074e-14 9.8802e-05 6.4302e-05 8.2635e-05 v CourantNb 1.8563e-09 0.0002425 1.439e-05 7.6578e-06 v FourierNb 0.12599 0.6281 0.2031 0.17326 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9309 4.931 0.00046285 -4.3254e-07 v volume_forces[Z] -4.9309 4.931 -0.0004627 5.2254e-07 v ǁvolume_forcesǁ 1.7169e-08 4.9324 0.46955 0.2089 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.39 290.46 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.016952 5.9369e-05 3.3434e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.12599 0.6281 0.20311 0.17327 INSTANT 0.448758000E+00 TIME STEP NUMBER 466 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.82285E-05 0.25468E-02 Friction velocity uk : 0.82320E-05 0.25467E-02 Dimensionless distance yplus : 0.54816E-04 0.16944E-01 Friction thermal sca. tstar : -0.10961E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.38499E-04 0.11900E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.82285E-05 0.25468E-02 Friction velocity uk : 0.82320E-05 0.25467E-02 Dimensionless distance yplus : 0.54816E-04 0.16944E-01 Friction thermal sca. tstar : -0.10961E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.38499E-04 0.11900E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34305E-08 3 0.25013E-06 0.43457E-12 0.13004E+01 c Velocity[X] 0.27869E-31 c Velocity[Y] 0.21728E-12 c Velocity[Z] 0.21729E-12 c Pressure 0.15936E-13 20 0.57090E-08 0.12470E-06 0.17423E+01 c k 0.53440E-06 2 0.69069E-07 0.10371E-07 0.20831E+01 c omega 0.13153E+02 1 0.30570E-08 0.10782E+01 0.54058E-02 c TempK 0.94519E+02 1 0.18012E-06 0.42457E-01 0.22863E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.191e-13 9.8659e-14 -1.2159e-17 -3.1111e-18 v Velocity[Y] -0.00014223 0.00013825 -1.0871e-09 -4.0071e-12 v Velocity[Z] -0.00013825 0.00014223 9.1579e-10 -1.9903e-12 v ǁVelocityǁ 4.8336e-10 0.00015356 1.0343e-05 6.113e-06 v Pressure -0.00078731 0.017424 0.00092445 -9.3935e-20 v k 2.7998e-09 0.0017388 0.0012156 0.0015122 v omega 20.794 1.0313e+05 2670.6 504.99 v TempK 288 341.82 293.18 290.32 v Density 1.205 1.205 1.205 1.205 v TurbVisc 3.2893e-14 9.8786e-05 6.4271e-05 8.2602e-05 v CourantNb 1.8603e-09 0.00024227 1.4384e-05 7.6583e-06 v FourierNb 0.1259 0.6281 0.20302 0.1732 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.931 4.9311 0.00046316 -4.3307e-07 v volume_forces[Z] -4.931 4.9311 -0.00046301 5.2313e-07 v ǁvolume_forcesǁ 1.7321e-08 4.9325 0.46986 0.20913 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.39 290.46 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.016944 5.9344e-05 3.3418e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.1259 0.6281 0.20304 0.1732 INSTANT 0.449721000E+00 TIME STEP NUMBER 467 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.82680E-05 0.25455E-02 Friction velocity uk : 0.82714E-05 0.25454E-02 Dimensionless distance yplus : 0.55079E-04 0.16935E-01 Friction thermal sca. tstar : -0.11052E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.38684E-04 0.11894E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.82680E-05 0.25455E-02 Friction velocity uk : 0.82714E-05 0.25454E-02 Dimensionless distance yplus : 0.55079E-04 0.16935E-01 Friction thermal sca. tstar : -0.11052E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.38684E-04 0.11894E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34301E-08 3 0.24934E-06 0.43287E-12 0.12983E+01 c Velocity[X] 0.27685E-31 c Velocity[Y] 0.21643E-12 c Velocity[Z] 0.21644E-12 c Pressure 0.15820E-13 20 0.56831E-08 0.12379E-06 0.17384E+01 c k 0.53336E-06 2 0.68868E-07 0.10296E-07 0.20797E+01 c omega 0.13153E+02 1 0.30449E-08 0.10710E+01 0.53877E-02 c TempK 0.94519E+02 1 0.17958E-06 0.42322E-01 0.22826E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.1898e-13 9.8564e-14 -1.2148e-17 -3.1083e-18 v Velocity[Y] -0.00014213 0.00013815 -1.0868e-09 -3.997e-12 v Velocity[Z] -0.00013814 0.00014213 9.1497e-10 -1.9928e-12 v ǁVelocityǁ 4.8759e-10 0.00015344 1.0343e-05 6.117e-06 v Pressure -0.00078901 0.017443 0.00092576 2.4317e-20 v k 2.7846e-09 0.0017353 0.001213 0.0015092 v omega 20.76 1.0313e+05 2670.5 504.96 v TempK 288 341.82 293.18 290.32 v Density 1.205 1.205 1.205 1.205 v TurbVisc 3.2714e-14 9.877e-05 6.424e-05 8.2569e-05 v CourantNb 1.8643e-09 0.00024205 1.4379e-05 7.6589e-06 v FourierNb 0.12581 0.6281 0.20295 0.17313 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9311 4.9312 0.00046347 -4.336e-07 v volume_forces[Z] -4.9311 4.9312 -0.00046333 5.2373e-07 v ǁvolume_forcesǁ 1.7473e-08 4.9326 0.47017 0.20936 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.4 290.47 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.016935 5.9318e-05 3.3403e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.12582 0.6281 0.20296 0.17314 INSTANT 0.450684000E+00 TIME STEP NUMBER 468 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.83074E-05 0.25442E-02 Friction velocity uk : 0.83108E-05 0.25441E-02 Dimensionless distance yplus : 0.55341E-04 0.16926E-01 Friction thermal sca. tstar : -0.11147E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.38868E-04 0.11888E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.83074E-05 0.25442E-02 Friction velocity uk : 0.83108E-05 0.25441E-02 Dimensionless distance yplus : 0.55341E-04 0.16926E-01 Friction thermal sca. tstar : -0.11147E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.38868E-04 0.11888E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34297E-08 3 0.24859E-06 0.43120E-12 0.12963E+01 c Velocity[X] 0.27503E-31 c Velocity[Y] 0.21559E-12 c Velocity[Z] 0.21561E-12 c Pressure 0.15771E-13 20 0.56714E-08 0.12339E-06 0.17345E+01 c k 0.53232E-06 2 0.68668E-07 0.10222E-07 0.20763E+01 c omega 0.13153E+02 1 0.30329E-08 0.10639E+01 0.53698E-02 c TempK 0.94520E+02 1 0.17905E-06 0.42189E-01 0.22790E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.1886e-13 9.8469e-14 -1.2136e-17 -3.1055e-18 v Velocity[Y] -0.00014203 0.00013804 -1.0864e-09 -3.9871e-12 v Velocity[Z] -0.00013803 0.00014204 9.1414e-10 -1.9952e-12 v ǁVelocityǁ 4.9183e-10 0.00015332 1.0343e-05 6.1211e-06 v Pressure -0.00079071 0.017462 0.00092706 1.912e-20 v k 2.7695e-09 0.0017318 0.0012104 0.0015061 v omega 20.726 1.0313e+05 2670.5 504.93 v TempK 288 341.82 293.18 290.33 v Density 1.205 1.205 1.205 1.205 v TurbVisc 3.2536e-14 9.8753e-05 6.421e-05 8.2535e-05 v CourantNb 1.8683e-09 0.00024183 1.4373e-05 7.6595e-06 v FourierNb 0.12573 0.6281 0.20288 0.17307 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9312 4.9313 0.00046379 -4.3412e-07 v volume_forces[Z] -4.9312 4.9313 -0.00046364 5.2432e-07 v ǁvolume_forcesǁ 1.7626e-08 4.9327 0.47049 0.20958 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.4 290.47 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.016926 5.9293e-05 3.3388e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.12573 0.6281 0.20289 0.17307 INSTANT 0.451647000E+00 TIME STEP NUMBER 469 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.83467E-05 0.25429E-02 Friction velocity uk : 0.83501E-05 0.25428E-02 Dimensionless distance yplus : 0.55602E-04 0.16918E-01 Friction thermal sca. tstar : -0.11244E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.39051E-04 0.11882E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.83467E-05 0.25429E-02 Friction velocity uk : 0.83501E-05 0.25428E-02 Dimensionless distance yplus : 0.55602E-04 0.16918E-01 Friction thermal sca. tstar : -0.11244E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.39051E-04 0.11882E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34293E-08 3 0.24785E-06 0.42955E-12 0.12943E+01 c Velocity[X] 0.27322E-31 c Velocity[Y] 0.21477E-12 c Velocity[Z] 0.21478E-12 c Pressure 0.15721E-13 20 0.56594E-08 0.12300E-06 0.17307E+01 c k 0.53129E-06 2 0.68470E-07 0.10148E-07 0.20729E+01 c omega 0.13153E+02 1 0.30209E-08 0.10568E+01 0.53520E-02 c TempK 0.94521E+02 1 0.17852E-06 0.42056E-01 0.22754E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.1874e-13 9.8374e-14 -1.2125e-17 -3.1028e-18 v Velocity[Y] -0.00014194 0.00013793 -1.0861e-09 -3.9771e-12 v Velocity[Z] -0.00013793 0.00014194 9.133e-10 -1.9976e-12 v ǁVelocityǁ 4.9609e-10 0.00015321 1.0342e-05 6.1251e-06 v Pressure -0.00079241 0.01748 0.00092836 2.0689e-20 v k 2.7545e-09 0.0017283 0.0012078 0.0015031 v omega 20.692 1.0313e+05 2670.5 504.9 v TempK 288 341.82 293.19 290.33 v Density 1.205 1.205 1.205 1.205 v TurbVisc 3.236e-14 9.8737e-05 6.4179e-05 8.2502e-05 v CourantNb 1.8723e-09 0.00024161 1.4367e-05 7.6602e-06 v FourierNb 0.12564 0.6281 0.20281 0.173 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9314 4.9314 0.0004641 -4.3464e-07 v volume_forces[Z] -4.9314 4.9314 -0.00046395 5.2491e-07 v ǁvolume_forcesǁ 1.778e-08 4.9328 0.4708 0.20981 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.4 290.47 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.016918 5.9267e-05 3.3372e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.12564 0.6281 0.20282 0.17301 INSTANT 0.452610000E+00 TIME STEP NUMBER 470 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.83859E-05 0.25416E-02 Friction velocity uk : 0.83892E-05 0.25415E-02 Dimensionless distance yplus : 0.55863E-04 0.16909E-01 Friction thermal sca. tstar : -0.11344E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.39235E-04 0.11876E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.83859E-05 0.25416E-02 Friction velocity uk : 0.83892E-05 0.25415E-02 Dimensionless distance yplus : 0.55863E-04 0.16909E-01 Friction thermal sca. tstar : -0.11344E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.39235E-04 0.11876E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34289E-08 3 0.24711E-06 0.42792E-12 0.12923E+01 c Velocity[X] 0.27144E-31 c Velocity[Y] 0.21396E-12 c Velocity[Z] 0.21397E-12 c Pressure 0.15674E-13 20 0.56470E-08 0.12263E-06 0.17268E+01 c k 0.53026E-06 2 0.68272E-07 0.10075E-07 0.20695E+01 c omega 0.13153E+02 1 0.30090E-08 0.10499E+01 0.53342E-02 c TempK 0.94521E+02 1 0.17799E-06 0.41923E-01 0.22718E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.1862e-13 9.828e-14 -1.2113e-17 -3.1e-18 v Velocity[Y] -0.00014184 0.00013783 -1.0857e-09 -3.9672e-12 v Velocity[Z] -0.00013782 0.00014184 9.1246e-10 -2e-12 v ǁVelocityǁ 5.0035e-10 0.00015309 1.0342e-05 6.1292e-06 v Pressure -0.00079411 0.017499 0.00092966 4.0202e-20 v k 2.7397e-09 0.0017248 0.0012053 0.0015001 v omega 20.659 1.0313e+05 2670.5 504.87 v TempK 288 341.82 293.19 290.33 v Density 1.205 1.205 1.205 1.205 v TurbVisc 3.2185e-14 9.8721e-05 6.4149e-05 8.2469e-05 v CourantNb 1.8763e-09 0.00024139 1.4362e-05 7.6609e-06 v FourierNb 0.12555 0.6281 0.20273 0.17294 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9315 4.9315 0.00046441 -4.3516e-07 v volume_forces[Z] -4.9315 4.9315 -0.00046426 5.255e-07 v ǁvolume_forcesǁ 1.7934e-08 4.9329 0.47111 0.21003 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.41 290.47 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.016909 5.9242e-05 3.3357e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.12556 0.6281 0.20275 0.17295 INSTANT 0.453573000E+00 TIME STEP NUMBER 471 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.84250E-05 0.25403E-02 Friction velocity uk : 0.84283E-05 0.25402E-02 Dimensionless distance yplus : 0.56123E-04 0.16900E-01 Friction thermal sca. tstar : -0.11446E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.39417E-04 0.11870E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.84250E-05 0.25403E-02 Friction velocity uk : 0.84283E-05 0.25402E-02 Dimensionless distance yplus : 0.56123E-04 0.16900E-01 Friction thermal sca. tstar : -0.11446E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.39417E-04 0.11870E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34285E-08 3 0.24636E-06 0.42632E-12 0.12903E+01 c Velocity[X] 0.26968E-31 c Velocity[Y] 0.21315E-12 c Velocity[Z] 0.21316E-12 c Pressure 0.15618E-13 20 0.56362E-08 0.12219E-06 0.17230E+01 c k 0.52923E-06 2 0.68076E-07 0.10003E-07 0.20661E+01 c omega 0.13153E+02 1 0.29972E-08 0.10429E+01 0.53166E-02 c TempK 0.94522E+02 1 0.17746E-06 0.41792E-01 0.22682E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.185e-13 9.8186e-14 -1.2102e-17 -3.0973e-18 v Velocity[Y] -0.00014174 0.00013772 -1.0853e-09 -3.9573e-12 v Velocity[Z] -0.00013772 0.00014174 9.116e-10 -2.0023e-12 v ǁVelocityǁ 5.0463e-10 0.00015297 1.0342e-05 6.1333e-06 v Pressure -0.00079581 0.017518 0.00093096 -4.6477e-20 v k 2.7249e-09 0.0017213 0.0012028 0.0014971 v omega 20.625 1.0313e+05 2670.4 504.84 v TempK 288 341.83 293.19 290.33 v Density 1.205 1.205 1.205 1.205 v TurbVisc 3.2011e-14 9.8705e-05 6.4118e-05 8.2436e-05 v CourantNb 1.8803e-09 0.00024117 1.4356e-05 7.6616e-06 v FourierNb 0.12546 0.6281 0.20266 0.17287 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9316 4.9316 0.00046472 -4.3568e-07 v volume_forces[Z] -4.9316 4.9316 -0.00046457 5.2609e-07 v ǁvolume_forcesǁ 1.8088e-08 4.933 0.47142 0.21026 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.41 290.48 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.0169 5.9217e-05 3.3342e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.12547 0.6281 0.20268 0.17288 INSTANT 0.454536000E+00 TIME STEP NUMBER 472 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.84641E-05 0.25390E-02 Friction velocity uk : 0.84673E-05 0.25389E-02 Dimensionless distance yplus : 0.56383E-04 0.16892E-01 Friction thermal sca. tstar : -0.11552E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.39600E-04 0.11864E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.84641E-05 0.25390E-02 Friction velocity uk : 0.84673E-05 0.25389E-02 Dimensionless distance yplus : 0.56383E-04 0.16892E-01 Friction thermal sca. tstar : -0.11552E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.39600E-04 0.11864E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34281E-08 3 0.24564E-06 0.42473E-12 0.12883E+01 c Velocity[X] 0.26794E-31 c Velocity[Y] 0.21236E-12 c Velocity[Z] 0.21237E-12 c Pressure 0.15581E-13 20 0.56227E-08 0.12190E-06 0.17192E+01 c k 0.52821E-06 2 0.67881E-07 0.99313E-08 0.20627E+01 c omega 0.13153E+02 1 0.29854E-08 0.10360E+01 0.52990E-02 c TempK 0.94523E+02 1 0.17694E-06 0.41661E-01 0.22646E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.1838e-13 9.8092e-14 -1.209e-17 -3.0945e-18 v Velocity[Y] -0.00014164 0.00013762 -1.085e-09 -3.9474e-12 v Velocity[Z] -0.00013761 0.00014165 9.1074e-10 -2.0046e-12 v ǁVelocityǁ 5.0892e-10 0.00015286 1.0342e-05 6.1375e-06 v Pressure -0.00079751 0.017536 0.00093226 9.8396e-20 v k 2.7102e-09 0.0017179 0.0012002 0.0014941 v omega 20.591 1.0313e+05 2670.4 504.81 v TempK 288 341.83 293.2 290.34 v Density 1.205 1.205 1.205 1.205 v TurbVisc 3.1838e-14 9.8689e-05 6.4088e-05 8.2403e-05 v CourantNb 1.8843e-09 0.00024095 1.435e-05 7.6623e-06 v FourierNb 0.12536 0.6281 0.20259 0.17281 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9317 4.9317 0.00046503 -4.362e-07 v volume_forces[Z] -4.9317 4.9317 -0.00046488 5.2667e-07 v ǁvolume_forcesǁ 1.8242e-08 4.9331 0.47173 0.21048 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.41 290.48 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.016892 5.9192e-05 3.3327e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.12536 0.6281 0.20261 0.17282 INSTANT 0.455499000E+00 TIME STEP NUMBER 473 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.85030E-05 0.25377E-02 Friction velocity uk : 0.85062E-05 0.25376E-02 Dimensionless distance yplus : 0.56642E-04 0.16883E-01 Friction thermal sca. tstar : -0.11661E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.39782E-04 0.11858E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.85030E-05 0.25377E-02 Friction velocity uk : 0.85062E-05 0.25376E-02 Dimensionless distance yplus : 0.56642E-04 0.16883E-01 Friction thermal sca. tstar : -0.11661E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.39782E-04 0.11858E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34278E-08 3 0.24490E-06 0.42316E-12 0.12864E+01 c Velocity[X] 0.26621E-31 c Velocity[Y] 0.21158E-12 c Velocity[Z] 0.21159E-12 c Pressure 0.15525E-13 20 0.56136E-08 0.12145E-06 0.17154E+01 c k 0.52719E-06 2 0.67686E-07 0.98604E-08 0.20593E+01 c omega 0.13153E+02 1 0.29737E-08 0.10292E+01 0.52815E-02 c TempK 0.94523E+02 1 0.17642E-06 0.41531E-01 0.22611E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.1826e-13 9.7999e-14 -1.2079e-17 -3.0918e-18 v Velocity[Y] -0.00014155 0.00013751 -1.0846e-09 -3.9377e-12 v Velocity[Z] -0.00013751 0.00014155 9.0987e-10 -2.007e-12 v ǁVelocityǁ 5.1322e-10 0.00015274 1.0341e-05 6.1416e-06 v Pressure -0.00079921 0.017555 0.00093355 5.6871e-20 v k 2.6957e-09 0.0017144 0.0011977 0.0014911 v omega 20.558 1.0313e+05 2670.4 504.78 v TempK 288 341.83 293.2 290.34 v Density 1.205 1.205 1.205 1.205 v TurbVisc 3.1667e-14 9.8673e-05 6.4057e-05 8.237e-05 v CourantNb 1.8883e-09 0.00024073 1.4345e-05 7.6631e-06 v FourierNb 0.12526 0.6281 0.20252 0.17275 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9318 4.9318 0.00046533 -4.3672e-07 v volume_forces[Z] -4.9318 4.9318 -0.00046519 5.2726e-07 v ǁvolume_forcesǁ 1.8398e-08 4.9332 0.47204 0.21071 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.42 290.48 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.016883 5.9167e-05 3.3312e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.12526 0.6281 0.20253 0.17275 INSTANT 0.456462000E+00 TIME STEP NUMBER 474 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.85419E-05 0.25364E-02 Friction velocity uk : 0.85450E-05 0.25364E-02 Dimensionless distance yplus : 0.56900E-04 0.16875E-01 Friction thermal sca. tstar : -0.11773E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.39963E-04 0.11852E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.85419E-05 0.25364E-02 Friction velocity uk : 0.85450E-05 0.25364E-02 Dimensionless distance yplus : 0.56900E-04 0.16875E-01 Friction thermal sca. tstar : -0.11773E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.39963E-04 0.11852E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34274E-08 3 0.24418E-06 0.42162E-12 0.12845E+01 c Velocity[X] 0.26451E-31 c Velocity[Y] 0.21080E-12 c Velocity[Z] 0.21081E-12 c Pressure 0.15480E-13 20 0.55999E-08 0.12110E-06 0.17117E+01 c k 0.52618E-06 2 0.67493E-07 0.97900E-08 0.20560E+01 c omega 0.13153E+02 1 0.29621E-08 0.10224E+01 0.52641E-02 c TempK 0.94524E+02 1 0.17590E-06 0.41401E-01 0.22575E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.1814e-13 9.7906e-14 -1.2068e-17 -3.0891e-18 v Velocity[Y] -0.00014145 0.00013741 -1.0841e-09 -3.9278e-12 v Velocity[Z] -0.0001374 0.00014146 9.0899e-10 -2.0093e-12 v ǁVelocityǁ 5.1753e-10 0.00015262 1.0341e-05 6.1458e-06 v Pressure -0.00080091 0.017574 0.00093485 -5.2752e-20 v k 2.6812e-09 0.001711 0.0011952 0.0014881 v omega 20.525 1.0313e+05 2670.4 504.75 v TempK 288 341.83 293.2 290.34 v Density 1.205 1.205 1.205 1.205 v TurbVisc 3.1497e-14 9.8657e-05 6.4027e-05 8.2337e-05 v CourantNb 1.8923e-09 0.00024052 1.434e-05 7.6639e-06 v FourierNb 0.12516 0.6281 0.20245 0.17268 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9319 4.9319 0.00046564 -4.3723e-07 v volume_forces[Z] -4.9319 4.9319 -0.0004655 5.2784e-07 v ǁvolume_forcesǁ 1.8553e-08 4.9333 0.47234 0.21093 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.42 290.48 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.016875 5.9142e-05 3.3297e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.12516 0.6281 0.20246 0.17269 INSTANT 0.457425000E+00 TIME STEP NUMBER 475 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.85806E-05 0.25352E-02 Friction velocity uk : 0.85837E-05 0.25351E-02 Dimensionless distance yplus : 0.57158E-04 0.16866E-01 Friction thermal sca. tstar : -0.11889E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.40144E-04 0.11846E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.85806E-05 0.25352E-02 Friction velocity uk : 0.85837E-05 0.25351E-02 Dimensionless distance yplus : 0.57158E-04 0.16866E-01 Friction thermal sca. tstar : -0.11889E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.40144E-04 0.11846E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34271E-08 3 0.24345E-06 0.42009E-12 0.12826E+01 c Velocity[X] 0.26282E-31 c Velocity[Y] 0.21004E-12 c Velocity[Z] 0.21005E-12 c Pressure 0.15424E-13 20 0.55901E-08 0.12065E-06 0.17079E+01 c k 0.52517E-06 2 0.67301E-07 0.97203E-08 0.20526E+01 c omega 0.13153E+02 1 0.29505E-08 0.10157E+01 0.52467E-02 c TempK 0.94524E+02 1 0.17538E-06 0.41272E-01 0.22540E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.1802e-13 9.7813e-14 -1.2056e-17 -3.0863e-18 v Velocity[Y] -0.00014136 0.00013731 -1.0837e-09 -3.9181e-12 v Velocity[Z] -0.0001373 0.00014136 9.081e-10 -2.0115e-12 v ǁVelocityǁ 5.2186e-10 0.00015251 1.0341e-05 6.15e-06 v Pressure -0.00080261 0.017592 0.00093614 9.266e-21 v k 2.6669e-09 0.0017076 0.0011927 0.0014851 v omega 20.491 1.0313e+05 2670.3 504.72 v TempK 288 341.83 293.21 290.34 v Density 1.205 1.205 1.205 1.205 v TurbVisc 3.1328e-14 9.8641e-05 6.3997e-05 8.2304e-05 v CourantNb 1.8963e-09 0.0002403 1.4334e-05 7.6647e-06 v FourierNb 0.12506 0.6281 0.20238 0.17262 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.932 4.932 0.00046595 -4.3775e-07 v volume_forces[Z] -4.932 4.932 -0.0004658 5.2842e-07 v ǁvolume_forcesǁ 1.8709e-08 4.9334 0.47265 0.21116 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.42 290.49 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.016866 5.9117e-05 3.3281e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.12506 0.6281 0.20239 0.17263 INSTANT 0.458388000E+00 TIME STEP NUMBER 476 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.86193E-05 0.25339E-02 Friction velocity uk : 0.86224E-05 0.25338E-02 Dimensionless distance yplus : 0.57415E-04 0.16858E-01 Friction thermal sca. tstar : -0.12009E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.40325E-04 0.11840E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.86193E-05 0.25339E-02 Friction velocity uk : 0.86224E-05 0.25338E-02 Dimensionless distance yplus : 0.57415E-04 0.16858E-01 Friction thermal sca. tstar : -0.12009E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.40325E-04 0.11840E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34268E-08 3 0.24273E-06 0.41858E-12 0.12807E+01 c Velocity[X] 0.26115E-31 c Velocity[Y] 0.20928E-12 c Velocity[Z] 0.20929E-12 c Pressure 0.15376E-13 20 0.55793E-08 0.12028E-06 0.17042E+01 c k 0.52416E-06 2 0.67110E-07 0.96512E-08 0.20493E+01 c omega 0.13153E+02 1 0.29390E-08 0.10090E+01 0.52295E-02 c TempK 0.94525E+02 1 0.17487E-06 0.41144E-01 0.22504E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.1791e-13 9.7721e-14 -1.2045e-17 -3.0836e-18 v Velocity[Y] -0.00014126 0.0001372 -1.0833e-09 -3.9083e-12 v Velocity[Z] -0.0001372 0.00014127 9.072e-10 -2.0138e-12 v ǁVelocityǁ 5.2619e-10 0.00015239 1.0341e-05 6.1542e-06 v Pressure -0.00080431 0.017611 0.00093743 1.5002e-20 v k 2.6526e-09 0.0017042 0.0011902 0.0014822 v omega 20.458 1.0313e+05 2670.3 504.69 v TempK 288 341.83 293.21 290.35 v Density 1.205 1.205 1.205 1.205 v TurbVisc 3.116e-14 9.8625e-05 6.3967e-05 8.2271e-05 v CourantNb 1.9003e-09 0.00024009 1.4329e-05 7.6655e-06 v FourierNb 0.12496 0.6281 0.20231 0.17255 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9321 4.9321 0.00046626 -4.3826e-07 v volume_forces[Z] -4.9321 4.9321 -0.00046611 5.2901e-07 v ǁvolume_forcesǁ 1.8865e-08 4.9335 0.47296 0.21138 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.43 290.49 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.016858 5.9092e-05 3.3266e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.12496 0.6281 0.20232 0.17256 INSTANT 0.459351000E+00 TIME STEP NUMBER 477 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.86579E-05 0.25326E-02 Friction velocity uk : 0.86609E-05 0.25325E-02 Dimensionless distance yplus : 0.57672E-04 0.16849E-01 Friction thermal sca. tstar : -0.12132E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.40505E-04 0.11834E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.86579E-05 0.25326E-02 Friction velocity uk : 0.86609E-05 0.25325E-02 Dimensionless distance yplus : 0.57672E-04 0.16849E-01 Friction thermal sca. tstar : -0.12132E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.40505E-04 0.11834E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34265E-08 3 0.24524E-06 0.41709E-12 0.12789E+01 c Velocity[X] 0.25949E-31 c Velocity[Y] 0.20854E-12 c Velocity[Z] 0.20855E-12 c Pressure 0.15346E-13 20 0.55660E-08 0.12004E-06 0.17004E+01 c k 0.52315E-06 2 0.66920E-07 0.95827E-08 0.20460E+01 c omega 0.13153E+02 1 0.29275E-08 0.10024E+01 0.52124E-02 c TempK 0.94526E+02 1 0.17436E-06 0.41017E-01 0.22469E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.1779e-13 9.7629e-14 -1.2034e-17 -3.0809e-18 v Velocity[Y] -0.00014117 0.0001371 -1.0829e-09 -3.8986e-12 v Velocity[Z] -0.00013709 0.00014117 9.0629e-10 -2.0162e-12 v ǁVelocityǁ 5.3054e-10 0.00015228 1.0341e-05 6.1585e-06 v Pressure -0.00080601 0.017629 0.00093872 -2.8729e-20 v k 2.6385e-09 0.0017008 0.0011877 0.0014792 v omega 20.425 1.0313e+05 2670.3 504.66 v TempK 288 341.83 293.21 290.35 v Density 1.205 1.205 1.205 1.205 v TurbVisc 3.0994e-14 9.8609e-05 6.3936e-05 8.2238e-05 v CourantNb 1.9043e-09 0.00023987 1.4323e-05 7.6664e-06 v FourierNb 0.12486 0.6281 0.20224 0.17249 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9322 4.9322 0.00046657 -4.3877e-07 v volume_forces[Z] -4.9322 4.9322 -0.00046642 5.2959e-07 v ǁvolume_forcesǁ 1.9022e-08 4.9336 0.47327 0.21161 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.43 290.49 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.016849 5.9067e-05 3.3251e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.12486 0.6281 0.20225 0.1725 INSTANT 0.460314000E+00 TIME STEP NUMBER 478 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.86964E-05 0.25314E-02 Friction velocity uk : 0.86994E-05 0.25313E-02 Dimensionless distance yplus : 0.57928E-04 0.16841E-01 Friction thermal sca. tstar : -0.12260E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.40685E-04 0.11828E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.86964E-05 0.25314E-02 Friction velocity uk : 0.86994E-05 0.25313E-02 Dimensionless distance yplus : 0.57928E-04 0.16841E-01 Friction thermal sca. tstar : -0.12260E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.40685E-04 0.11828E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34262E-08 3 0.24131E-06 0.41561E-12 0.12770E+01 c Velocity[X] 0.25786E-31 c Velocity[Y] 0.20780E-12 c Velocity[Z] 0.20781E-12 c Pressure 0.15284E-13 20 0.55561E-08 0.11955E-06 0.16967E+01 c k 0.52215E-06 2 0.66731E-07 0.95148E-08 0.20427E+01 c omega 0.13153E+02 1 0.29161E-08 0.99587E+00 0.51953E-02 c TempK 0.94526E+02 1 0.17385E-06 0.40890E-01 0.22434E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.1767e-13 9.7537e-14 -1.2023e-17 -3.0782e-18 v Velocity[Y] -0.00014107 0.000137 -1.0824e-09 -3.8889e-12 v Velocity[Z] -0.00013699 0.00014108 9.0538e-10 -2.0183e-12 v ǁVelocityǁ 5.349e-10 0.00015216 1.0341e-05 6.1627e-06 v Pressure -0.00080771 0.017648 0.00094001 1.0394e-19 v k 2.6244e-09 0.0016974 0.0011852 0.0014763 v omega 20.392 1.0313e+05 2670.3 504.63 v TempK 288 341.83 293.22 290.35 v Density 1.205 1.205 1.205 1.205 v TurbVisc 3.0829e-14 9.8593e-05 6.3906e-05 8.2206e-05 v CourantNb 1.9083e-09 0.00023966 1.4318e-05 7.6673e-06 v FourierNb 0.12476 0.6281 0.20217 0.17243 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9323 4.9323 0.00046687 -4.3928e-07 v volume_forces[Z] -4.9323 4.9323 -0.00046672 5.3016e-07 v ǁvolume_forcesǁ 1.9179e-08 4.9337 0.47357 0.21183 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.43 290.49 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.016841 5.9042e-05 3.3236e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.12476 0.6281 0.20218 0.17244 INSTANT 0.461277000E+00 TIME STEP NUMBER 479 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.87348E-05 0.25301E-02 Friction velocity uk : 0.87377E-05 0.25300E-02 Dimensionless distance yplus : 0.58184E-04 0.16832E-01 Friction thermal sca. tstar : -0.12392E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.40865E-04 0.11822E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.87348E-05 0.25301E-02 Friction velocity uk : 0.87377E-05 0.25300E-02 Dimensionless distance yplus : 0.58184E-04 0.16832E-01 Friction thermal sca. tstar : -0.12392E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.40865E-04 0.11822E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34259E-08 3 0.24060E-06 0.41416E-12 0.12752E+01 c Velocity[X] 0.25624E-31 c Velocity[Y] 0.20707E-12 c Velocity[Z] 0.20709E-12 c Pressure 0.15235E-13 20 0.55450E-08 0.11917E-06 0.16931E+01 c k 0.52115E-06 2 0.66542E-07 0.94475E-08 0.20394E+01 c omega 0.13153E+02 1 0.29048E-08 0.98937E+00 0.51783E-02 c TempK 0.94527E+02 1 0.17334E-06 0.40763E-01 0.22399E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.1756e-13 9.7445e-14 -1.2012e-17 -3.0755e-18 v Velocity[Y] -0.00014098 0.0001369 -1.082e-09 -3.8792e-12 v Velocity[Z] -0.00013689 0.00014098 9.0446e-10 -2.0206e-12 v ǁVelocityǁ 5.3927e-10 0.00015205 1.0341e-05 6.167e-06 v Pressure -0.00080941 0.017666 0.0009413 3.7358e-20 v k 2.6105e-09 0.001694 0.0011828 0.0014734 v omega 20.36 1.0313e+05 2670.2 504.6 v TempK 288 341.83 293.22 290.35 v Density 1.205 1.205 1.205 1.205 v TurbVisc 3.0664e-14 9.8577e-05 6.3876e-05 8.2173e-05 v CourantNb 1.9122e-09 0.00023945 1.4313e-05 7.6682e-06 v FourierNb 0.12466 0.6281 0.2021 0.17236 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9324 4.9324 0.00046718 -4.3979e-07 v volume_forces[Z] -4.9324 4.9324 -0.00046703 5.3074e-07 v ǁvolume_forcesǁ 1.9337e-08 4.9338 0.47388 0.21205 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.44 290.5 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.016832 5.9018e-05 3.3222e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.12466 0.6281 0.20211 0.17237 INSTANT 0.462240000E+00 TIME STEP NUMBER 480 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.87732E-05 0.25288E-02 Friction velocity uk : 0.87760E-05 0.25288E-02 Dimensionless distance yplus : 0.58439E-04 0.16824E-01 Friction thermal sca. tstar : -0.12529E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.41044E-04 0.11816E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.87732E-05 0.25288E-02 Friction velocity uk : 0.87760E-05 0.25288E-02 Dimensionless distance yplus : 0.58439E-04 0.16824E-01 Friction thermal sca. tstar : -0.12529E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.41044E-04 0.11816E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34256E-08 3 0.23988E-06 0.41272E-12 0.12734E+01 c Velocity[X] 0.25464E-31 c Velocity[Y] 0.20636E-12 c Velocity[Z] 0.20637E-12 c Pressure 0.15195E-13 20 0.55348E-08 0.11885E-06 0.16894E+01 c k 0.52016E-06 2 0.66355E-07 0.93808E-08 0.20361E+01 c omega 0.13153E+02 1 0.28936E-08 0.98292E+00 0.51614E-02 c TempK 0.94528E+02 1 0.17284E-06 0.40638E-01 0.22365E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.1744e-13 9.7354e-14 -1.2e-17 -3.0729e-18 v Velocity[Y] -0.00014089 0.00013679 -1.0815e-09 -3.8695e-12 v Velocity[Z] -0.00013679 0.00014089 9.0353e-10 -2.0228e-12 v ǁVelocityǁ 5.4365e-10 0.00015194 1.0341e-05 6.1713e-06 v Pressure -0.0008111 0.017685 0.00094258 -1.3629e-20 v k 2.5966e-09 0.0016906 0.0011803 0.0014705 v omega 20.327 1.0313e+05 2670.2 504.57 v TempK 288 341.84 293.23 290.36 v Density 1.205 1.205 1.205 1.205 v TurbVisc 3.0502e-14 9.8561e-05 6.3847e-05 8.214e-05 v CourantNb 1.9162e-09 0.00023923 1.4308e-05 7.6692e-06 v FourierNb 0.12456 0.6281 0.20203 0.1723 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9325 4.9325 0.00046748 -4.403e-07 v volume_forces[Z] -4.9325 4.9325 -0.00046734 5.3132e-07 v ǁvolume_forcesǁ 1.9495e-08 4.9339 0.47418 0.21228 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.44 290.5 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.016824 5.8993e-05 3.3207e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.12456 0.6281 0.20204 0.17231 INSTANT 0.463203000E+00 TIME STEP NUMBER 481 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.88114E-05 0.25276E-02 Friction velocity uk : 0.88143E-05 0.25275E-02 Dimensionless distance yplus : 0.58693E-04 0.16816E-01 Friction thermal sca. tstar : -0.12670E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.41222E-04 0.11810E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.88114E-05 0.25276E-02 Friction velocity uk : 0.88143E-05 0.25275E-02 Dimensionless distance yplus : 0.58693E-04 0.16816E-01 Friction thermal sca. tstar : -0.12670E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.41222E-04 0.11810E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34254E-08 3 0.23918E-06 0.41130E-12 0.12716E+01 c Velocity[X] 0.25305E-31 c Velocity[Y] 0.20565E-12 c Velocity[Z] 0.20566E-12 c Pressure 0.15141E-13 20 0.55230E-08 0.11843E-06 0.16857E+01 c k 0.51917E-06 2 0.66169E-07 0.93146E-08 0.20328E+01 c omega 0.13153E+02 1 0.28823E-08 0.97652E+00 0.51446E-02 c TempK 0.94528E+02 1 0.17234E-06 0.40513E-01 0.22330E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.1732e-13 9.7263e-14 -1.1989e-17 -3.0702e-18 v Velocity[Y] -0.00014079 0.00013669 -1.081e-09 -3.8599e-12 v Velocity[Z] -0.00013668 0.0001408 9.0259e-10 -2.025e-12 v ǁVelocityǁ 5.4804e-10 0.00015183 1.0341e-05 6.1756e-06 v Pressure -0.0008128 0.017703 0.00094387 -5.388e-20 v k 2.5829e-09 0.0016873 0.0011779 0.0014676 v omega 20.294 1.0313e+05 2670.2 504.54 v TempK 288 341.84 293.23 290.36 v Density 1.205 1.205 1.205 1.205 v TurbVisc 3.034e-14 9.8545e-05 6.3817e-05 8.2108e-05 v CourantNb 1.9202e-09 0.00023902 1.4303e-05 7.6701e-06 v FourierNb 0.12446 0.6281 0.20196 0.17224 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9326 4.9326 0.00046779 -4.4081e-07 v volume_forces[Z] -4.9326 4.9326 -0.00046764 5.3189e-07 v ǁvolume_forcesǁ 1.9653e-08 4.934 0.47449 0.2125 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.45 290.5 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.016816 5.8968e-05 3.3192e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.12446 0.6281 0.20197 0.17225 INSTANT 0.464166000E+00 TIME STEP NUMBER 482 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.88496E-05 0.25263E-02 Friction velocity uk : 0.88524E-05 0.25262E-02 Dimensionless distance yplus : 0.58947E-04 0.16807E-01 Friction thermal sca. tstar : -0.12817E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.41401E-04 0.11804E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.88496E-05 0.25263E-02 Friction velocity uk : 0.88524E-05 0.25262E-02 Dimensionless distance yplus : 0.58947E-04 0.16807E-01 Friction thermal sca. tstar : -0.12817E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.41401E-04 0.11804E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34251E-08 3 0.23848E-06 0.40990E-12 0.12698E+01 c Velocity[X] 0.25148E-31 c Velocity[Y] 0.20494E-12 c Velocity[Z] 0.20495E-12 c Pressure 0.15098E-13 20 0.55127E-08 0.11808E-06 0.16821E+01 c k 0.51818E-06 2 0.65984E-07 0.92490E-08 0.20295E+01 c omega 0.13153E+02 1 0.28712E-08 0.97018E+00 0.51278E-02 c TempK 0.94529E+02 1 0.17184E-06 0.40389E-01 0.22296E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.1721e-13 9.7173e-14 -1.1978e-17 -3.0675e-18 v Velocity[Y] -0.0001407 0.00013659 -1.0806e-09 -3.8503e-12 v Velocity[Z] -0.00013658 0.0001407 9.0164e-10 -2.0273e-12 v ǁVelocityǁ 5.5245e-10 0.00015171 1.0342e-05 6.18e-06 v Pressure -0.0008145 0.017722 0.00094515 3.1671e-20 v k 2.5692e-09 0.0016839 0.0011754 0.0014647 v omega 20.262 1.0313e+05 2670.2 504.51 v TempK 288 341.84 293.23 290.36 v Density 1.205 1.205 1.205 1.205 v TurbVisc 3.0179e-14 9.8529e-05 6.3787e-05 8.2075e-05 v CourantNb 1.9242e-09 0.00023881 1.4298e-05 7.6711e-06 v FourierNb 0.12436 0.6281 0.20189 0.17218 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9327 4.9328 0.00046809 -4.4132e-07 v volume_forces[Z] -4.9327 4.9328 -0.00046795 5.3246e-07 v ǁvolume_forcesǁ 1.9812e-08 4.9341 0.47479 0.21272 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.45 290.5 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.016807 5.8944e-05 3.3177e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.12436 0.6281 0.2019 0.17218 INSTANT 0.465129000E+00 TIME STEP NUMBER 483 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.88877E-05 0.25251E-02 Friction velocity uk : 0.88904E-05 0.25250E-02 Dimensionless distance yplus : 0.59201E-04 0.16799E-01 Friction thermal sca. tstar : -0.12970E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.41579E-04 0.11799E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.88877E-05 0.25251E-02 Friction velocity uk : 0.88904E-05 0.25250E-02 Dimensionless distance yplus : 0.59201E-04 0.16799E-01 Friction thermal sca. tstar : -0.12970E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.41579E-04 0.11799E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34249E-08 3 0.23778E-06 0.40851E-12 0.12681E+01 c Velocity[X] 0.24993E-31 c Velocity[Y] 0.20425E-12 c Velocity[Z] 0.20426E-12 c Pressure 0.15056E-13 20 0.54998E-08 0.11775E-06 0.16784E+01 c k 0.51719E-06 2 0.65800E-07 0.91840E-08 0.20263E+01 c omega 0.13153E+02 1 0.28601E-08 0.96388E+00 0.51112E-02 c TempK 0.94530E+02 1 0.17134E-06 0.40265E-01 0.22261E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.1709e-13 9.7082e-14 -1.1967e-17 -3.0649e-18 v Velocity[Y] -0.00014061 0.00013649 -1.0801e-09 -3.8407e-12 v Velocity[Z] -0.00013648 0.00014061 9.0068e-10 -2.0294e-12 v ǁVelocityǁ 5.5686e-10 0.0001516 1.0342e-05 6.1843e-06 v Pressure -0.0008162 0.01774 0.00094643 -1.5384e-19 v k 2.5557e-09 0.0016806 0.001173 0.0014618 v omega 20.229 1.0313e+05 2670.1 504.48 v TempK 288 341.84 293.24 290.36 v Density 1.205 1.205 1.205 1.205 v TurbVisc 3.002e-14 9.8513e-05 6.3757e-05 8.2043e-05 v CourantNb 1.9282e-09 0.0002386 1.4293e-05 7.6722e-06 v FourierNb 0.12426 0.6281 0.20182 0.17211 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9328 4.9329 0.0004684 -4.4182e-07 v volume_forces[Z] -4.9328 4.9329 -0.00046825 5.3303e-07 v ǁvolume_forcesǁ 1.9971e-08 4.9342 0.4751 0.21294 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.45 290.51 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.016799 5.8919e-05 3.3162e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.12426 0.6281 0.20183 0.17212 INSTANT 0.466092000E+00 TIME STEP NUMBER 484 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.89257E-05 0.25238E-02 Friction velocity uk : 0.89284E-05 0.25238E-02 Dimensionless distance yplus : 0.59453E-04 0.16791E-01 Friction thermal sca. tstar : -0.13128E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.41756E-04 0.11793E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.89257E-05 0.25238E-02 Friction velocity uk : 0.89284E-05 0.25238E-02 Dimensionless distance yplus : 0.59453E-04 0.16791E-01 Friction thermal sca. tstar : -0.13128E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.41756E-04 0.11793E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34247E-08 3 0.23708E-06 0.40714E-12 0.12663E+01 c Velocity[X] 0.24839E-31 c Velocity[Y] 0.20356E-12 c Velocity[Z] 0.20357E-12 c Pressure 0.15004E-13 20 0.54902E-08 0.11734E-06 0.16748E+01 c k 0.51621E-06 2 0.65616E-07 0.91196E-08 0.20230E+01 c omega 0.13153E+02 1 0.28491E-08 0.95764E+00 0.50946E-02 c TempK 0.94530E+02 1 0.17085E-06 0.40142E-01 0.22227E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.1698e-13 9.6992e-14 -1.1956e-17 -3.0622e-18 v Velocity[Y] -0.00014051 0.00013639 -1.0796e-09 -3.8312e-12 v Velocity[Z] -0.00013638 0.00014052 8.9972e-10 -2.0316e-12 v ǁVelocityǁ 5.6129e-10 0.00015149 1.0342e-05 6.1887e-06 v Pressure -0.0008179 0.017758 0.00094771 1.1134e-19 v k 2.5422e-09 0.0016772 0.0011706 0.0014589 v omega 20.197 1.0313e+05 2670.1 504.45 v TempK 288 341.84 293.24 290.37 v Density 1.205 1.205 1.205 1.205 v TurbVisc 2.9862e-14 9.8497e-05 6.3727e-05 8.201e-05 v CourantNb 1.9321e-09 0.0002384 1.4288e-05 7.6732e-06 v FourierNb 0.12416 0.6281 0.20175 0.17205 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9329 4.933 0.0004687 -4.4233e-07 v volume_forces[Z] -4.9329 4.933 -0.00046855 5.336e-07 v ǁvolume_forcesǁ 2.0131e-08 4.9343 0.4754 0.21317 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.46 290.51 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.016791 5.8895e-05 3.3147e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.12416 0.6281 0.20176 0.17206 INSTANT 0.467055000E+00 TIME STEP NUMBER 485 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.89636E-05 0.25226E-02 Friction velocity uk : 0.89663E-05 0.25225E-02 Dimensionless distance yplus : 0.59706E-04 0.16782E-01 Friction thermal sca. tstar : -0.13292E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.41934E-04 0.11787E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.89636E-05 0.25226E-02 Friction velocity uk : 0.89663E-05 0.25225E-02 Dimensionless distance yplus : 0.59706E-04 0.16782E-01 Friction thermal sca. tstar : -0.13292E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.41934E-04 0.11787E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34245E-08 3 0.23639E-06 0.40578E-12 0.12646E+01 c Velocity[X] 0.24687E-31 c Velocity[Y] 0.20289E-12 c Velocity[Z] 0.20290E-12 c Pressure 0.14960E-13 20 0.54796E-08 0.11699E-06 0.16712E+01 c k 0.51524E-06 2 0.65434E-07 0.90557E-08 0.20198E+01 c omega 0.13153E+02 1 0.28381E-08 0.95144E+00 0.50781E-02 c TempK 0.94531E+02 1 0.17036E-06 0.40019E-01 0.22193E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.1687e-13 9.6903e-14 -1.1945e-17 -3.0596e-18 v Velocity[Y] -0.00014042 0.00013629 -1.0791e-09 -3.8217e-12 v Velocity[Z] -0.00013628 0.00014042 8.9875e-10 -2.0338e-12 v ǁVelocityǁ 5.6572e-10 0.00015138 1.0342e-05 6.1931e-06 v Pressure -0.0008196 0.017777 0.00094899 2.7651e-20 v k 2.5289e-09 0.0016739 0.0011682 0.0014561 v omega 20.165 1.0313e+05 2670.1 504.42 v TempK 288 341.84 293.24 290.37 v Density 1.205 1.205 1.205 1.205 v TurbVisc 2.9704e-14 9.8482e-05 6.3698e-05 8.1978e-05 v CourantNb 1.9361e-09 0.00023819 1.4283e-05 7.6743e-06 v FourierNb 0.12406 0.6281 0.20168 0.17199 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.933 4.9331 0.000469 -4.4283e-07 v volume_forces[Z] -4.933 4.9331 -0.00046886 5.3417e-07 v ǁvolume_forcesǁ 2.0291e-08 4.9344 0.4757 0.21339 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.46 290.51 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.016782 5.887e-05 3.3133e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.12406 0.6281 0.20169 0.172 INSTANT 0.468018000E+00 TIME STEP NUMBER 486 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.90015E-05 0.25214E-02 Friction velocity uk : 0.90041E-05 0.25213E-02 Dimensionless distance yplus : 0.59958E-04 0.16774E-01 Friction thermal sca. tstar : -0.13464E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.42110E-04 0.11781E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.90015E-05 0.25214E-02 Friction velocity uk : 0.90041E-05 0.25213E-02 Dimensionless distance yplus : 0.59958E-04 0.16774E-01 Friction thermal sca. tstar : -0.13464E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.42110E-04 0.11781E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34243E-08 3 0.23570E-06 0.40444E-12 0.12629E+01 c Velocity[X] 0.24536E-31 c Velocity[Y] 0.20222E-12 c Velocity[Z] 0.20223E-12 c Pressure 0.14915E-13 20 0.54685E-08 0.11664E-06 0.16676E+01 c k 0.51426E-06 2 0.65253E-07 0.89924E-08 0.20166E+01 c omega 0.13153E+02 1 0.28272E-08 0.94530E+00 0.50616E-02 c TempK 0.94531E+02 1 0.16987E-06 0.39897E-01 0.22159E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.1675e-13 9.6813e-14 -1.1934e-17 -3.0569e-18 v Velocity[Y] -0.00014033 0.00013619 -1.0786e-09 -3.8122e-12 v Velocity[Z] -0.00013618 0.00014033 8.9777e-10 -2.0359e-12 v ǁVelocityǁ 5.7017e-10 0.00015127 1.0342e-05 6.1975e-06 v Pressure -0.0008213 0.017795 0.00095027 -6.0302e-21 v k 2.5156e-09 0.0016706 0.0011658 0.0014532 v omega 20.133 1.0313e+05 2670.1 504.4 v TempK 288 341.84 293.25 290.37 v Density 1.205 1.205 1.205 1.205 v TurbVisc 2.9548e-14 9.8466e-05 6.3668e-05 8.1946e-05 v CourantNb 1.9401e-09 0.00023798 1.4278e-05 7.6754e-06 v FourierNb 0.12396 0.6281 0.20161 0.17193 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9331 4.9332 0.00046931 -4.4333e-07 v volume_forces[Z] -4.9331 4.9332 -0.00046916 5.3474e-07 v ǁvolume_forcesǁ 2.0451e-08 4.9345 0.47601 0.21361 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.46 290.51 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.016774 5.8846e-05 3.3118e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.12396 0.6281 0.20163 0.17193 INSTANT 0.468981000E+00 TIME STEP NUMBER 487 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.90393E-05 0.25201E-02 Friction velocity uk : 0.90419E-05 0.25200E-02 Dimensionless distance yplus : 0.60209E-04 0.16766E-01 Friction thermal sca. tstar : -0.13642E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.42287E-04 0.11775E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.90393E-05 0.25201E-02 Friction velocity uk : 0.90419E-05 0.25200E-02 Dimensionless distance yplus : 0.60209E-04 0.16766E-01 Friction thermal sca. tstar : -0.13642E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.42287E-04 0.11775E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34241E-08 3 0.23502E-06 0.40312E-12 0.12612E+01 c Velocity[X] 0.24387E-31 c Velocity[Y] 0.20155E-12 c Velocity[Z] 0.20156E-12 c Pressure 0.14871E-13 20 0.54576E-08 0.11629E-06 0.16641E+01 c k 0.51329E-06 2 0.65072E-07 0.89296E-08 0.20134E+01 c omega 0.13153E+02 1 0.28164E-08 0.93920E+00 0.50453E-02 c TempK 0.94532E+02 1 0.16938E-06 0.39776E-01 0.22125E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.1664e-13 9.6724e-14 -1.1923e-17 -3.0543e-18 v Velocity[Y] -0.00014024 0.00013609 -1.078e-09 -3.8028e-12 v Velocity[Z] -0.00013608 0.00014024 8.9678e-10 -2.0381e-12 v ǁVelocityǁ 5.7463e-10 0.00015116 1.0343e-05 6.2019e-06 v Pressure -0.00082299 0.017813 0.00095154 -1.0129e-19 v k 2.5025e-09 0.0016673 0.0011634 0.0014504 v omega 20.101 1.0313e+05 2670.1 504.37 v TempK 288 341.84 293.25 290.37 v Density 1.205 1.205 1.205 1.205 v TurbVisc 2.9393e-14 9.845e-05 6.3639e-05 8.1914e-05 v CourantNb 1.9441e-09 0.00023778 1.4273e-05 7.6765e-06 v FourierNb 0.12386 0.6281 0.20154 0.17186 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9332 4.9333 0.00046961 -4.4383e-07 v volume_forces[Z] -4.9332 4.9333 -0.00046946 5.353e-07 v ǁvolume_forcesǁ 2.0612e-08 4.9346 0.47631 0.21383 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.47 290.52 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.016766 5.8822e-05 3.3103e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.12386 0.6281 0.20156 0.17187 INSTANT 0.469944000E+00 TIME STEP NUMBER 488 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.90770E-05 0.25189E-02 Friction velocity uk : 0.90796E-05 0.25188E-02 Dimensionless distance yplus : 0.60460E-04 0.16758E-01 Friction thermal sca. tstar : -0.13828E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.42463E-04 0.11770E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.90770E-05 0.25189E-02 Friction velocity uk : 0.90796E-05 0.25188E-02 Dimensionless distance yplus : 0.60460E-04 0.16758E-01 Friction thermal sca. tstar : -0.13828E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.42463E-04 0.11770E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34239E-08 3 0.23470E-06 0.40180E-12 0.12596E+01 c Velocity[X] 0.24240E-31 c Velocity[Y] 0.20090E-12 c Velocity[Z] 0.20091E-12 c Pressure 0.14872E-13 20 0.54426E-08 0.11630E-06 0.16605E+01 c k 0.51232E-06 2 0.64893E-07 0.88673E-08 0.20102E+01 c omega 0.13153E+02 1 0.28056E-08 0.93315E+00 0.50290E-02 c TempK 0.94533E+02 1 0.16890E-06 0.39656E-01 0.22091E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.1653e-13 9.6635e-14 -1.1913e-17 -3.0517e-18 v Velocity[Y] -0.00014015 0.00013599 -1.0775e-09 -3.7935e-12 v Velocity[Z] -0.00013598 0.00014015 8.9578e-10 -2.0403e-12 v ǁVelocityǁ 5.791e-10 0.00015105 1.0343e-05 6.2064e-06 v Pressure -0.00082469 0.017832 0.00095282 4.5104e-21 v k 2.4894e-09 0.001664 0.001161 0.0014475 v omega 20.069 1.0313e+05 2670 504.34 v TempK 288 341.84 293.25 290.38 v Density 1.205 1.205 1.205 1.205 v TurbVisc 2.9239e-14 9.8434e-05 6.3609e-05 8.1881e-05 v CourantNb 1.948e-09 0.00023757 1.4268e-05 7.6776e-06 v FourierNb 0.12376 0.6281 0.20147 0.1718 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9333 4.9334 0.00046991 -4.4433e-07 v volume_forces[Z] -4.9333 4.9334 -0.00046976 5.3587e-07 v ǁvolume_forcesǁ 2.0773e-08 4.9347 0.47661 0.21405 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.47 290.52 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.016758 5.8798e-05 3.3089e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.12377 0.6281 0.20149 0.17181 INSTANT 0.470907000E+00 TIME STEP NUMBER 489 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.91146E-05 0.25177E-02 Friction velocity uk : 0.91171E-05 0.25176E-02 Dimensionless distance yplus : 0.60710E-04 0.16750E-01 Friction thermal sca. tstar : -0.14022E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.42639E-04 0.11764E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.91146E-05 0.25177E-02 Friction velocity uk : 0.91171E-05 0.25176E-02 Dimensionless distance yplus : 0.60710E-04 0.16750E-01 Friction thermal sca. tstar : -0.14022E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.42639E-04 0.11764E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34238E-08 3 0.23365E-06 0.40051E-12 0.12579E+01 c Velocity[X] 0.24092E-31 c Velocity[Y] 0.20025E-12 c Velocity[Z] 0.20026E-12 c Pressure 0.14792E-13 20 0.54338E-08 0.11566E-06 0.16570E+01 c k 0.51136E-06 2 0.64714E-07 0.88056E-08 0.20070E+01 c omega 0.13153E+02 1 0.27949E-08 0.92715E+00 0.50128E-02 c TempK 0.94533E+02 1 0.16841E-06 0.39536E-01 0.22058E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.1641e-13 9.6546e-14 -1.1902e-17 -3.0491e-18 v Velocity[Y] -0.00014006 0.00013589 -1.077e-09 -3.784e-12 v Velocity[Z] -0.00013588 0.00014006 8.9478e-10 -2.0425e-12 v ǁVelocityǁ 5.8359e-10 0.00015094 1.0343e-05 6.2108e-06 v Pressure -0.00082639 0.01785 0.00095409 1.7551e-20 v k 2.4764e-09 0.0016608 0.0011586 0.0014447 v omega 20.037 1.0313e+05 2670 504.31 v TempK 288 341.85 293.26 290.38 v Density 1.205 1.205 1.205 1.205 v TurbVisc 2.9087e-14 9.8419e-05 6.358e-05 8.1849e-05 v CourantNb 1.952e-09 0.00023737 1.4263e-05 7.6788e-06 v FourierNb 0.12366 0.6281 0.20141 0.17174 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9334 4.9335 0.00047021 -4.4483e-07 v volume_forces[Z] -4.9334 4.9335 -0.00047006 5.3643e-07 v ǁvolume_forcesǁ 2.0935e-08 4.9348 0.47691 0.21427 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.47 290.52 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.01675 5.8773e-05 3.3074e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.12367 0.6281 0.20142 0.17175 INSTANT 0.471870000E+00 TIME STEP NUMBER 490 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.91522E-05 0.25164E-02 Friction velocity uk : 0.91547E-05 0.25164E-02 Dimensionless distance yplus : 0.60960E-04 0.16741E-01 Friction thermal sca. tstar : -0.14226E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.42814E-04 0.11758E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.91522E-05 0.25164E-02 Friction velocity uk : 0.91547E-05 0.25164E-02 Dimensionless distance yplus : 0.60960E-04 0.16741E-01 Friction thermal sca. tstar : -0.14226E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.42814E-04 0.11758E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34236E-08 3 0.24290E-06 0.39923E-12 0.12562E+01 c Velocity[X] 0.23948E-31 c Velocity[Y] 0.19961E-12 c Velocity[Z] 0.19962E-12 c Pressure 0.14746E-13 20 0.54255E-08 0.11530E-06 0.16535E+01 c k 0.51040E-06 2 0.64536E-07 0.87444E-08 0.20038E+01 c omega 0.13153E+02 1 0.27842E-08 0.92120E+00 0.49967E-02 c TempK 0.94534E+02 1 0.16793E-06 0.39416E-01 0.22024E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.163e-13 9.6458e-14 -1.1891e-17 -3.0465e-18 v Velocity[Y] -0.00013997 0.00013579 -1.0764e-09 -3.7747e-12 v Velocity[Z] -0.00013579 0.00013997 8.9376e-10 -2.0446e-12 v ǁVelocityǁ 5.8808e-10 0.00015083 1.0344e-05 6.2153e-06 v Pressure -0.00082809 0.017868 0.00095536 6.045e-20 v k 2.4635e-09 0.0016575 0.0011562 0.0014419 v omega 20.006 1.0313e+05 2670 504.28 v TempK 288 341.85 293.26 290.38 v Density 1.205 1.205 1.205 1.205 v TurbVisc 2.8935e-14 9.8403e-05 6.3551e-05 8.1817e-05 v CourantNb 1.956e-09 0.00023716 1.4258e-05 7.6799e-06 v FourierNb 0.12357 0.6281 0.20134 0.17168 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9335 4.9336 0.00047051 -4.4532e-07 v volume_forces[Z] -4.9335 4.9336 -0.00047036 5.3699e-07 v ǁvolume_forcesǁ 2.1097e-08 4.9349 0.47721 0.21449 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.48 290.52 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.016741 5.8749e-05 3.306e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.12357 0.6281 0.20135 0.17169 INSTANT 0.472833000E+00 TIME STEP NUMBER 491 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.91896E-05 0.25152E-02 Friction velocity uk : 0.91921E-05 0.25151E-02 Dimensionless distance yplus : 0.61209E-04 0.16733E-01 Friction thermal sca. tstar : -0.14438E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.42990E-04 0.11752E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.91896E-05 0.25152E-02 Friction velocity uk : 0.91921E-05 0.25151E-02 Dimensionless distance yplus : 0.61209E-04 0.16733E-01 Friction thermal sca. tstar : -0.14438E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.42990E-04 0.11752E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34235E-08 3 0.23231E-06 0.39796E-12 0.12546E+01 c Velocity[X] 0.23804E-31 c Velocity[Y] 0.19897E-12 c Velocity[Z] 0.19898E-12 c Pressure 0.14697E-13 20 0.54158E-08 0.11492E-06 0.16499E+01 c k 0.50944E-06 2 0.64359E-07 0.86837E-08 0.20006E+01 c omega 0.13153E+02 1 0.27736E-08 0.91530E+00 0.49807E-02 c TempK 0.94535E+02 1 0.16746E-06 0.39297E-01 0.21991E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.1619e-13 9.637e-14 -1.188e-17 -3.0439e-18 v Velocity[Y] -0.00013988 0.0001357 -1.0758e-09 -3.7653e-12 v Velocity[Z] -0.00013569 0.00013988 8.9274e-10 -2.0468e-12 v ǁVelocityǁ 5.9258e-10 0.00015072 1.0344e-05 6.2198e-06 v Pressure -0.00082979 0.017886 0.00095663 -3.8584e-20 v k 2.4507e-09 0.0016543 0.0011539 0.0014391 v omega 19.974 1.0313e+05 2670 504.25 v TempK 288 341.85 293.26 290.38 v Density 1.205 1.205 1.205 1.205 v TurbVisc 2.8784e-14 9.8387e-05 6.3521e-05 8.1785e-05 v CourantNb 1.9599e-09 0.00023696 1.4254e-05 7.6811e-06 v FourierNb 0.12347 0.6281 0.20127 0.17162 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9336 4.9337 0.00047081 -4.4582e-07 v volume_forces[Z] -4.9336 4.9337 -0.00047066 5.3755e-07 v ǁvolume_forcesǁ 2.1259e-08 4.935 0.47751 0.21471 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.48 290.53 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.016733 5.8725e-05 3.3045e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.12347 0.6281 0.20128 0.17163 INSTANT 0.473796000E+00 TIME STEP NUMBER 492 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.92271E-05 0.25140E-02 Friction velocity uk : 0.92295E-05 0.25139E-02 Dimensionless distance yplus : 0.61458E-04 0.16725E-01 Friction thermal sca. tstar : -0.14661E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.43164E-04 0.11747E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.92271E-05 0.25140E-02 Friction velocity uk : 0.92295E-05 0.25139E-02 Dimensionless distance yplus : 0.61458E-04 0.16725E-01 Friction thermal sca. tstar : -0.14661E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.43164E-04 0.11747E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34234E-08 3 0.23164E-06 0.39670E-12 0.12530E+01 c Velocity[X] 0.23662E-31 c Velocity[Y] 0.19835E-12 c Velocity[Z] 0.19836E-12 c Pressure 0.14651E-13 20 0.54051E-08 0.11456E-06 0.16465E+01 c k 0.50849E-06 2 0.64184E-07 0.86236E-08 0.19975E+01 c omega 0.13153E+02 1 0.27630E-08 0.90944E+00 0.49647E-02 c TempK 0.94535E+02 1 0.16698E-06 0.39179E-01 0.21957E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.1608e-13 9.6282e-14 -1.1869e-17 -3.0413e-18 v Velocity[Y] -0.00013979 0.0001356 -1.0753e-09 -3.756e-12 v Velocity[Z] -0.00013559 0.00013979 8.9171e-10 -2.0489e-12 v ǁVelocityǁ 5.971e-10 0.00015061 1.0345e-05 6.2243e-06 v Pressure -0.00083149 0.017905 0.0009579 -4.3584e-20 v k 2.438e-09 0.001651 0.0011515 0.0014363 v omega 19.943 1.0313e+05 2669.9 504.22 v TempK 288 341.85 293.27 290.39 v Density 1.205 1.205 1.205 1.205 v TurbVisc 2.8635e-14 9.8372e-05 6.3492e-05 8.1753e-05 v CourantNb 1.9639e-09 0.00023676 1.4249e-05 7.6824e-06 v FourierNb 0.12337 0.6281 0.2012 0.17156 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9337 4.9338 0.00047111 -4.4631e-07 v volume_forces[Z] -4.9337 4.9338 -0.00047096 5.3811e-07 v ǁvolume_forcesǁ 2.1422e-08 4.9351 0.47781 0.21493 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.48 290.53 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.016725 5.8701e-05 3.303e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.12337 0.6281 0.20122 0.17156 INSTANT 0.474759000E+00 TIME STEP NUMBER 493 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.92644E-05 0.25128E-02 Friction velocity uk : 0.92668E-05 0.25127E-02 Dimensionless distance yplus : 0.61707E-04 0.16717E-01 Friction thermal sca. tstar : -0.14895E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.43339E-04 0.11741E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.92644E-05 0.25128E-02 Friction velocity uk : 0.92668E-05 0.25127E-02 Dimensionless distance yplus : 0.61707E-04 0.16717E-01 Friction thermal sca. tstar : -0.14895E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.43339E-04 0.11741E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34233E-08 3 0.23098E-06 0.39546E-12 0.12514E+01 c Velocity[X] 0.23522E-31 c Velocity[Y] 0.19773E-12 c Velocity[Z] 0.19774E-12 c Pressure 0.14637E-13 20 0.53915E-08 0.11444E-06 0.16430E+01 c k 0.50754E-06 2 0.64009E-07 0.85639E-08 0.19943E+01 c omega 0.13153E+02 1 0.27525E-08 0.90363E+00 0.49488E-02 c TempK 0.94536E+02 1 0.16651E-06 0.39061E-01 0.21924E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.1597e-13 9.6195e-14 -1.1859e-17 -3.0387e-18 v Velocity[Y] -0.0001397 0.0001355 -1.0747e-09 -3.7467e-12 v Velocity[Z] -0.00013549 0.0001397 8.9068e-10 -2.051e-12 v ǁVelocityǁ 6.0162e-10 0.0001505 1.0345e-05 6.2289e-06 v Pressure -0.00083319 0.017923 0.00095917 1.4904e-20 v k 2.4254e-09 0.0016478 0.0011492 0.0014335 v omega 19.911 1.0313e+05 2669.9 504.2 v TempK 288 341.85 293.27 290.39 v Density 1.205 1.205 1.205 1.205 v TurbVisc 2.8486e-14 9.8356e-05 6.3463e-05 8.1721e-05 v CourantNb 1.9679e-09 0.00023655 1.4244e-05 7.6836e-06 v FourierNb 0.12327 0.6281 0.20114 0.1715 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9338 4.9339 0.00047141 -4.4681e-07 v volume_forces[Z] -4.9338 4.9339 -0.00047126 5.3867e-07 v ǁvolume_forcesǁ 2.1585e-08 4.9352 0.47811 0.21515 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.49 290.53 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.016717 5.8677e-05 3.3016e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.12327 0.6281 0.20115 0.1715 INSTANT 0.475722000E+00 TIME STEP NUMBER 494 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.93017E-05 0.25116E-02 Friction velocity uk : 0.93041E-05 0.25115E-02 Dimensionless distance yplus : 0.61955E-04 0.16709E-01 Friction thermal sca. tstar : -0.15142E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.43513E-04 0.11735E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.93017E-05 0.25116E-02 Friction velocity uk : 0.93041E-05 0.25115E-02 Dimensionless distance yplus : 0.61955E-04 0.16709E-01 Friction thermal sca. tstar : -0.15142E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.43513E-04 0.11735E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34232E-08 3 0.23034E-06 0.39423E-12 0.12498E+01 c Velocity[X] 0.23382E-31 c Velocity[Y] 0.19711E-12 c Velocity[Z] 0.19712E-12 c Pressure 0.14610E-13 20 0.53875E-08 0.11423E-06 0.16395E+01 c k 0.50659E-06 2 0.63834E-07 0.85048E-08 0.19912E+01 c omega 0.13153E+02 1 0.27421E-08 0.89787E+00 0.49330E-02 c TempK 0.94537E+02 1 0.16604E-06 0.38944E-01 0.21891E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.1586e-13 9.6107e-14 -1.1848e-17 -3.0361e-18 v Velocity[Y] -0.00013961 0.0001354 -1.0741e-09 -3.7377e-12 v Velocity[Z] -0.0001354 0.00013961 8.8963e-10 -2.0531e-12 v ǁVelocityǁ 6.0616e-10 0.00015039 1.0346e-05 6.2334e-06 v Pressure -0.00083488 0.017941 0.00096044 1.157e-19 v k 2.4128e-09 0.0016446 0.0011469 0.0014307 v omega 19.88 1.0313e+05 2669.9 504.17 v TempK 288 341.85 293.27 290.39 v Density 1.205 1.205 1.205 1.205 v TurbVisc 2.8339e-14 9.8341e-05 6.3434e-05 8.169e-05 v CourantNb 1.9718e-09 0.00023635 1.424e-05 7.6849e-06 v FourierNb 0.12317 0.6281 0.20107 0.17143 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9339 4.934 0.00047171 -4.473e-07 v volume_forces[Z] -4.9339 4.934 -0.00047156 5.3922e-07 v ǁvolume_forcesǁ 2.1749e-08 4.9353 0.47841 0.21537 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.49 290.53 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.016709 5.8653e-05 3.3002e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.12318 0.6281 0.20108 0.17144 INSTANT 0.476685000E+00 TIME STEP NUMBER 495 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.93389E-05 0.25104E-02 Friction velocity uk : 0.93412E-05 0.25103E-02 Dimensionless distance yplus : 0.62202E-04 0.16701E-01 Friction thermal sca. tstar : -0.15401E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.43687E-04 0.11730E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.93389E-05 0.25104E-02 Friction velocity uk : 0.93412E-05 0.25103E-02 Dimensionless distance yplus : 0.62202E-04 0.16701E-01 Friction thermal sca. tstar : -0.15401E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.43687E-04 0.11730E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34231E-08 3 0.22967E-06 0.39302E-12 0.12482E+01 c Velocity[X] 0.23244E-31 c Velocity[Y] 0.19650E-12 c Velocity[Z] 0.19652E-12 c Pressure 0.14544E-13 20 0.53765E-08 0.11371E-06 0.16361E+01 c k 0.50564E-06 2 0.63661E-07 0.84462E-08 0.19880E+01 c omega 0.13153E+02 1 0.27317E-08 0.89215E+00 0.49173E-02 c TempK 0.94537E+02 1 0.16557E-06 0.38828E-01 0.21858E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.1575e-13 9.602e-14 -1.1837e-17 -3.0335e-18 v Velocity[Y] -0.00013952 0.00013531 -1.0735e-09 -3.7283e-12 v Velocity[Z] -0.0001353 0.00013952 8.8858e-10 -2.0552e-12 v ǁVelocityǁ 6.1071e-10 0.00015029 1.0346e-05 6.238e-06 v Pressure -0.00083658 0.017959 0.0009617 -3.8927e-20 v k 2.4004e-09 0.0016414 0.0011445 0.001428 v omega 19.849 1.0313e+05 2669.9 504.14 v TempK 288 341.85 293.28 290.39 v Density 1.205 1.205 1.205 1.205 v TurbVisc 2.8192e-14 9.8325e-05 6.3405e-05 8.1658e-05 v CourantNb 1.9758e-09 0.00023615 1.4235e-05 7.6862e-06 v FourierNb 0.12308 0.6281 0.201 0.17137 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.934 4.9341 0.00047201 -4.4779e-07 v volume_forces[Z] -4.934 4.9341 -0.00047186 5.3978e-07 v ǁvolume_forcesǁ 2.1913e-08 4.9354 0.47871 0.21559 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.49 290.54 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.016701 5.863e-05 3.2987e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.12308 0.6281 0.20102 0.17138 INSTANT 0.477648000E+00 TIME STEP NUMBER 496 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.93760E-05 0.25091E-02 Friction velocity uk : 0.93783E-05 0.25091E-02 Dimensionless distance yplus : 0.62449E-04 0.16693E-01 Friction thermal sca. tstar : -0.15673E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.43860E-04 0.11724E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.93760E-05 0.25091E-02 Friction velocity uk : 0.93783E-05 0.25091E-02 Dimensionless distance yplus : 0.62449E-04 0.16693E-01 Friction thermal sca. tstar : -0.15673E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.43860E-04 0.11724E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34230E-08 3 0.22898E-06 0.39182E-12 0.12467E+01 c Velocity[X] 0.23108E-31 c Velocity[Y] 0.19590E-12 c Velocity[Z] 0.19591E-12 c Pressure 0.14482E-13 20 0.53637E-08 0.11322E-06 0.16326E+01 c k 0.50470E-06 2 0.63489E-07 0.83881E-08 0.19849E+01 c omega 0.13153E+02 1 0.27213E-08 0.88647E+00 0.49016E-02 c TempK 0.94538E+02 1 0.16510E-06 0.38712E-01 0.21825E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.1564e-13 9.5934e-14 -1.1827e-17 -3.031e-18 v Velocity[Y] -0.00013943 0.00013521 -1.0729e-09 -3.7189e-12 v Velocity[Z] -0.0001352 0.00013943 8.8752e-10 -2.0573e-12 v ǁVelocityǁ 6.1526e-10 0.00015018 1.0347e-05 6.2426e-06 v Pressure -0.00083828 0.017977 0.00096296 6.8441e-20 v k 2.388e-09 0.0016383 0.0011422 0.0014252 v omega 19.818 1.0313e+05 2669.8 504.11 v TempK 288 341.85 293.28 290.4 v Density 1.205 1.205 1.205 1.205 v TurbVisc 2.8047e-14 9.831e-05 6.3376e-05 8.1626e-05 v CourantNb 1.9797e-09 0.00023595 1.4231e-05 7.6875e-06 v FourierNb 0.12298 0.6281 0.20093 0.17131 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9341 4.9342 0.00047231 -4.4828e-07 v volume_forces[Z] -4.9341 4.9342 -0.00047216 5.4033e-07 v ǁvolume_forcesǁ 2.2077e-08 4.9355 0.47901 0.21581 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.49 290.54 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.016693 5.8606e-05 3.2973e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.12298 0.6281 0.20095 0.17132 INSTANT 0.478611000E+00 TIME STEP NUMBER 497 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.94131E-05 0.25079E-02 Friction velocity uk : 0.94154E-05 0.25079E-02 Dimensionless distance yplus : 0.62696E-04 0.16685E-01 Friction thermal sca. tstar : -0.15961E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.44034E-04 0.11719E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.94131E-05 0.25079E-02 Friction velocity uk : 0.94154E-05 0.25079E-02 Dimensionless distance yplus : 0.62696E-04 0.16685E-01 Friction thermal sca. tstar : -0.15961E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.44034E-04 0.11719E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34229E-08 3 0.22833E-06 0.39063E-12 0.12451E+01 c Velocity[X] 0.22972E-31 c Velocity[Y] 0.19531E-12 c Velocity[Z] 0.19532E-12 c Pressure 0.14446E-13 20 0.53525E-08 0.11294E-06 0.16292E+01 c k 0.50377E-06 2 0.63317E-07 0.83304E-08 0.19818E+01 c omega 0.13153E+02 1 0.27111E-08 0.88084E+00 0.48860E-02 c TempK 0.94538E+02 1 0.16464E-06 0.38597E-01 0.21793E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.1553e-13 9.5847e-14 -1.1816e-17 -3.0284e-18 v Velocity[Y] -0.00013934 0.00013512 -1.0723e-09 -3.7098e-12 v Velocity[Z] -0.00013511 0.00013934 8.8645e-10 -2.0593e-12 v ǁVelocityǁ 6.1983e-10 0.00015007 1.0347e-05 6.2472e-06 v Pressure -0.00083998 0.017995 0.00096423 -8.962e-20 v k 2.3757e-09 0.0016352 0.0011399 0.0014225 v omega 19.787 1.0313e+05 2669.8 504.08 v TempK 288 341.85 293.28 290.4 v Density 1.205 1.205 1.205 1.205 v TurbVisc 2.7902e-14 9.8294e-05 6.3347e-05 8.1594e-05 v CourantNb 1.9837e-09 0.00023575 1.4226e-05 7.6888e-06 v FourierNb 0.12288 0.6281 0.20087 0.17125 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9342 4.9343 0.0004726 -4.4877e-07 v volume_forces[Z] -4.9342 4.9343 -0.00047246 5.4088e-07 v ǁvolume_forcesǁ 2.2242e-08 4.9356 0.4793 0.21603 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.5 290.54 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.016685 5.8582e-05 3.2958e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.12289 0.6281 0.20088 0.17126 INSTANT 0.479574000E+00 TIME STEP NUMBER 498 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.94501E-05 0.25067E-02 Friction velocity uk : 0.94523E-05 0.25067E-02 Dimensionless distance yplus : 0.62942E-04 0.16677E-01 Friction thermal sca. tstar : -0.16267E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.44207E-04 0.11713E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.94501E-05 0.25067E-02 Friction velocity uk : 0.94523E-05 0.25067E-02 Dimensionless distance yplus : 0.62942E-04 0.16677E-01 Friction thermal sca. tstar : -0.16267E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.44207E-04 0.11713E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34229E-08 3 0.22768E-06 0.38945E-12 0.12436E+01 c Velocity[X] 0.22838E-31 c Velocity[Y] 0.19472E-12 c Velocity[Z] 0.19473E-12 c Pressure 0.14404E-13 20 0.53426E-08 0.11261E-06 0.16258E+01 c k 0.50283E-06 2 0.63147E-07 0.82733E-08 0.19787E+01 c omega 0.13153E+02 1 0.27008E-08 0.87526E+00 0.48705E-02 c TempK 0.94539E+02 1 0.16418E-06 0.38482E-01 0.21760E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.1542e-13 9.5761e-14 -1.1806e-17 -3.0259e-18 v Velocity[Y] -0.00013925 0.00013502 -1.0717e-09 -3.7006e-12 v Velocity[Z] -0.00013501 0.00013925 8.8537e-10 -2.0614e-12 v ǁVelocityǁ 6.2441e-10 0.00014997 1.0348e-05 6.2518e-06 v Pressure -0.00084167 0.018013 0.00096549 7.4226e-20 v k 2.3635e-09 0.0016321 0.0011376 0.0014197 v omega 19.756 1.0313e+05 2669.8 504.06 v TempK 288 341.86 293.29 290.4 v Density 1.205 1.205 1.205 1.205 v TurbVisc 2.7759e-14 9.8279e-05 6.3318e-05 8.1563e-05 v CourantNb 1.9876e-09 0.00023556 1.4222e-05 7.6902e-06 v FourierNb 0.12279 0.6281 0.2008 0.17119 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9343 4.9344 0.0004729 -4.4926e-07 v volume_forces[Z] -4.9343 4.9344 -0.00047275 5.4143e-07 v ǁvolume_forcesǁ 2.2407e-08 4.9357 0.4796 0.21625 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.5 290.54 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.016677 5.8558e-05 3.2944e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.12279 0.6281 0.20081 0.1712 INSTANT 0.480537000E+00 TIME STEP NUMBER 499 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.94870E-05 0.25056E-02 Friction velocity uk : 0.94892E-05 0.25055E-02 Dimensionless distance yplus : 0.63188E-04 0.16669E-01 Friction thermal sca. tstar : -0.16592E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.44379E-04 0.11707E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.94870E-05 0.25056E-02 Friction velocity uk : 0.94892E-05 0.25055E-02 Dimensionless distance yplus : 0.63188E-04 0.16669E-01 Friction thermal sca. tstar : -0.16592E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.44379E-04 0.11707E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34228E-08 3 0.22703E-06 0.38828E-12 0.12420E+01 c Velocity[X] 0.22705E-31 c Velocity[Y] 0.19414E-12 c Velocity[Z] 0.19415E-12 c Pressure 0.14359E-13 20 0.53331E-08 0.11225E-06 0.16224E+01 c k 0.50190E-06 2 0.62977E-07 0.82166E-08 0.19756E+01 c omega 0.13153E+02 1 0.26907E-08 0.86972E+00 0.48551E-02 c TempK 0.94540E+02 1 0.16372E-06 0.38368E-01 0.21727E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.1531e-13 9.5675e-14 -1.1795e-17 -3.0233e-18 v Velocity[Y] -0.00013916 0.00013492 -1.071e-09 -3.6915e-12 v Velocity[Z] -0.00013492 0.00013917 8.8429e-10 -2.0634e-12 v ǁVelocityǁ 6.29e-10 0.00014986 1.0348e-05 6.2564e-06 v Pressure -0.00084337 0.018032 0.00096675 9.7072e-21 v k 2.3514e-09 0.0016291 0.0011353 0.001417 v omega 19.725 1.0313e+05 2669.8 504.03 v TempK 288 341.86 293.29 290.4 v Density 1.205 1.205 1.205 1.205 v TurbVisc 2.7616e-14 9.8263e-05 6.3289e-05 8.1531e-05 v CourantNb 1.9916e-09 0.00023536 1.4217e-05 7.6915e-06 v FourierNb 0.12269 0.6281 0.20073 0.17113 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9344 4.9345 0.0004732 -4.4974e-07 v volume_forces[Z] -4.9344 4.9345 -0.00047305 5.4198e-07 v ǁvolume_forcesǁ 2.2573e-08 4.9358 0.4799 0.21647 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.5 290.55 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.016669 5.8535e-05 3.293e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.12269 0.6281 0.20075 0.17114 INSTANT 0.481500000E+00 TIME STEP NUMBER 500 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.95239E-05 0.25044E-02 Friction velocity uk : 0.95261E-05 0.25043E-02 Dimensionless distance yplus : 0.63433E-04 0.16661E-01 Friction thermal sca. tstar : -0.16938E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.44551E-04 0.11702E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.95239E-05 0.25044E-02 Friction velocity uk : 0.95261E-05 0.25043E-02 Dimensionless distance yplus : 0.63433E-04 0.16661E-01 Friction thermal sca. tstar : -0.16938E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.44551E-04 0.11702E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34228E-08 3 0.22643E-06 0.38713E-12 0.12405E+01 c Velocity[X] 0.22572E-31 c Velocity[Y] 0.19356E-12 c Velocity[Z] 0.19357E-12 c Pressure 0.14354E-13 19 0.53733E-08 0.11221E-06 0.16190E+01 c k 0.50097E-06 2 0.62808E-07 0.81604E-08 0.19725E+01 c omega 0.13153E+02 1 0.26805E-08 0.86422E+00 0.48397E-02 c TempK 0.94540E+02 1 0.16326E-06 0.38254E-01 0.21695E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.152e-13 9.5589e-14 -1.1785e-17 -3.0208e-18 v Velocity[Y] -0.00013908 0.00013483 -1.0705e-09 -3.7676e-12 v Velocity[Z] -0.00013482 0.00013908 8.8309e-10 -2.1626e-12 v ǁVelocityǁ 6.338e-10 0.00014975 1.0349e-05 6.2611e-06 v Pressure -0.00084507 0.01805 0.00096801 1.5688e-21 v k 2.3394e-09 0.001626 0.001133 0.0014143 v omega 19.694 1.0313e+05 2669.8 504 v TempK 288 341.86 293.29 290.4 v Density 1.205 1.205 1.205 1.205 v TurbVisc 2.7475e-14 9.8248e-05 6.3261e-05 8.15e-05 v CourantNb 1.9956e-09 0.00023516 1.4213e-05 7.6929e-06 v FourierNb 0.12259 0.6281 0.20067 0.17107 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9345 4.9346 0.00047349 -4.5023e-07 v volume_forces[Z] -4.9345 4.9346 -0.00047334 5.4253e-07 v ǁvolume_forcesǁ 2.2738e-08 4.9359 0.48019 0.21669 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.51 290.55 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.016661 5.8511e-05 3.2915e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.1226 0.6281 0.20068 0.17108 INSTANT 0.482463000E+00 TIME STEP NUMBER 501 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.95622E-05 0.25032E-02 Friction velocity uk : 0.95644E-05 0.25031E-02 Dimensionless distance yplus : 0.63688E-04 0.16653E-01 Friction thermal sca. tstar : -0.17308E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.44731E-04 0.11696E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.95622E-05 0.25032E-02 Friction velocity uk : 0.95644E-05 0.25031E-02 Dimensionless distance yplus : 0.63688E-04 0.16653E-01 Friction thermal sca. tstar : -0.17308E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.44731E-04 0.11696E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34228E-08 3 0.22576E-06 0.38599E-12 0.12390E+01 c Velocity[X] 0.22443E-31 c Velocity[Y] 0.19299E-12 c Velocity[Z] 0.19300E-12 c Pressure 0.14276E-13 19 0.53632E-08 0.11160E-06 0.16156E+01 c k 0.50004E-06 2 0.62640E-07 0.81047E-08 0.19695E+01 c omega 0.13153E+02 1 0.26705E-08 0.85876E+00 0.48244E-02 c TempK 0.94541E+02 1 0.16281E-06 0.38141E-01 0.21663E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.1509e-13 9.5504e-14 -1.1774e-17 -3.0183e-18 v Velocity[Y] -0.00013899 0.00013473 -1.0698e-09 -3.759e-12 v Velocity[Z] -0.00013473 0.00013899 8.82e-10 -2.1645e-12 v ǁVelocityǁ 6.3837e-10 0.00014965 1.035e-05 6.2658e-06 v Pressure -0.00084677 0.018068 0.00096926 3.1377e-21 v k 2.3275e-09 0.001623 0.0011308 0.0014116 v omega 19.664 1.0313e+05 2669.7 503.97 v TempK 288 341.86 293.3 290.41 v Density 1.205 1.205 1.205 1.205 v TurbVisc 2.7334e-14 9.8233e-05 6.3232e-05 8.1468e-05 v CourantNb 1.9995e-09 0.00023496 1.4209e-05 7.6943e-06 v FourierNb 0.1225 0.6281 0.2006 0.17101 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9346 4.9346 0.00047379 -4.5072e-07 v volume_forces[Z] -4.9346 4.9346 -0.00047364 5.4308e-07 v ǁvolume_forcesǁ 2.2912e-08 4.936 0.48049 0.21691 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.51 290.55 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.016653 5.8487e-05 3.2901e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.1225 0.6281 0.20062 0.17102 INSTANT 0.483426000E+00 TIME STEP NUMBER 502 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.95986E-05 0.25020E-02 Friction velocity uk : 0.96007E-05 0.25019E-02 Dimensionless distance yplus : 0.63930E-04 0.16645E-01 Friction thermal sca. tstar : -0.17704E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.44901E-04 0.11691E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.95986E-05 0.25020E-02 Friction velocity uk : 0.96007E-05 0.25019E-02 Dimensionless distance yplus : 0.63930E-04 0.16645E-01 Friction thermal sca. tstar : -0.17704E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.44901E-04 0.11691E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34228E-08 3 0.22510E-06 0.38486E-12 0.12375E+01 c Velocity[X] 0.22313E-31 c Velocity[Y] 0.19242E-12 c Velocity[Z] 0.19243E-12 c Pressure 0.14235E-13 19 0.53538E-08 0.11127E-06 0.16123E+01 c k 0.49912E-06 2 0.62472E-07 0.80494E-08 0.19664E+01 c omega 0.13153E+02 1 0.26604E-08 0.85335E+00 0.48092E-02 c TempK 0.94542E+02 1 0.16235E-06 0.38028E-01 0.21631E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.1498e-13 9.5419e-14 -1.1764e-17 -3.0158e-18 v Velocity[Y] -0.0001389 0.00013464 -1.0692e-09 -3.7495e-12 v Velocity[Z] -0.00013463 0.0001389 8.8089e-10 -2.1664e-12 v ǁVelocityǁ 6.4298e-10 0.00014954 1.035e-05 6.2704e-06 v Pressure -0.00084846 0.018086 0.00097052 2.9906e-20 v k 2.3156e-09 0.0016199 0.0011285 0.0014089 v omega 19.633 1.0313e+05 2669.7 503.94 v TempK 288 341.86 293.3 290.41 v Density 1.205 1.205 1.205 1.205 v TurbVisc 2.7195e-14 9.8217e-05 6.3203e-05 8.1437e-05 v CourantNb 2.0035e-09 0.00023477 1.4204e-05 7.6957e-06 v FourierNb 0.1224 0.6281 0.20054 0.17095 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9347 4.9347 0.00047408 -4.512e-07 v volume_forces[Z] -4.9347 4.9347 -0.00047394 5.4363e-07 v ǁvolume_forcesǁ 2.3077e-08 4.9361 0.48078 0.21712 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.51 290.55 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.016645 5.8464e-05 3.2887e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.1224 0.6281 0.20055 0.17096 INSTANT 0.484389000E+00 TIME STEP NUMBER 503 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.96351E-05 0.25008E-02 Friction velocity uk : 0.96372E-05 0.25007E-02 Dimensionless distance yplus : 0.64173E-04 0.16638E-01 Friction thermal sca. tstar : -0.18130E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.45071E-04 0.11685E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.96351E-05 0.25008E-02 Friction velocity uk : 0.96372E-05 0.25007E-02 Dimensionless distance yplus : 0.64173E-04 0.16638E-01 Friction thermal sca. tstar : -0.18130E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.45071E-04 0.11685E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34227E-08 3 0.22446E-06 0.38374E-12 0.12360E+01 c Velocity[X] 0.22185E-31 c Velocity[Y] 0.19186E-12 c Velocity[Z] 0.19187E-12 c Pressure 0.14199E-13 19 0.53425E-08 0.11099E-06 0.16089E+01 c k 0.49820E-06 2 0.62306E-07 0.79947E-08 0.19633E+01 c omega 0.13153E+02 1 0.26505E-08 0.84798E+00 0.47940E-02 c TempK 0.94542E+02 1 0.16190E-06 0.37916E-01 0.21598E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.1488e-13 9.5334e-14 -1.1753e-17 -3.0132e-18 v Velocity[Y] -0.00013881 0.00013455 -1.0685e-09 -3.7404e-12 v Velocity[Z] -0.00013454 0.00013882 8.7978e-10 -2.1682e-12 v ǁVelocityǁ 6.476e-10 0.00014944 1.0351e-05 6.2751e-06 v Pressure -0.00085016 0.018104 0.00097177 -1.9022e-20 v k 2.3038e-09 0.0016169 0.0011262 0.0014062 v omega 19.603 1.0313e+05 2669.7 503.92 v TempK 288 341.86 293.3 290.41 v Density 1.205 1.205 1.205 1.205 v TurbVisc 2.7056e-14 9.8202e-05 6.3175e-05 8.1405e-05 v CourantNb 2.0074e-09 0.00023457 1.42e-05 7.6972e-06 v FourierNb 0.1223 0.6281 0.20047 0.17089 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9348 4.9348 0.00047438 -4.5168e-07 v volume_forces[Z] -4.9348 4.9348 -0.00047423 5.4417e-07 v ǁvolume_forcesǁ 2.3244e-08 4.9362 0.48108 0.21734 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.52 290.56 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.016638 5.844e-05 3.2873e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.12231 0.6281 0.20048 0.1709 INSTANT 0.485352000E+00 TIME STEP NUMBER 504 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.96716E-05 0.24996E-02 Friction velocity uk : 0.96737E-05 0.24995E-02 Dimensionless distance yplus : 0.64416E-04 0.16630E-01 Friction thermal sca. tstar : -0.18588E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.45242E-04 0.11680E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.96716E-05 0.24996E-02 Friction velocity uk : 0.96737E-05 0.24995E-02 Dimensionless distance yplus : 0.64416E-04 0.16630E-01 Friction thermal sca. tstar : -0.18588E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.45242E-04 0.11680E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34228E-08 3 0.26500E-06 0.38263E-12 0.12346E+01 c Velocity[X] 0.22058E-31 c Velocity[Y] 0.19131E-12 c Velocity[Z] 0.19132E-12 c Pressure 0.14199E-13 19 0.53338E-08 0.11098E-06 0.16056E+01 c k 0.49729E-06 2 0.62140E-07 0.79403E-08 0.19603E+01 c omega 0.13153E+02 1 0.26406E-08 0.84265E+00 0.47789E-02 c TempK 0.94543E+02 1 0.16145E-06 0.37805E-01 0.21567E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.1477e-13 9.5249e-14 -1.1743e-17 -3.0107e-18 v Velocity[Y] -0.00013873 0.00013445 -1.0678e-09 -3.7312e-12 v Velocity[Z] -0.00013444 0.00013873 8.7865e-10 -2.1701e-12 v ǁVelocityǁ 6.5224e-10 0.00014933 1.0352e-05 6.2799e-06 v Pressure -0.00085186 0.018122 0.00097303 6.9421e-20 v k 2.2921e-09 0.0016139 0.001124 0.0014035 v omega 19.573 1.0313e+05 2669.7 503.89 v TempK 288 341.86 293.31 290.41 v Density 1.205 1.205 1.205 1.205 v TurbVisc 2.6919e-14 9.8187e-05 6.3146e-05 8.1374e-05 v CourantNb 2.0114e-09 0.00023438 1.4196e-05 7.6986e-06 v FourierNb 0.12221 0.6281 0.20041 0.17083 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9349 4.9349 0.00047467 -4.5216e-07 v volume_forces[Z] -4.9349 4.9349 -0.00047452 5.4471e-07 v ǁvolume_forcesǁ 2.3411e-08 4.9363 0.48137 0.21756 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.52 290.56 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.01663 5.8417e-05 3.2859e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.12221 0.6281 0.20042 0.17084 INSTANT 0.486315000E+00 TIME STEP NUMBER 505 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.97081E-05 0.24984E-02 Friction velocity uk : 0.97102E-05 0.24984E-02 Dimensionless distance yplus : 0.64659E-04 0.16622E-01 Friction thermal sca. tstar : -0.19085E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.45412E-04 0.11674E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.97081E-05 0.24984E-02 Friction velocity uk : 0.97102E-05 0.24984E-02 Dimensionless distance yplus : 0.64659E-04 0.16622E-01 Friction thermal sca. tstar : -0.19085E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.45412E-04 0.11674E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34228E-08 3 0.22320E-06 0.38153E-12 0.12331E+01 c Velocity[X] 0.21932E-31 c Velocity[Y] 0.19076E-12 c Velocity[Z] 0.19077E-12 c Pressure 0.14167E-13 19 0.53237E-08 0.11073E-06 0.16023E+01 c k 0.49637E-06 2 0.61975E-07 0.78865E-08 0.19573E+01 c omega 0.13153E+02 1 0.26307E-08 0.83737E+00 0.47639E-02 c TempK 0.94543E+02 1 0.16100E-06 0.37694E-01 0.21535E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.1466e-13 9.5164e-14 -1.1732e-17 -3.0082e-18 v Velocity[Y] -0.00013864 0.00013436 -1.0672e-09 -3.7222e-12 v Velocity[Z] -0.00013435 0.00013865 8.7752e-10 -2.1719e-12 v ǁVelocityǁ 6.5689e-10 0.00014923 1.0353e-05 6.2846e-06 v Pressure -0.00085355 0.01814 0.00097428 4.6183e-20 v k 2.2805e-09 0.0016109 0.0011218 0.0014009 v omega 19.542 1.0313e+05 2669.6 503.86 v TempK 288 341.86 293.31 290.42 v Density 1.205 1.205 1.205 1.205 v TurbVisc 2.6782e-14 9.8171e-05 6.3118e-05 8.1343e-05 v CourantNb 2.0153e-09 0.00023419 1.4191e-05 7.7001e-06 v FourierNb 0.12211 0.6281 0.20034 0.17077 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.935 4.935 0.00047496 -4.5264e-07 v volume_forces[Z] -4.935 4.935 -0.00047482 5.4525e-07 v ǁvolume_forcesǁ 2.3578e-08 4.9364 0.48166 0.21778 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.52 290.56 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.016622 5.8394e-05 3.2844e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.12212 0.6281 0.20035 0.17078 INSTANT 0.487278000E+00 TIME STEP NUMBER 506 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.97445E-05 0.24973E-02 Friction velocity uk : 0.97466E-05 0.24972E-02 Dimensionless distance yplus : 0.64901E-04 0.16614E-01 Friction thermal sca. tstar : -0.19624E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.45583E-04 0.11669E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.97445E-05 0.24973E-02 Friction velocity uk : 0.97466E-05 0.24972E-02 Dimensionless distance yplus : 0.64901E-04 0.16614E-01 Friction thermal sca. tstar : -0.19624E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.45583E-04 0.11669E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34228E-08 3 0.22393E-06 0.38044E-12 0.12317E+01 c Velocity[X] 0.21807E-31 c Velocity[Y] 0.19021E-12 c Velocity[Z] 0.19022E-12 c Pressure 0.14074E-13 19 0.53135E-08 0.11000E-06 0.15990E+01 c k 0.49546E-06 2 0.61811E-07 0.78330E-08 0.19542E+01 c omega 0.13153E+02 1 0.26209E-08 0.83212E+00 0.47490E-02 c TempK 0.94544E+02 1 0.16056E-06 0.37584E-01 0.21503E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.1456e-13 9.508e-14 -1.1722e-17 -3.0057e-18 v Velocity[Y] -0.00013856 0.00013427 -1.0665e-09 -3.7129e-12 v Velocity[Z] -0.00013426 0.00013856 8.7639e-10 -2.1738e-12 v ǁVelocityǁ 6.6155e-10 0.00014913 1.0353e-05 6.2893e-06 v Pressure -0.00085525 0.018158 0.00097553 5.138e-20 v k 2.269e-09 0.0016079 0.0011195 0.0013982 v omega 19.512 1.0313e+05 2669.6 503.84 v TempK 288 341.86 293.31 290.42 v Density 1.205 1.205 1.205 1.205 v TurbVisc 2.6646e-14 9.8156e-05 6.3089e-05 8.1312e-05 v CourantNb 2.0192e-09 0.00023399 1.4187e-05 7.7016e-06 v FourierNb 0.12202 0.6281 0.20027 0.17071 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9351 4.9351 0.00047526 -4.5312e-07 v volume_forces[Z] -4.9351 4.9351 -0.00047511 5.4579e-07 v ǁvolume_forcesǁ 2.3746e-08 4.9365 0.48196 0.21799 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.53 290.56 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.016614 5.837e-05 3.283e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.12202 0.6281 0.20029 0.17072 INSTANT 0.488241000E+00 TIME STEP NUMBER 507 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.97809E-05 0.24961E-02 Friction velocity uk : 0.97830E-05 0.24960E-02 Dimensionless distance yplus : 0.65144E-04 0.16606E-01 Friction thermal sca. tstar : -0.20214E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.45753E-04 0.11663E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.97809E-05 0.24961E-02 Friction velocity uk : 0.97830E-05 0.24960E-02 Dimensionless distance yplus : 0.65144E-04 0.16606E-01 Friction thermal sca. tstar : -0.20214E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.45753E-04 0.11663E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34228E-08 3 0.22192E-06 0.37936E-12 0.12302E+01 c Velocity[X] 0.21683E-31 c Velocity[Y] 0.18968E-12 c Velocity[Z] 0.18969E-12 c Pressure 0.14046E-13 19 0.53018E-08 0.10978E-06 0.15957E+01 c k 0.49456E-06 2 0.61648E-07 0.77800E-08 0.19512E+01 c omega 0.13153E+02 1 0.26111E-08 0.82691E+00 0.47341E-02 c TempK 0.94545E+02 1 0.16012E-06 0.37474E-01 0.21471E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.1445e-13 9.4996e-14 -1.1712e-17 -3.0033e-18 v Velocity[Y] -0.00013847 0.00013417 -1.0658e-09 -3.7038e-12 v Velocity[Z] -0.00013416 0.00013847 8.7524e-10 -2.1756e-12 v ǁVelocityǁ 6.6622e-10 0.00014902 1.0354e-05 6.2941e-06 v Pressure -0.00085695 0.018175 0.00097678 1.2203e-19 v k 2.2575e-09 0.0016049 0.0011173 0.0013955 v omega 19.482 1.0313e+05 2669.6 503.81 v TempK 288 341.86 293.31 290.42 v Density 1.205 1.205 1.205 1.205 v TurbVisc 2.6511e-14 9.8141e-05 6.3061e-05 8.1281e-05 v CourantNb 2.0232e-09 0.0002338 1.4183e-05 7.7031e-06 v FourierNb 0.12192 0.6281 0.20021 0.17065 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9352 4.9352 0.00047555 -4.536e-07 v volume_forces[Z] -4.9352 4.9352 -0.0004754 5.4633e-07 v ǁvolume_forcesǁ 2.3915e-08 4.9366 0.48225 0.21821 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.53 290.57 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.016606 5.8347e-05 3.2816e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.12193 0.6281 0.20022 0.17066 INSTANT 0.489204000E+00 TIME STEP NUMBER 508 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.98173E-05 0.24949E-02 Friction velocity uk : 0.98193E-05 0.24949E-02 Dimensionless distance yplus : 0.65385E-04 0.16598E-01 Friction thermal sca. tstar : -0.20861E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.45923E-04 0.11658E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.98173E-05 0.24949E-02 Friction velocity uk : 0.98193E-05 0.24949E-02 Dimensionless distance yplus : 0.65385E-04 0.16598E-01 Friction thermal sca. tstar : -0.20861E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.45923E-04 0.11658E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34229E-08 3 0.22130E-06 0.37829E-12 0.12288E+01 c Velocity[X] 0.21561E-31 c Velocity[Y] 0.18914E-12 c Velocity[Z] 0.18915E-12 c Pressure 0.14023E-13 19 0.52888E-08 0.10960E-06 0.15924E+01 c k 0.49365E-06 2 0.61486E-07 0.77275E-08 0.19482E+01 c omega 0.13153E+02 1 0.26014E-08 0.82175E+00 0.47193E-02 c TempK 0.94545E+02 1 0.15968E-06 0.37364E-01 0.21440E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.1434e-13 9.4912e-14 -1.1702e-17 -3.0008e-18 v Velocity[Y] -0.00013838 0.00013408 -1.0651e-09 -3.6948e-12 v Velocity[Z] -0.00013407 0.00013839 8.7409e-10 -2.1774e-12 v ǁVelocityǁ 6.7091e-10 0.00014892 1.0355e-05 6.2989e-06 v Pressure -0.00085864 0.018193 0.00097803 -1.0099e-20 v k 2.2461e-09 0.0016019 0.0011151 0.0013929 v omega 19.452 1.0313e+05 2669.6 503.78 v TempK 288 341.87 293.32 290.42 v Density 1.205 1.205 1.205 1.205 v TurbVisc 2.6378e-14 9.8126e-05 6.3033e-05 8.1249e-05 v CourantNb 2.0271e-09 0.00023361 1.4179e-05 7.7047e-06 v FourierNb 0.12183 0.6281 0.20014 0.17059 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9353 4.9353 0.00047584 -4.5408e-07 v volume_forces[Z] -4.9353 4.9353 -0.0004757 5.4687e-07 v ǁvolume_forcesǁ 2.4084e-08 4.9367 0.48254 0.21843 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.53 290.57 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.016598 5.8324e-05 3.2802e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.12183 0.6281 0.20016 0.1706 INSTANT 0.490167000E+00 TIME STEP NUMBER 509 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.98536E-05 0.24938E-02 Friction velocity uk : 0.98555E-05 0.24937E-02 Dimensionless distance yplus : 0.65627E-04 0.16591E-01 Friction thermal sca. tstar : -0.21576E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.46092E-04 0.11652E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.98536E-05 0.24938E-02 Friction velocity uk : 0.98555E-05 0.24937E-02 Dimensionless distance yplus : 0.65627E-04 0.16591E-01 Friction thermal sca. tstar : -0.21576E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.46092E-04 0.11652E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34229E-08 3 0.22066E-06 0.37723E-12 0.12274E+01 c Velocity[X] 0.21439E-31 c Velocity[Y] 0.18861E-12 c Velocity[Z] 0.18862E-12 c Pressure 0.13955E-13 19 0.52848E-08 0.10906E-06 0.15892E+01 c k 0.49275E-06 2 0.61324E-07 0.76754E-08 0.19452E+01 c omega 0.13153E+02 1 0.25918E-08 0.81662E+00 0.47046E-02 c TempK 0.94546E+02 1 0.15924E-06 0.37256E-01 0.21408E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.1424e-13 9.4829e-14 -1.1691e-17 -2.9983e-18 v Velocity[Y] -0.0001383 0.00013399 -1.0643e-09 -3.6861e-12 v Velocity[Z] -0.00013398 0.0001383 8.7293e-10 -2.1802e-12 v ǁVelocityǁ 6.756e-10 0.00014882 1.0356e-05 6.3037e-06 v Pressure -0.00086034 0.018211 0.00097927 2.1768e-20 v k 2.2348e-09 0.0015989 0.0011129 0.0013903 v omega 19.422 1.0313e+05 2669.6 503.75 v TempK 288 341.87 293.32 290.43 v Density 1.205 1.205 1.205 1.205 v TurbVisc 2.6245e-14 9.811e-05 6.3005e-05 8.1218e-05 v CourantNb 2.0311e-09 0.00023342 1.4175e-05 7.7062e-06 v FourierNb 0.12173 0.6281 0.20008 0.17053 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9354 4.9354 0.00047613 -4.5455e-07 v volume_forces[Z] -4.9354 4.9354 -0.00047599 5.4741e-07 v ǁvolume_forcesǁ 2.4253e-08 4.9368 0.48283 0.21864 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.54 290.57 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.016591 5.83e-05 3.2788e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.12174 0.6281 0.20009 0.17054 INSTANT 0.491130000E+00 TIME STEP NUMBER 510 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.98898E-05 0.24926E-02 Friction velocity uk : 0.98917E-05 0.24925E-02 Dimensionless distance yplus : 0.65868E-04 0.16583E-01 Friction thermal sca. tstar : -0.22372E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.46261E-04 0.11647E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.98898E-05 0.24926E-02 Friction velocity uk : 0.98917E-05 0.24925E-02 Dimensionless distance yplus : 0.65868E-04 0.16583E-01 Friction thermal sca. tstar : -0.22372E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.46261E-04 0.11647E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34230E-08 3 0.22005E-06 0.37618E-12 0.12260E+01 c Velocity[X] 0.21318E-31 c Velocity[Y] 0.18809E-12 c Velocity[Z] 0.18810E-12 c Pressure 0.13947E-13 19 0.52715E-08 0.10900E-06 0.15859E+01 c k 0.49185E-06 2 0.61163E-07 0.76237E-08 0.19422E+01 c omega 0.13153E+02 1 0.25822E-08 0.81154E+00 0.46899E-02 c TempK 0.94547E+02 1 0.15880E-06 0.37147E-01 0.21377E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.1413e-13 9.4745e-14 -1.1681e-17 -2.9958e-18 v Velocity[Y] -0.00013821 0.0001339 -1.0636e-09 -3.6773e-12 v Velocity[Z] -0.00013389 0.00013822 8.7176e-10 -2.182e-12 v ǁVelocityǁ 6.8031e-10 0.00014872 1.0357e-05 6.3085e-06 v Pressure -0.00086203 0.018229 0.00098052 5.1478e-20 v k 2.2236e-09 0.001596 0.0011107 0.0013876 v omega 19.393 1.0313e+05 2669.5 503.73 v TempK 288 341.87 293.32 290.43 v Density 1.205 1.205 1.205 1.205 v TurbVisc 2.6112e-14 9.8095e-05 6.2976e-05 8.1187e-05 v CourantNb 2.035e-09 0.00023323 1.4171e-05 7.7078e-06 v FourierNb 0.12164 0.6281 0.20002 0.17048 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9355 4.9355 0.00047643 -4.5503e-07 v volume_forces[Z] -4.9355 4.9355 -0.00047628 5.4794e-07 v ǁvolume_forcesǁ 2.4423e-08 4.9369 0.48312 0.21886 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.54 290.57 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.016583 5.8277e-05 3.2774e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.12164 0.6281 0.20003 0.17048 INSTANT 0.492093000E+00 TIME STEP NUMBER 511 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.99259E-05 0.24914E-02 Friction velocity uk : 0.99279E-05 0.24914E-02 Dimensionless distance yplus : 0.66109E-04 0.16575E-01 Friction thermal sca. tstar : -0.23264E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.46430E-04 0.11641E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.99259E-05 0.24914E-02 Friction velocity uk : 0.99279E-05 0.24914E-02 Dimensionless distance yplus : 0.66109E-04 0.16575E-01 Friction thermal sca. tstar : -0.23264E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.46430E-04 0.11641E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34231E-08 3 0.21943E-06 0.37514E-12 0.12246E+01 c Velocity[X] 0.21199E-31 c Velocity[Y] 0.18757E-12 c Velocity[Z] 0.18758E-12 c Pressure 0.13917E-13 19 0.52588E-08 0.10876E-06 0.15827E+01 c k 0.49096E-06 2 0.61003E-07 0.75725E-08 0.19393E+01 c omega 0.13153E+02 1 0.25726E-08 0.80649E+00 0.46753E-02 c TempK 0.94547E+02 1 0.15837E-06 0.37040E-01 0.21346E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.1403e-13 9.4662e-14 -1.1671e-17 -2.9934e-18 v Velocity[Y] -0.00013813 0.0001338 -1.0629e-09 -3.6682e-12 v Velocity[Z] -0.00013379 0.00013813 8.7059e-10 -2.1839e-12 v ǁVelocityǁ 6.8503e-10 0.00014861 1.0358e-05 6.3133e-06 v Pressure -0.00086373 0.018247 0.00098176 1.1717e-19 v k 2.2125e-09 0.001593 0.0011085 0.001385 v omega 19.363 1.0313e+05 2669.5 503.7 v TempK 288 341.87 293.33 290.43 v Density 1.205 1.205 1.205 1.205 v TurbVisc 2.5981e-14 9.808e-05 6.2948e-05 8.1156e-05 v CourantNb 2.0389e-09 0.00023304 1.4167e-05 7.7094e-06 v FourierNb 0.12154 0.6281 0.19995 0.17042 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9356 4.9356 0.00047672 -4.555e-07 v volume_forces[Z] -4.9356 4.9356 -0.00047657 5.4848e-07 v ǁvolume_forcesǁ 2.4593e-08 4.937 0.48342 0.21908 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.54 290.58 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.016575 5.8254e-05 3.276e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.12155 0.6281 0.19997 0.17042 INSTANT 0.493056000E+00 TIME STEP NUMBER 512 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.99621E-05 0.24903E-02 Friction velocity uk : 0.99640E-05 0.24902E-02 Dimensionless distance yplus : 0.66349E-04 0.16568E-01 Friction thermal sca. tstar : -0.24275E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.46599E-04 0.11636E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.99621E-05 0.24903E-02 Friction velocity uk : 0.99640E-05 0.24902E-02 Dimensionless distance yplus : 0.66349E-04 0.16568E-01 Friction thermal sca. tstar : -0.24275E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.46599E-04 0.11636E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34232E-08 3 0.21886E-06 0.37412E-12 0.12232E+01 c Velocity[X] 0.21080E-31 c Velocity[Y] 0.18705E-12 c Velocity[Z] 0.18706E-12 c Pressure 0.13984E-13 19 0.52598E-08 0.10928E-06 0.15794E+01 c k 0.49007E-06 2 0.60844E-07 0.75217E-08 0.19363E+01 c omega 0.13153E+02 1 0.25631E-08 0.80149E+00 0.46607E-02 c TempK 0.94548E+02 1 0.15793E-06 0.36932E-01 0.21315E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.1392e-13 9.458e-14 -1.1661e-17 -2.9909e-18 v Velocity[Y] -0.00013805 0.00013371 -1.0621e-09 -3.6597e-12 v Velocity[Z] -0.0001337 0.00013805 8.694e-10 -2.1857e-12 v ǁVelocityǁ 6.8975e-10 0.00014851 1.0359e-05 6.3181e-06 v Pressure -0.00086542 0.018265 0.000983 -4.9615e-20 v k 2.2014e-09 0.0015901 0.0011063 0.0013824 v omega 19.333 1.0313e+05 2669.5 503.67 v TempK 288 341.87 293.33 290.43 v Density 1.205 1.205 1.205 1.205 v TurbVisc 2.5851e-14 9.8065e-05 6.292e-05 8.1126e-05 v CourantNb 2.0429e-09 0.00023285 1.4163e-05 7.711e-06 v FourierNb 0.12145 0.6281 0.19989 0.17036 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9357 4.9357 0.00047701 -4.5597e-07 v volume_forces[Z] -4.9357 4.9357 -0.00047686 5.4901e-07 v ǁvolume_forcesǁ 2.4764e-08 4.9371 0.48371 0.21929 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.55 290.58 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.016568 5.8231e-05 3.2746e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.12145 0.6281 0.1999 0.17037 INSTANT 0.494019000E+00 TIME STEP NUMBER 513 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.99981E-05 0.24891E-02 Friction velocity uk : 0.10000E-04 0.24891E-02 Dimensionless distance yplus : 0.66589E-04 0.16560E-01 Friction thermal sca. tstar : -0.25426E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.46768E-04 0.11631E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.99981E-05 0.24891E-02 Friction velocity uk : 0.10000E-04 0.24891E-02 Dimensionless distance yplus : 0.66589E-04 0.16560E-01 Friction thermal sca. tstar : -0.25426E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.46768E-04 0.11631E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34233E-08 3 0.21823E-06 0.37309E-12 0.12218E+01 c Velocity[X] 0.20962E-31 c Velocity[Y] 0.18654E-12 c Velocity[Z] 0.18655E-12 c Pressure 0.13808E-13 19 0.52456E-08 0.10791E-06 0.15762E+01 c k 0.48918E-06 2 0.60685E-07 0.74713E-08 0.19334E+01 c omega 0.13153E+02 1 0.25537E-08 0.79652E+00 0.46463E-02 c TempK 0.94548E+02 1 0.15750E-06 0.36826E-01 0.21284E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.1382e-13 9.4497e-14 -1.1651e-17 -2.9885e-18 v Velocity[Y] -0.00013796 0.00013362 -1.0614e-09 -3.6503e-12 v Velocity[Z] -0.00013361 0.00013797 8.6821e-10 -2.1875e-12 v ǁVelocityǁ 6.9449e-10 0.00014841 1.036e-05 6.323e-06 v Pressure -0.00086712 0.018283 0.00098425 -2.7357e-20 v k 2.1904e-09 0.0015872 0.0011041 0.0013798 v omega 19.304 1.0313e+05 2669.5 503.65 v TempK 288 341.87 293.33 290.44 v Density 1.205 1.205 1.205 1.205 v TurbVisc 2.5722e-14 9.805e-05 6.2892e-05 8.1095e-05 v CourantNb 2.0468e-09 0.00023266 1.4159e-05 7.7126e-06 v FourierNb 0.12135 0.6281 0.19982 0.1703 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9358 4.9358 0.0004773 -4.5644e-07 v volume_forces[Z] -4.9358 4.9358 -0.00047715 5.4954e-07 v ǁvolume_forcesǁ 2.4935e-08 4.9371 0.484 0.21951 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.55 290.58 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.01656 5.8208e-05 3.2732e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.12136 0.6281 0.19984 0.17031 INSTANT 0.494982000E+00 TIME STEP NUMBER 514 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10034E-04 0.24880E-02 Friction velocity uk : 0.10036E-04 0.24879E-02 Dimensionless distance yplus : 0.66829E-04 0.16552E-01 Friction thermal sca. tstar : -0.26755E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.46936E-04 0.11625E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10034E-04 0.24880E-02 Friction velocity uk : 0.10036E-04 0.24879E-02 Dimensionless distance yplus : 0.66829E-04 0.16552E-01 Friction thermal sca. tstar : -0.26755E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.46936E-04 0.11625E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34234E-08 3 0.21757E-06 0.37208E-12 0.12204E+01 c Velocity[X] 0.20847E-31 c Velocity[Y] 0.18604E-12 c Velocity[Z] 0.18604E-12 c Pressure 0.13765E-13 19 0.51929E-08 0.10756E-06 0.15730E+01 c k 0.48829E-06 2 0.60527E-07 0.74213E-08 0.19304E+01 c omega 0.13153E+02 1 0.25442E-08 0.79159E+00 0.46319E-02 c TempK 0.94549E+02 1 0.15707E-06 0.36719E-01 0.21253E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.1371e-13 9.4415e-14 -1.164e-17 -2.9861e-18 v Velocity[Y] -0.00013788 0.00013353 -1.0605e-09 -3.4835e-12 v Velocity[Z] -0.00013352 0.00013788 8.6726e-10 -1.9519e-12 v ǁVelocityǁ 6.9922e-10 0.00014831 1.0361e-05 6.3278e-06 v Pressure -0.00086881 0.0183 0.00098549 2.77e-20 v k 2.1795e-09 0.0015842 0.0011019 0.0013772 v omega 19.275 1.0313e+05 2669.5 503.62 v TempK 288 341.87 293.34 290.44 v Density 1.205 1.205 1.205 1.205 v TurbVisc 2.5593e-14 9.8035e-05 6.2864e-05 8.1064e-05 v CourantNb 2.0507e-09 0.00023247 1.4155e-05 7.7143e-06 v FourierNb 0.12126 0.6281 0.19976 0.17024 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9359 4.9359 0.00047759 -4.5691e-07 v volume_forces[Z] -4.9359 4.9359 -0.00047744 5.5007e-07 v ǁvolume_forcesǁ 2.5106e-08 4.9372 0.48429 0.21972 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.55 290.58 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.016552 5.8185e-05 3.2718e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.12126 0.6281 0.19977 0.17025 INSTANT 0.495945000E+00 TIME STEP NUMBER 515 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10070E-04 0.24868E-02 Friction velocity uk : 0.10072E-04 0.24868E-02 Dimensionless distance yplus : 0.67067E-04 0.16545E-01 Friction thermal sca. tstar : -0.28323E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.47103E-04 0.11620E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10070E-04 0.24868E-02 Friction velocity uk : 0.10072E-04 0.24868E-02 Dimensionless distance yplus : 0.67067E-04 0.16545E-01 Friction thermal sca. tstar : -0.28323E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.47103E-04 0.11620E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34235E-08 3 0.21694E-06 0.37108E-12 0.12190E+01 c Velocity[X] 0.20730E-31 c Velocity[Y] 0.18553E-12 c Velocity[Z] 0.18554E-12 c Pressure 0.13721E-13 19 0.51840E-08 0.10722E-06 0.15698E+01 c k 0.48741E-06 2 0.60370E-07 0.73717E-08 0.19275E+01 c omega 0.13153E+02 1 0.25349E-08 0.78669E+00 0.46175E-02 c TempK 0.94550E+02 1 0.15665E-06 0.36614E-01 0.21222E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.1361e-13 9.4332e-14 -1.163e-17 -2.9836e-18 v Velocity[Y] -0.00013779 0.00013344 -1.0597e-09 -3.4736e-12 v Velocity[Z] -0.00013343 0.0001378 8.6605e-10 -1.9537e-12 v ǁVelocityǁ 7.0404e-10 0.00014821 1.0362e-05 6.3327e-06 v Pressure -0.00087051 0.018318 0.00098672 7.9178e-20 v k 2.1686e-09 0.0015813 0.0010998 0.0013746 v omega 19.245 1.0313e+05 2669.4 503.59 v TempK 288 341.87 293.34 290.44 v Density 1.205 1.205 1.205 1.205 v TurbVisc 2.5465e-14 9.802e-05 6.2836e-05 8.1033e-05 v CourantNb 2.0546e-09 0.00023228 1.4151e-05 7.7159e-06 v FourierNb 0.12117 0.6281 0.1997 0.17018 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.936 4.936 0.00047788 -4.5737e-07 v volume_forces[Z] -4.936 4.936 -0.00047773 5.506e-07 v ǁvolume_forcesǁ 2.5277e-08 4.9373 0.48457 0.21994 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.56 290.58 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.016545 5.8162e-05 3.2704e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.12117 0.6281 0.19971 0.17019 INSTANT 0.496908000E+00 TIME STEP NUMBER 516 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10106E-04 0.24857E-02 Friction velocity uk : 0.10108E-04 0.24856E-02 Dimensionless distance yplus : 0.67308E-04 0.16537E-01 Friction thermal sca. tstar : -0.30210E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.47273E-04 0.11615E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10106E-04 0.24857E-02 Friction velocity uk : 0.10108E-04 0.24856E-02 Dimensionless distance yplus : 0.67308E-04 0.16537E-01 Friction thermal sca. tstar : -0.30210E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.47273E-04 0.11615E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34236E-08 3 0.21633E-06 0.37008E-12 0.12177E+01 c Velocity[X] 0.20615E-31 c Velocity[Y] 0.18504E-12 c Velocity[Z] 0.18505E-12 c Pressure 0.13684E-13 19 0.51748E-08 0.10693E-06 0.15667E+01 c k 0.48653E-06 2 0.60214E-07 0.73226E-08 0.19245E+01 c omega 0.13153E+02 1 0.25256E-08 0.78184E+00 0.46033E-02 c TempK 0.94550E+02 1 0.15622E-06 0.36509E-01 0.21191E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.1351e-13 9.425e-14 -1.162e-17 -2.9812e-18 v Velocity[Y] -0.00013771 0.00013335 -1.0589e-09 -3.4659e-12 v Velocity[Z] -0.00013334 0.00013771 8.6484e-10 -1.9561e-12 v ǁVelocityǁ 7.0884e-10 0.00014811 1.0363e-05 6.3376e-06 v Pressure -0.0008722 0.018336 0.00098796 3.5544e-20 v k 2.1578e-09 0.0015784 0.0010976 0.0013721 v omega 19.216 1.0313e+05 2669.4 503.57 v TempK 288 341.87 293.34 290.44 v Density 1.205 1.205 1.205 1.205 v TurbVisc 2.5339e-14 9.8005e-05 6.2809e-05 8.1003e-05 v CourantNb 2.0546e-09 0.0002321 1.4147e-05 7.7176e-06 v FourierNb 0.12107 0.6281 0.19963 0.17012 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.936 4.9361 0.00047817 -4.5784e-07 v volume_forces[Z] -4.936 4.9361 -0.00047802 5.5112e-07 v ǁvolume_forcesǁ 2.5451e-08 4.9374 0.48486 0.22015 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.56 290.59 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.016537 5.8139e-05 3.2691e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.12108 0.6281 0.19965 0.17013 INSTANT 0.497871000E+00 TIME STEP NUMBER 517 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+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-04 0.24846E-02 Friction velocity uk : 0.10144E-04 0.24845E-02 Dimensionless distance yplus : 0.67549E-04 0.16529E-01 Friction thermal sca. tstar : -0.32540E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.47442E-04 0.11609E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+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-04 0.24846E-02 Friction velocity uk : 0.10144E-04 0.24845E-02 Dimensionless distance yplus : 0.67549E-04 0.16529E-01 Friction thermal sca. tstar : -0.32540E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.47442E-04 0.11609E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34237E-08 3 0.21573E-06 0.36909E-12 0.12163E+01 c Velocity[X] 0.20502E-31 c Velocity[Y] 0.18454E-12 c Velocity[Z] 0.18455E-12 c Pressure 0.13646E-13 19 0.51655E-08 0.10663E-06 0.15635E+01 c k 0.48565E-06 2 0.60058E-07 0.72738E-08 0.19216E+01 c omega 0.13153E+02 1 0.25163E-08 0.77702E+00 0.45891E-02 c TempK 0.94551E+02 1 0.15580E-06 0.36404E-01 0.21161E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.134e-13 9.4169e-14 -1.161e-17 -2.9788e-18 v Velocity[Y] -0.00013763 0.00013326 -1.0582e-09 -3.4573e-12 v Velocity[Z] -0.00013325 0.00013763 8.6362e-10 -1.9583e-12 v ǁVelocityǁ 7.1364e-10 0.00014801 1.0364e-05 6.3425e-06 v Pressure -0.0008739 0.018354 0.0009892 1.7453e-20 v k 2.1471e-09 0.0015755 0.0010955 0.0013695 v omega 19.187 1.0313e+05 2669.4 503.54 v TempK 288 341.87 293.35 290.45 v Density 1.205 1.205 1.205 1.205 v TurbVisc 2.5213e-14 9.799e-05 6.2781e-05 8.0972e-05 v CourantNb 2.0534e-09 0.00023191 1.4143e-05 7.7193e-06 v FourierNb 0.12098 0.6281 0.19957 0.17007 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9361 4.9362 0.00047845 -4.5831e-07 v volume_forces[Z] -4.9361 4.9362 -0.00047831 5.5165e-07 v ǁvolume_forcesǁ 2.5625e-08 4.9375 0.48515 0.22037 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.56 290.59 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.016529 5.8116e-05 3.2677e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.12098 0.6281 0.19958 0.17007 INSTANT 0.498834000E+00 TIME STEP NUMBER 518 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10178E-04 0.24834E-02 Friction velocity uk : 0.10180E-04 0.24833E-02 Dimensionless distance yplus : 0.67788E-04 0.16522E-01 Friction thermal sca. tstar : -0.35518E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.47610E-04 0.11604E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10178E-04 0.24834E-02 Friction velocity uk : 0.10180E-04 0.24833E-02 Dimensionless distance yplus : 0.67788E-04 0.16522E-01 Friction thermal sca. tstar : -0.35518E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.47610E-04 0.11604E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34239E-08 3 0.21512E-06 0.36811E-12 0.12150E+01 c Velocity[X] 0.20389E-31 c Velocity[Y] 0.18405E-12 c Velocity[Z] 0.18406E-12 c Pressure 0.13613E-13 19 0.51550E-08 0.10636E-06 0.15604E+01 c k 0.48477E-06 2 0.59903E-07 0.72255E-08 0.19187E+01 c omega 0.13153E+02 1 0.25071E-08 0.77224E+00 0.45749E-02 c TempK 0.94552E+02 1 0.15538E-06 0.36300E-01 0.21130E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.133e-13 9.4087e-14 -1.16e-17 -2.9764e-18 v Velocity[Y] -0.00013755 0.00013317 -1.0574e-09 -3.4489e-12 v Velocity[Z] -0.00013316 0.00013755 8.6239e-10 -1.9604e-12 v ǁVelocityǁ 7.1844e-10 0.00014791 1.0365e-05 6.3474e-06 v Pressure -0.00087559 0.018371 0.00099043 -2.0591e-20 v k 2.1365e-09 0.0015726 0.0010933 0.0013669 v omega 19.158 1.0313e+05 2669.4 503.52 v TempK 288 341.88 293.35 290.45 v Density 1.205 1.205 1.205 1.205 v TurbVisc 2.5087e-14 9.7975e-05 6.2753e-05 8.0941e-05 v CourantNb 2.0521e-09 0.00023172 1.4139e-05 7.721e-06 v FourierNb 0.12089 0.6281 0.19951 0.17001 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9362 4.9363 0.00047874 -4.5877e-07 v volume_forces[Z] -4.9362 4.9363 -0.0004786 5.5218e-07 v ǁvolume_forcesǁ 2.5798e-08 4.9376 0.48544 0.22058 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.57 290.59 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.016522 5.8093e-05 3.2663e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.12089 0.6281 0.19952 0.17002 INSTANT 0.499797000E+00 TIME STEP NUMBER 519 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10214E-04 0.24823E-02 Friction velocity uk : 0.10216E-04 0.24822E-02 Dimensionless distance yplus : 0.68026E-04 0.16514E-01 Friction thermal sca. tstar : -0.39513E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.47777E-04 0.11599E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10214E-04 0.24823E-02 Friction velocity uk : 0.10216E-04 0.24822E-02 Dimensionless distance yplus : 0.68026E-04 0.16514E-01 Friction thermal sca. tstar : -0.39513E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.47777E-04 0.11599E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34240E-08 3 0.21452E-06 0.36714E-12 0.12136E+01 c Velocity[X] 0.20277E-31 c Velocity[Y] 0.18357E-12 c Velocity[Z] 0.18358E-12 c Pressure 0.13587E-13 19 0.51455E-08 0.10616E-06 0.15572E+01 c k 0.48390E-06 2 0.59749E-07 0.71775E-08 0.19158E+01 c omega 0.13153E+02 1 0.24979E-08 0.76749E+00 0.45608E-02 c TempK 0.94552E+02 1 0.15496E-06 0.36196E-01 0.21100E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.132e-13 9.4006e-14 -1.159e-17 -2.974e-18 v Velocity[Y] -0.00013746 0.00013308 -1.0566e-09 -3.4405e-12 v Velocity[Z] -0.00013307 0.00013747 8.6115e-10 -1.9625e-12 v ǁVelocityǁ 7.2325e-10 0.00014781 1.0366e-05 6.3523e-06 v Pressure -0.00087729 0.018389 0.00099167 6.4176e-20 v k 2.1259e-09 0.0015697 0.0010912 0.0013644 v omega 19.129 1.0313e+05 2669.3 503.49 v TempK 288 341.88 293.35 290.45 v Density 1.205 1.205 1.205 1.205 v TurbVisc 2.4963e-14 9.796e-05 6.2725e-05 8.0911e-05 v CourantNb 2.0509e-09 0.00023154 1.4136e-05 7.7227e-06 v FourierNb 0.12079 0.6281 0.19944 0.16995 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9363 4.9364 0.00047903 -4.5924e-07 v volume_forces[Z] -4.9363 4.9364 -0.00047888 5.527e-07 v ǁvolume_forcesǁ 2.5972e-08 4.9377 0.48573 0.2208 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.57 290.59 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.016514 5.807e-05 3.2649e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.1208 0.6281 0.19946 0.16996 INSTANT 0.500760000E+00 TIME STEP NUMBER 520 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10250E-04 0.24811E-02 Friction velocity uk : 0.10252E-04 0.24811E-02 Dimensionless distance yplus : 0.68264E-04 0.16507E-01 Friction thermal sca. tstar : -0.45272E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.47944E-04 0.11593E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10250E-04 0.24811E-02 Friction velocity uk : 0.10252E-04 0.24811E-02 Dimensionless distance yplus : 0.68264E-04 0.16507E-01 Friction thermal sca. tstar : -0.45272E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.47944E-04 0.11593E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34242E-08 3 0.21392E-06 0.36618E-12 0.12123E+01 c Velocity[X] 0.20166E-31 c Velocity[Y] 0.18309E-12 c Velocity[Z] 0.18310E-12 c Pressure 0.13545E-13 19 0.51384E-08 0.10583E-06 0.15541E+01 c k 0.48303E-06 2 0.59596E-07 0.71299E-08 0.19129E+01 c omega 0.13153E+02 1 0.24888E-08 0.76278E+00 0.45468E-02 c TempK 0.94553E+02 1 0.15454E-06 0.36093E-01 0.21070E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.131e-13 9.3925e-14 -1.158e-17 -2.9716e-18 v Velocity[Y] -0.00013738 0.00013299 -1.0558e-09 -3.4321e-12 v Velocity[Z] -0.00013298 0.00013738 8.5991e-10 -1.9647e-12 v ǁVelocityǁ 7.2807e-10 0.00014771 1.0367e-05 6.3573e-06 v Pressure -0.00087898 0.018407 0.0009929 -8.1188e-20 v k 2.1154e-09 0.0015669 0.0010891 0.0013619 v omega 19.1 1.0313e+05 2669.3 503.46 v TempK 288 341.88 293.36 290.45 v Density 1.205 1.205 1.205 1.205 v TurbVisc 2.484e-14 9.7945e-05 6.2698e-05 8.088e-05 v CourantNb 2.0496e-09 0.00023135 1.4132e-05 7.7245e-06 v FourierNb 0.1207 0.6281 0.19938 0.16989 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9364 4.9364 0.00047932 -4.597e-07 v volume_forces[Z] -4.9364 4.9364 -0.00047917 5.5322e-07 v ǁvolume_forcesǁ 2.6146e-08 4.9378 0.48601 0.22101 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.57 290.6 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.016507 5.8047e-05 3.2635e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.1207 0.6281 0.19939 0.1699 INSTANT 0.501723000E+00 TIME STEP NUMBER 521 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10285E-04 0.24800E-02 Friction velocity uk : 0.10287E-04 0.24799E-02 Dimensionless distance yplus : 0.68501E-04 0.16499E-01 Friction thermal sca. tstar : -0.54640E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.48111E-04 0.11588E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10285E-04 0.24800E-02 Friction velocity uk : 0.10287E-04 0.24799E-02 Dimensionless distance yplus : 0.68501E-04 0.16499E-01 Friction thermal sca. tstar : -0.54640E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.48111E-04 0.11588E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34243E-08 3 0.21332E-06 0.36523E-12 0.12110E+01 c Velocity[X] 0.20056E-31 c Velocity[Y] 0.18261E-12 c Velocity[Z] 0.18262E-12 c Pressure 0.13498E-13 19 0.51286E-08 0.10546E-06 0.15510E+01 c k 0.48217E-06 2 0.59443E-07 0.70827E-08 0.19100E+01 c omega 0.13153E+02 1 0.24797E-08 0.75811E+00 0.45329E-02 c TempK 0.94553E+02 1 0.15413E-06 0.35990E-01 0.21039E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.1299e-13 9.3844e-14 -1.1571e-17 -2.9692e-18 v Velocity[Y] -0.0001373 0.0001329 -1.0549e-09 -3.4236e-12 v Velocity[Z] -0.00013289 0.0001373 8.5866e-10 -1.9668e-12 v ǁVelocityǁ 7.329e-10 0.00014761 1.0368e-05 6.3622e-06 v Pressure -0.00088068 0.018424 0.00099413 -2.5592e-20 v k 2.105e-09 0.001564 0.0010869 0.0013593 v omega 19.071 1.0313e+05 2669.3 503.44 v TempK 288 341.88 293.36 290.46 v Density 1.205 1.205 1.205 1.205 v TurbVisc 2.4717e-14 9.793e-05 6.267e-05 8.085e-05 v CourantNb 2.0483e-09 0.00023117 1.4128e-05 7.7262e-06 v FourierNb 0.12061 0.6281 0.19932 0.16983 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9365 4.9365 0.0004796 -4.6017e-07 v volume_forces[Z] -4.9365 4.9365 -0.00047946 5.5375e-07 v ǁvolume_forcesǁ 2.632e-08 4.9379 0.4863 0.22122 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.58 290.6 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.016499 5.8024e-05 3.2621e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.12061 0.6281 0.19933 0.16984 INSTANT 0.502686000E+00 TIME STEP NUMBER 522 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10321E-04 0.24789E-02 Friction velocity uk : 0.10323E-04 0.24788E-02 Dimensionless distance yplus : 0.68738E-04 0.16492E-01 Friction thermal sca. tstar : -0.74201E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.48277E-04 0.11583E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10321E-04 0.24789E-02 Friction velocity uk : 0.10323E-04 0.24788E-02 Dimensionless distance yplus : 0.68738E-04 0.16492E-01 Friction thermal sca. tstar : -0.74201E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.48277E-04 0.11583E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34245E-08 3 0.21272E-06 0.36428E-12 0.12097E+01 c Velocity[X] 0.19947E-31 c Velocity[Y] 0.18214E-12 c Velocity[Z] 0.18214E-12 c Pressure 0.13462E-13 19 0.51193E-08 0.10517E-06 0.15479E+01 c k 0.48130E-06 2 0.59291E-07 0.70359E-08 0.19072E+01 c omega 0.13153E+02 1 0.24707E-08 0.75347E+00 0.45190E-02 c TempK 0.94554E+02 1 0.15371E-06 0.35888E-01 0.21009E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.1289e-13 9.3763e-14 -1.1561e-17 -2.9668e-18 v Velocity[Y] -0.00013722 0.00013281 -1.0541e-09 -3.4153e-12 v Velocity[Z] -0.0001328 0.00013722 8.574e-10 -1.9688e-12 v ǁVelocityǁ 7.3774e-10 0.00014751 1.0369e-05 6.3672e-06 v Pressure -0.00088237 0.018442 0.00099536 -5.5008e-20 v k 2.0946e-09 0.0015611 0.0010848 0.0013568 v omega 19.043 1.0313e+05 2669.3 503.41 v TempK 288 341.88 293.36 290.46 v Density 1.205 1.205 1.205 1.205 v TurbVisc 2.4595e-14 9.7915e-05 6.2643e-05 8.0819e-05 v CourantNb 2.047e-09 0.00023099 1.4125e-05 7.728e-06 v FourierNb 0.12051 0.6281 0.19925 0.16978 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9366 4.9366 0.00047989 -4.6063e-07 v volume_forces[Z] -4.9366 4.9366 -0.00047974 5.5427e-07 v ǁvolume_forcesǁ 2.6494e-08 4.938 0.48659 0.22144 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.58 290.6 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.016492 5.8001e-05 3.2607e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.12052 0.6281 0.19927 0.16978 INSTANT 0.503649000E+00 TIME STEP NUMBER 523 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10357E-04 0.24778E-02 Friction velocity uk : 0.10358E-04 0.24777E-02 Dimensionless distance yplus : 0.68975E-04 0.16484E-01 Friction thermal sca. tstar : -0.18910E+05 0.00000E+00 Dim-less thermal sca. tplus : 0.48443E-04 0.11578E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10357E-04 0.24778E-02 Friction velocity uk : 0.10358E-04 0.24777E-02 Dimensionless distance yplus : 0.68975E-04 0.16484E-01 Friction thermal sca. tstar : -0.18910E+05 0.00000E+00 Dim-less thermal sca. tplus : 0.48443E-04 0.11578E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34247E-08 3 0.21212E-06 0.36334E-12 0.12084E+01 c Velocity[X] 0.19760E-31 c Velocity[Y] 0.18167E-12 c Velocity[Z] 0.18167E-12 c Pressure 0.13423E-13 20 0.91291E-08 0.10487E-06 0.15448E+01 c k 0.48044E-06 2 0.59140E-07 0.69895E-08 0.19043E+01 c omega 0.13153E+02 1 0.24617E-08 0.74887E+00 0.45052E-02 c TempK 0.94555E+02 1 0.15330E-06 0.35786E-01 0.20979E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.1279e-13 9.3683e-14 -1.1551e-17 -2.9646e-18 v Velocity[Y] -0.00013714 0.00013272 -1.0536e-09 -3.8019e-12 v Velocity[Z] -0.00013271 0.00013714 8.5645e-10 -1.6242e-12 v ǁVelocityǁ 7.3792e-10 0.00014741 1.0371e-05 6.3722e-06 v Pressure -0.00088406 0.01846 0.00099659 -8.4227e-20 v k 2.0843e-09 0.0015583 0.0010827 0.0013543 v omega 19.014 1.0313e+05 2669.3 503.39 v TempK 288 341.88 293.37 290.46 v Density 1.205 1.205 1.205 1.205 v TurbVisc 2.4474e-14 9.79e-05 6.2615e-05 8.0789e-05 v CourantNb 2.0527e-09 0.0002308 1.4121e-05 7.7298e-06 v FourierNb 0.12042 0.6281 0.19919 0.16972 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9367 4.9367 0.00048018 -4.6109e-07 v volume_forces[Z] -4.9367 4.9367 -0.00048003 5.5479e-07 v ǁvolume_forcesǁ 2.6669e-08 4.9381 0.48687 0.22165 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.58 290.6 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.016484 5.7977e-05 3.2593e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.12042 0.6281 0.19921 0.16973 INSTANT 0.504612000E+00 TIME STEP NUMBER 524 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10358E-04 0.24766E-02 Friction velocity uk : 0.10359E-04 0.24766E-02 Dimensionless distance yplus : 0.68981E-04 0.16477E-01 Friction thermal sca. tstar : -0.10866E+05 0.00000E+00 Dim-less thermal sca. tplus : 0.48448E-04 0.11572E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10358E-04 0.24766E-02 Friction velocity uk : 0.10359E-04 0.24766E-02 Dimensionless distance yplus : 0.68981E-04 0.16477E-01 Friction thermal sca. tstar : -0.10866E+05 0.00000E+00 Dim-less thermal sca. tplus : 0.48448E-04 0.11572E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34249E-08 3 0.21249E-06 0.36241E-12 0.12071E+01 c Velocity[X] 0.19706E-31 c Velocity[Y] 0.18120E-12 c Velocity[Z] 0.18121E-12 c Pressure 0.13468E-13 20 0.91580E-08 0.10522E-06 0.15418E+01 c k 0.47958E-06 2 0.58989E-07 0.69435E-08 0.19014E+01 c omega 0.13153E+02 1 0.24527E-08 0.74430E+00 0.44914E-02 c TempK 0.94555E+02 1 0.15289E-06 0.35685E-01 0.20949E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.1269e-13 9.3603e-14 -1.1541e-17 -2.9621e-18 v Velocity[Y] -0.00013705 0.00013264 -1.0528e-09 -3.7539e-12 v Velocity[Z] -0.00013263 0.00013706 8.5508e-10 -1.7165e-12 v ǁVelocityǁ 7.431e-10 0.00014732 1.0372e-05 6.3771e-06 v Pressure -0.00088576 0.018477 0.00099782 2.1768e-20 v k 2.0741e-09 0.0015555 0.0010806 0.0013518 v omega 18.986 1.0313e+05 2669.2 503.36 v TempK 288 341.88 293.37 290.46 v Density 1.205 1.205 1.205 1.205 v TurbVisc 2.4354e-14 9.7885e-05 6.2588e-05 8.0759e-05 v CourantNb 2.051e-09 0.00023062 1.4117e-05 7.7316e-06 v FourierNb 0.12033 0.6281 0.19913 0.16966 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9368 4.9368 0.00048046 -4.6154e-07 v volume_forces[Z] -4.9368 4.9368 -0.00048032 5.5532e-07 v ǁvolume_forcesǁ 2.6676e-08 4.9381 0.48716 0.22186 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.58 290.61 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.016477 5.7955e-05 3.258e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.12033 0.6281 0.19914 0.16967 INSTANT 0.505575000E+00 TIME STEP NUMBER 525 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10396E-04 0.24755E-02 Friction velocity uk : 0.10397E-04 0.24755E-02 Dimensionless distance yplus : 0.69233E-04 0.16469E-01 Friction thermal sca. tstar : -0.64715E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.48625E-04 0.11567E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10396E-04 0.24755E-02 Friction velocity uk : 0.10397E-04 0.24755E-02 Dimensionless distance yplus : 0.69233E-04 0.16469E-01 Friction thermal sca. tstar : -0.64715E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.48625E-04 0.11567E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34251E-08 3 0.21173E-06 0.36148E-12 0.12058E+01 c Velocity[X] 0.19616E-31 c Velocity[Y] 0.18074E-12 c Velocity[Z] 0.18075E-12 c Pressure 0.13407E-13 20 0.91283E-08 0.10474E-06 0.15387E+01 c k 0.47873E-06 2 0.58839E-07 0.68978E-08 0.18986E+01 c omega 0.13153E+02 1 0.24438E-08 0.73977E+00 0.44777E-02 c TempK 0.94556E+02 1 0.15248E-06 0.35584E-01 0.20920E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.1259e-13 9.3523e-14 -1.1531e-17 -2.9597e-18 v Velocity[Y] -0.00013697 0.00013255 -1.0519e-09 -3.7491e-12 v Velocity[Z] -0.00013254 0.00013698 8.538e-10 -1.7229e-12 v ǁVelocityǁ 7.4805e-10 0.00014722 1.0373e-05 6.3821e-06 v Pressure -0.00088745 0.018495 0.00099904 6.8637e-21 v k 2.064e-09 0.0015526 0.0010785 0.0013493 v omega 18.957 1.0313e+05 2669.2 503.34 v TempK 288 341.88 293.37 290.47 v Density 1.205 1.205 1.205 1.205 v TurbVisc 2.4235e-14 9.7871e-05 6.256e-05 8.0728e-05 v CourantNb 2.0497e-09 0.00023044 1.4114e-05 7.7335e-06 v FourierNb 0.12024 0.6281 0.19907 0.1696 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9369 4.9369 0.00048075 -4.62e-07 v volume_forces[Z] -4.9369 4.9369 -0.0004806 5.5583e-07 v ǁvolume_forcesǁ 2.6863e-08 4.9382 0.48744 0.22208 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.59 290.61 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.016469 5.7934e-05 3.2567e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.12024 0.6281 0.19908 0.16961 INSTANT 0.506538000E+00 TIME STEP NUMBER 526 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10432E-04 0.24744E-02 Friction velocity uk : 0.10433E-04 0.24743E-02 Dimensionless distance yplus : 0.69473E-04 0.16462E-01 Friction thermal sca. tstar : -0.50433E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.48794E-04 0.11562E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10432E-04 0.24744E-02 Friction velocity uk : 0.10433E-04 0.24743E-02 Dimensionless distance yplus : 0.69473E-04 0.16462E-01 Friction thermal sca. tstar : -0.50433E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.48794E-04 0.11562E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34253E-08 3 0.21150E-06 0.36056E-12 0.12045E+01 c Velocity[X] 0.19515E-31 c Velocity[Y] 0.18028E-12 c Velocity[Z] 0.18029E-12 c Pressure 0.13373E-13 20 0.91047E-08 0.10447E-06 0.15356E+01 c k 0.47788E-06 2 0.58690E-07 0.68525E-08 0.18958E+01 c omega 0.13153E+02 1 0.24350E-08 0.73527E+00 0.44641E-02 c TempK 0.94557E+02 1 0.15208E-06 0.35483E-01 0.20890E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.1249e-13 9.3444e-14 -1.1521e-17 -2.9573e-18 v Velocity[Y] -0.00013689 0.00013246 -1.0511e-09 -3.7403e-12 v Velocity[Z] -0.00013245 0.0001369 8.5251e-10 -1.7244e-12 v ǁVelocityǁ 7.5297e-10 0.00014712 1.0374e-05 6.3872e-06 v Pressure -0.00088914 0.018512 0.0010003 2.3925e-20 v k 2.0539e-09 0.0015498 0.0010764 0.0013468 v omega 18.929 1.0313e+05 2669.2 503.31 v TempK 288 341.88 293.38 290.47 v Density 1.205 1.205 1.205 1.205 v TurbVisc 2.4116e-14 9.7856e-05 6.2533e-05 8.0698e-05 v CourantNb 2.0484e-09 0.00023026 1.411e-05 7.7353e-06 v FourierNb 0.12014 0.6281 0.19901 0.16955 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.937 4.937 0.00048103 -4.6246e-07 v volume_forces[Z] -4.937 4.937 -0.00048089 5.5635e-07 v ǁvolume_forcesǁ 2.7042e-08 4.9383 0.48772 0.22229 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.59 290.61 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.016462 5.7913e-05 3.2554e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.12015 0.6281 0.19902 0.16955 INSTANT 0.507501000E+00 TIME STEP NUMBER 527 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10467E-04 0.24733E-02 Friction velocity uk : 0.10469E-04 0.24732E-02 Dimensionless distance yplus : 0.69712E-04 0.16455E-01 Friction thermal sca. tstar : -0.42724E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.48961E-04 0.11557E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10467E-04 0.24733E-02 Friction velocity uk : 0.10469E-04 0.24732E-02 Dimensionless distance yplus : 0.69712E-04 0.16455E-01 Friction thermal sca. tstar : -0.42724E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.48961E-04 0.11557E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34255E-08 3 0.21048E-06 0.35965E-12 0.12032E+01 c Velocity[X] 0.19412E-31 c Velocity[Y] 0.17982E-12 c Velocity[Z] 0.17983E-12 c Pressure 0.13332E-13 20 0.90866E-08 0.10414E-06 0.15326E+01 c k 0.47703E-06 2 0.58542E-07 0.68076E-08 0.18929E+01 c omega 0.13153E+02 1 0.24262E-08 0.73080E+00 0.44505E-02 c TempK 0.94557E+02 1 0.15167E-06 0.35383E-01 0.20860E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.1239e-13 9.3364e-14 -1.1512e-17 -2.955e-18 v Velocity[Y] -0.00013681 0.00013237 -1.0502e-09 -3.7317e-12 v Velocity[Z] -0.00013236 0.00013681 8.5121e-10 -1.7263e-12 v ǁVelocityǁ 7.579e-10 0.00014702 1.0376e-05 6.3922e-06 v Pressure -0.00089084 0.01853 0.0010015 5.5008e-20 v k 2.0439e-09 0.001547 0.0010744 0.0013443 v omega 18.901 1.0313e+05 2669.2 503.28 v TempK 288 341.88 293.38 290.47 v Density 1.205 1.205 1.205 1.205 v TurbVisc 2.3998e-14 9.7841e-05 6.2506e-05 8.0668e-05 v CourantNb 2.0471e-09 0.00023008 1.4107e-05 7.7372e-06 v FourierNb 0.12005 0.6281 0.19894 0.16949 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9371 4.9371 0.00048131 -4.6291e-07 v volume_forces[Z] -4.9371 4.9371 -0.00048117 5.5687e-07 v ǁvolume_forcesǁ 2.722e-08 4.9384 0.48801 0.2225 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.59 290.61 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.016455 5.7892e-05 3.2541e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.12006 0.6281 0.19896 0.1695 INSTANT 0.508464000E+00 TIME STEP NUMBER 528 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10503E-04 0.24722E-02 Friction velocity uk : 0.10505E-04 0.24721E-02 Dimensionless distance yplus : 0.69949E-04 0.16447E-01 Friction thermal sca. tstar : -0.37720E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.49128E-04 0.11551E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10503E-04 0.24722E-02 Friction velocity uk : 0.10505E-04 0.24721E-02 Dimensionless distance yplus : 0.69949E-04 0.16447E-01 Friction thermal sca. tstar : -0.37720E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.49128E-04 0.11551E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34258E-08 3 0.20984E-06 0.35875E-12 0.12019E+01 c Velocity[X] 0.19309E-31 c Velocity[Y] 0.17937E-12 c Velocity[Z] 0.17938E-12 c Pressure 0.13289E-13 20 0.90656E-08 0.10381E-06 0.15295E+01 c k 0.47618E-06 2 0.58394E-07 0.67630E-08 0.18901E+01 c omega 0.13153E+02 1 0.24174E-08 0.72637E+00 0.44370E-02 c TempK 0.94558E+02 1 0.15127E-06 0.35284E-01 0.20831E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.1229e-13 9.3285e-14 -1.1502e-17 -2.9526e-18 v Velocity[Y] -0.00013673 0.00013229 -1.0493e-09 -3.7234e-12 v Velocity[Z] -0.00013228 0.00013673 8.4991e-10 -1.7285e-12 v ǁVelocityǁ 7.6283e-10 0.00014693 1.0377e-05 6.3972e-06 v Pressure -0.00089253 0.018547 0.0010027 8.8248e-22 v k 2.0339e-09 0.0015442 0.0010723 0.0013418 v omega 18.872 1.0313e+05 2669.2 503.26 v TempK 288 341.89 293.38 290.47 v Density 1.205 1.205 1.205 1.205 v TurbVisc 2.3881e-14 9.7826e-05 6.2479e-05 8.0638e-05 v CourantNb 2.0457e-09 0.0002299 1.4103e-05 7.7391e-06 v FourierNb 0.11996 0.6281 0.19888 0.16943 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9371 4.9372 0.0004816 -4.6337e-07 v volume_forces[Z] -4.9371 4.9372 -0.00048145 5.5738e-07 v ǁvolume_forcesǁ 2.7398e-08 4.9385 0.48829 0.22272 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.6 290.62 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.016447 5.787e-05 3.2528e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.11996 0.6281 0.1989 0.16944 INSTANT 0.509427000E+00 TIME STEP NUMBER 529 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10539E-04 0.24711E-02 Friction velocity uk : 0.10540E-04 0.24710E-02 Dimensionless distance yplus : 0.70186E-04 0.16440E-01 Friction thermal sca. tstar : -0.34137E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.49294E-04 0.11546E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10539E-04 0.24711E-02 Friction velocity uk : 0.10540E-04 0.24710E-02 Dimensionless distance yplus : 0.70186E-04 0.16440E-01 Friction thermal sca. tstar : -0.34137E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.49294E-04 0.11546E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34260E-08 3 0.20925E-06 0.35785E-12 0.12007E+01 c Velocity[X] 0.19206E-31 c Velocity[Y] 0.17892E-12 c Velocity[Z] 0.17893E-12 c Pressure 0.13253E-13 20 0.90467E-08 0.10352E-06 0.15265E+01 c k 0.47534E-06 2 0.58246E-07 0.67188E-08 0.18873E+01 c omega 0.13153E+02 1 0.24087E-08 0.72197E+00 0.44235E-02 c TempK 0.94558E+02 1 0.15087E-06 0.35185E-01 0.20801E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.1219e-13 9.3205e-14 -1.1492e-17 -2.9502e-18 v Velocity[Y] -0.00013665 0.0001322 -1.0484e-09 -3.715e-12 v Velocity[Z] -0.00013219 0.00013665 8.486e-10 -1.7305e-12 v ǁVelocityǁ 7.6776e-10 0.00014683 1.0378e-05 6.4023e-06 v Pressure -0.00089422 0.018565 0.0010039 3.9613e-20 v k 2.024e-09 0.0015414 0.0010702 0.0013394 v omega 18.844 1.0313e+05 2669.1 503.23 v TempK 288 341.89 293.39 290.48 v Density 1.205 1.205 1.205 1.205 v TurbVisc 2.3765e-14 9.7811e-05 6.2451e-05 8.0608e-05 v CourantNb 2.0443e-09 0.00022972 1.41e-05 7.741e-06 v FourierNb 0.11987 0.6281 0.19882 0.16938 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9372 4.9373 0.00048188 -4.6383e-07 v volume_forces[Z] -4.9372 4.9373 -0.00048174 5.5789e-07 v ǁvolume_forcesǁ 2.7576e-08 4.9386 0.48857 0.22293 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.6 290.62 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.01644 5.7849e-05 3.2515e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.11987 0.6281 0.19884 0.16938 INSTANT 0.510390000E+00 TIME STEP NUMBER 530 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10574E-04 0.24700E-02 Friction velocity uk : 0.10576E-04 0.24699E-02 Dimensionless distance yplus : 0.70422E-04 0.16432E-01 Friction thermal sca. tstar : -0.31408E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.49460E-04 0.11541E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10574E-04 0.24700E-02 Friction velocity uk : 0.10576E-04 0.24699E-02 Dimensionless distance yplus : 0.70422E-04 0.16432E-01 Friction thermal sca. tstar : -0.31408E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.49460E-04 0.11541E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34263E-08 3 0.20867E-06 0.35696E-12 0.11994E+01 c Velocity[X] 0.19103E-31 c Velocity[Y] 0.17847E-12 c Velocity[Z] 0.17848E-12 c Pressure 0.13228E-13 20 0.90270E-08 0.10332E-06 0.15235E+01 c k 0.47450E-06 2 0.58099E-07 0.66749E-08 0.18845E+01 c omega 0.13153E+02 1 0.24000E-08 0.71761E+00 0.44101E-02 c TempK 0.94559E+02 1 0.15047E-06 0.35087E-01 0.20772E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.1209e-13 9.3127e-14 -1.1482e-17 -2.9479e-18 v Velocity[Y] -0.00013657 0.00013211 -1.0476e-09 -3.7065e-12 v Velocity[Z] -0.0001321 0.00013657 8.4728e-10 -1.7323e-12 v ǁVelocityǁ 7.727e-10 0.00014673 1.0379e-05 6.4073e-06 v Pressure -0.00089591 0.018582 0.0010052 2.9416e-22 v k 2.0142e-09 0.0015386 0.0010682 0.0013369 v omega 18.816 1.0313e+05 2669.1 503.21 v TempK 288 341.89 293.39 290.48 v Density 1.205 1.205 1.205 1.205 v TurbVisc 2.3649e-14 9.7797e-05 6.2424e-05 8.0578e-05 v CourantNb 2.0428e-09 0.00022954 1.4096e-05 7.743e-06 v FourierNb 0.11978 0.6281 0.19876 0.16932 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9373 4.9374 0.00048216 -4.6428e-07 v volume_forces[Z] -4.9373 4.9374 -0.00048202 5.584e-07 v ǁvolume_forcesǁ 2.7755e-08 4.9387 0.48886 0.22314 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.6 290.62 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.016432 5.7827e-05 3.2502e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.11978 0.6281 0.19877 0.16933 INSTANT 0.511353000E+00 TIME STEP NUMBER 531 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10610E-04 0.24689E-02 Friction velocity uk : 0.10611E-04 0.24688E-02 Dimensionless distance yplus : 0.70658E-04 0.16425E-01 Friction thermal sca. tstar : -0.29240E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.49626E-04 0.11536E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10610E-04 0.24689E-02 Friction velocity uk : 0.10611E-04 0.24688E-02 Dimensionless distance yplus : 0.70658E-04 0.16425E-01 Friction thermal sca. tstar : -0.29240E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.49626E-04 0.11536E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34265E-08 3 0.20809E-06 0.35607E-12 0.11982E+01 c Velocity[X] 0.19002E-31 c Velocity[Y] 0.17803E-12 c Velocity[Z] 0.17804E-12 c Pressure 0.13190E-13 20 0.90110E-08 0.10302E-06 0.15205E+01 c k 0.47366E-06 2 0.57953E-07 0.66314E-08 0.18817E+01 c omega 0.13153E+02 1 0.23914E-08 0.71327E+00 0.43968E-02 c TempK 0.94560E+02 1 0.15007E-06 0.34989E-01 0.20743E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.1199e-13 9.3048e-14 -1.1473e-17 -2.9456e-18 v Velocity[Y] -0.00013649 0.00013203 -1.0467e-09 -3.6983e-12 v Velocity[Z] -0.00013202 0.0001365 8.4596e-10 -1.7343e-12 v ǁVelocityǁ 7.7765e-10 0.00014664 1.0381e-05 6.4124e-06 v Pressure -0.00089761 0.0186 0.0010064 1.8238e-20 v k 2.0044e-09 0.0015358 0.0010661 0.0013345 v omega 18.788 1.0313e+05 2669.1 503.18 v TempK 288 341.89 293.39 290.48 v Density 1.205 1.205 1.205 1.205 v TurbVisc 2.3534e-14 9.7782e-05 6.2397e-05 8.0548e-05 v CourantNb 2.0414e-09 0.00022936 1.4093e-05 7.7449e-06 v FourierNb 0.11969 0.6281 0.1987 0.16926 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9374 4.9374 0.00048245 -4.6473e-07 v volume_forces[Z] -4.9374 4.9374 -0.0004823 5.5891e-07 v ǁvolume_forcesǁ 2.7933e-08 4.9388 0.48914 0.22335 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.61 290.62 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.016425 5.7806e-05 3.2489e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.11969 0.6281 0.19871 0.16927 INSTANT 0.512316000E+00 TIME STEP NUMBER 532 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10645E-04 0.24678E-02 Friction velocity uk : 0.10646E-04 0.24677E-02 Dimensionless distance yplus : 0.70893E-04 0.16418E-01 Friction thermal sca. tstar : -0.27464E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.49791E-04 0.11531E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10645E-04 0.24678E-02 Friction velocity uk : 0.10646E-04 0.24677E-02 Dimensionless distance yplus : 0.70893E-04 0.16418E-01 Friction thermal sca. tstar : -0.27464E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.49791E-04 0.11531E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34268E-08 3 0.20752E-06 0.35519E-12 0.11969E+01 c Velocity[X] 0.18901E-31 c Velocity[Y] 0.17759E-12 c Velocity[Z] 0.17760E-12 c Pressure 0.13156E-13 20 0.89899E-08 0.10276E-06 0.15175E+01 c k 0.47282E-06 2 0.57808E-07 0.65883E-08 0.18789E+01 c omega 0.13153E+02 1 0.23828E-08 0.70897E+00 0.43835E-02 c TempK 0.94560E+02 1 0.14968E-06 0.34891E-01 0.20714E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.1189e-13 9.2969e-14 -1.1463e-17 -2.9432e-18 v Velocity[Y] -0.00013641 0.00013194 -1.0457e-09 -3.6898e-12 v Velocity[Z] -0.00013193 0.00013642 8.4462e-10 -1.7364e-12 v ǁVelocityǁ 7.8261e-10 0.00014654 1.0382e-05 6.4175e-06 v Pressure -0.0008993 0.018617 0.0010076 -3.8437e-20 v k 1.9947e-09 0.0015331 0.0010641 0.001332 v omega 18.761 1.0313e+05 2669.1 503.16 v TempK 288 341.89 293.39 290.48 v Density 1.205 1.205 1.205 1.205 v TurbVisc 2.342e-14 9.7767e-05 6.237e-05 8.0518e-05 v CourantNb 2.0427e-09 0.00022918 1.409e-05 7.7469e-06 v FourierNb 0.1196 0.6281 0.19864 0.16921 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9375 4.9375 0.00048273 -4.6518e-07 v volume_forces[Z] -4.9375 4.9375 -0.00048258 5.5942e-07 v ǁvolume_forcesǁ 2.8112e-08 4.9389 0.48942 0.22356 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.61 290.63 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.016418 5.7784e-05 3.2476e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.1196 0.6281 0.19865 0.16921 INSTANT 0.513279000E+00 TIME STEP NUMBER 533 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10680E-04 0.24667E-02 Friction velocity uk : 0.10682E-04 0.24666E-02 Dimensionless distance yplus : 0.71128E-04 0.16410E-01 Friction thermal sca. tstar : -0.25973E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.49956E-04 0.11526E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10680E-04 0.24667E-02 Friction velocity uk : 0.10682E-04 0.24666E-02 Dimensionless distance yplus : 0.71128E-04 0.16410E-01 Friction thermal sca. tstar : -0.25973E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.49956E-04 0.11526E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34271E-08 3 0.20694E-06 0.35432E-12 0.11957E+01 c Velocity[X] 0.18801E-31 c Velocity[Y] 0.17716E-12 c Velocity[Z] 0.17717E-12 c Pressure 0.13112E-13 20 0.89722E-08 0.10241E-06 0.15146E+01 c k 0.47199E-06 2 0.57663E-07 0.65454E-08 0.18761E+01 c omega 0.13153E+02 1 0.23742E-08 0.70470E+00 0.43703E-02 c TempK 0.94561E+02 1 0.14929E-06 0.34794E-01 0.20685E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.1179e-13 9.2891e-14 -1.1453e-17 -2.9409e-18 v Velocity[Y] -0.00013633 0.00013186 -1.0448e-09 -3.6814e-12 v Velocity[Z] -0.00013184 0.00013634 8.4329e-10 -1.7383e-12 v ǁVelocityǁ 7.8757e-10 0.00014645 1.0384e-05 6.4226e-06 v Pressure -0.00090099 0.018635 0.0010088 4.5398e-20 v k 1.9851e-09 0.0015303 0.0010621 0.0013296 v omega 18.733 1.0313e+05 2669.1 503.13 v TempK 288 341.89 293.4 290.48 v Density 1.205 1.205 1.205 1.205 v TurbVisc 2.3307e-14 9.7753e-05 6.2343e-05 8.0488e-05 v CourantNb 2.0463e-09 0.000229 1.4086e-05 7.7488e-06 v FourierNb 0.1195 0.6281 0.19858 0.16915 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9376 4.9376 0.00048301 -4.6564e-07 v volume_forces[Z] -4.9376 4.9376 -0.00048287 5.5993e-07 v ǁvolume_forcesǁ 2.8291e-08 4.9389 0.4897 0.22377 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.61 290.63 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.01641 5.7763e-05 3.2463e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.11951 0.6281 0.19859 0.16916 INSTANT 0.514242000E+00 TIME STEP NUMBER 534 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+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-04 0.24656E-02 Friction velocity uk : 0.10717E-04 0.24655E-02 Dimensionless distance yplus : 0.71362E-04 0.16403E-01 Friction thermal sca. tstar : -0.24700E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.50120E-04 0.11521E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+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-04 0.24656E-02 Friction velocity uk : 0.10717E-04 0.24655E-02 Dimensionless distance yplus : 0.71362E-04 0.16403E-01 Friction thermal sca. tstar : -0.24700E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.50120E-04 0.11521E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34273E-08 3 0.20636E-06 0.35346E-12 0.11944E+01 c Velocity[X] 0.18701E-31 c Velocity[Y] 0.17672E-12 c Velocity[Z] 0.17673E-12 c Pressure 0.13077E-13 20 0.89537E-08 0.10214E-06 0.15116E+01 c k 0.47116E-06 2 0.57519E-07 0.65030E-08 0.18734E+01 c omega 0.13153E+02 1 0.23657E-08 0.70046E+00 0.43571E-02 c TempK 0.94561E+02 1 0.14889E-06 0.34697E-01 0.20656E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.117e-13 9.2813e-14 -1.1444e-17 -2.9386e-18 v Velocity[Y] -0.00013625 0.00013177 -1.0439e-09 -3.6732e-12 v Velocity[Z] -0.00013176 0.00013626 8.4194e-10 -1.7402e-12 v ǁVelocityǁ 7.9254e-10 0.00014635 1.0385e-05 6.4277e-06 v Pressure -0.00090268 0.018652 0.00101 8.0207e-20 v k 1.9755e-09 0.0015276 0.00106 0.0013272 v omega 18.705 1.0313e+05 2669 503.11 v TempK 288 341.89 293.4 290.49 v Density 1.205 1.205 1.205 1.205 v TurbVisc 2.3195e-14 9.7738e-05 6.2316e-05 8.0458e-05 v CourantNb 2.05e-09 0.00022882 1.4083e-05 7.7508e-06 v FourierNb 0.11941 0.6281 0.19852 0.16909 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9377 4.9377 0.00048329 -4.6609e-07 v volume_forces[Z] -4.9377 4.9377 -0.00048315 5.6044e-07 v ǁvolume_forcesǁ 2.8471e-08 4.939 0.48998 0.22398 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.62 290.63 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.016403 5.7741e-05 3.245e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.11942 0.6281 0.19853 0.1691 INSTANT 0.515205000E+00 TIME STEP NUMBER 535 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10751E-04 0.24645E-02 Friction velocity uk : 0.10752E-04 0.24644E-02 Dimensionless distance yplus : 0.71596E-04 0.16396E-01 Friction thermal sca. tstar : -0.23595E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.50285E-04 0.11515E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10751E-04 0.24645E-02 Friction velocity uk : 0.10752E-04 0.24644E-02 Dimensionless distance yplus : 0.71596E-04 0.16396E-01 Friction thermal sca. tstar : -0.23595E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.50285E-04 0.11515E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34276E-08 3 0.22883E-06 0.35259E-12 0.11932E+01 c Velocity[X] 0.18602E-31 c Velocity[Y] 0.17629E-12 c Velocity[Z] 0.17630E-12 c Pressure 0.13042E-13 23 0.89204E-08 0.10186E-06 0.15086E+01 c k 0.47033E-06 2 0.57376E-07 0.64608E-08 0.18706E+01 c omega 0.13153E+02 1 0.23573E-08 0.69626E+00 0.43440E-02 c TempK 0.94562E+02 1 0.14850E-06 0.34601E-01 0.20627E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.116e-13 9.2735e-14 -1.1434e-17 -2.9363e-18 v Velocity[Y] -0.00013618 0.00013169 -1.0429e-09 -3.6209e-12 v Velocity[Z] -0.00013167 0.00013618 8.4075e-10 -1.5898e-12 v ǁVelocityǁ 7.9744e-10 0.00014626 1.0386e-05 6.4328e-06 v Pressure -0.00090438 0.018669 0.0010112 -4.785e-20 v k 1.966e-09 0.0015248 0.001058 0.0013248 v omega 18.678 1.0313e+05 2669 503.08 v TempK 288 341.89 293.4 290.49 v Density 1.205 1.205 1.205 1.205 v TurbVisc 2.3083e-14 9.7724e-05 6.2289e-05 8.0429e-05 v CourantNb 2.0535e-09 0.00022865 1.408e-05 7.7529e-06 v FourierNb 0.11932 0.6281 0.19846 0.16904 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9378 4.9378 0.00048357 -4.6653e-07 v volume_forces[Z] -4.9378 4.9378 -0.00048343 5.6094e-07 v ǁvolume_forcesǁ 2.865e-08 4.9391 0.49026 0.2242 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.62 290.63 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.016396 5.772e-05 3.2437e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.11933 0.6281 0.19847 0.16905 INSTANT 0.516168000E+00 TIME STEP NUMBER 536 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10785E-04 0.24634E-02 Friction velocity uk : 0.10786E-04 0.24633E-02 Dimensionless distance yplus : 0.71826E-04 0.16389E-01 Friction thermal sca. tstar : -0.22625E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.50446E-04 0.11510E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10785E-04 0.24634E-02 Friction velocity uk : 0.10786E-04 0.24633E-02 Dimensionless distance yplus : 0.71826E-04 0.16389E-01 Friction thermal sca. tstar : -0.22625E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.50446E-04 0.11510E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34279E-08 3 0.20520E-06 0.35174E-12 0.11920E+01 c Velocity[X] 0.18503E-31 c Velocity[Y] 0.17587E-12 c Velocity[Z] 0.17587E-12 c Pressure 0.13012E-13 23 0.89055E-08 0.10162E-06 0.15057E+01 c k 0.46951E-06 2 0.57233E-07 0.64191E-08 0.18678E+01 c omega 0.13153E+02 1 0.23488E-08 0.69208E+00 0.43310E-02 c TempK 0.94563E+02 1 0.14812E-06 0.34505E-01 0.20598E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.115e-13 9.2657e-14 -1.1425e-17 -2.934e-18 v Velocity[Y] -0.0001361 0.0001316 -1.042e-09 -3.611e-12 v Velocity[Z] -0.00013159 0.0001361 8.3938e-10 -1.5913e-12 v ǁVelocityǁ 8.0247e-10 0.00014616 1.0388e-05 6.438e-06 v Pressure -0.00090607 0.018687 0.0010124 1.2355e-20 v k 1.9566e-09 0.0015221 0.001056 0.0013224 v omega 18.65 1.0313e+05 2669 503.06 v TempK 288 341.89 293.41 290.49 v Density 1.205 1.205 1.205 1.205 v TurbVisc 2.2972e-14 9.7709e-05 6.2263e-05 8.0399e-05 v CourantNb 2.0572e-09 0.00022847 1.4076e-05 7.7549e-06 v FourierNb 0.11923 0.6281 0.1984 0.16898 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9379 4.9379 0.00048385 -4.6698e-07 v volume_forces[Z] -4.9379 4.9379 -0.00048371 5.6145e-07 v ǁvolume_forcesǁ 2.8827e-08 4.9392 0.49054 0.22441 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.62 290.63 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.016389 5.7699e-05 3.2424e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.11924 0.6281 0.19841 0.16899 INSTANT 0.517131000E+00 TIME STEP NUMBER 537 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10820E-04 0.24623E-02 Friction velocity uk : 0.10822E-04 0.24622E-02 Dimensionless distance yplus : 0.72061E-04 0.16381E-01 Friction thermal sca. tstar : -0.21763E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.50611E-04 0.11505E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10820E-04 0.24623E-02 Friction velocity uk : 0.10822E-04 0.24622E-02 Dimensionless distance yplus : 0.72061E-04 0.16381E-01 Friction thermal sca. tstar : -0.21763E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.50611E-04 0.11505E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34282E-08 3 0.20464E-06 0.35089E-12 0.11907E+01 c Velocity[X] 0.18406E-31 c Velocity[Y] 0.17544E-12 c Velocity[Z] 0.17545E-12 c Pressure 0.12976E-13 23 0.88812E-08 0.10134E-06 0.15028E+01 c k 0.46868E-06 2 0.57091E-07 0.63776E-08 0.18651E+01 c omega 0.13153E+02 1 0.23405E-08 0.68794E+00 0.43180E-02 c TempK 0.94563E+02 1 0.14773E-06 0.34410E-01 0.20569E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.114e-13 9.258e-14 -1.1415e-17 -2.9317e-18 v Velocity[Y] -0.00013602 0.00013152 -1.041e-09 -3.6041e-12 v Velocity[Z] -0.0001315 0.00013602 8.3802e-10 -1.5938e-12 v ǁVelocityǁ 8.0749e-10 0.00014607 1.0389e-05 6.4431e-06 v Pressure -0.00090776 0.018704 0.0010137 -6.6578e-20 v k 1.9472e-09 0.0015193 0.001054 0.00132 v omega 18.623 1.0313e+05 2669 503.03 v TempK 288 341.89 293.41 290.49 v Density 1.205 1.205 1.205 1.205 v TurbVisc 2.2861e-14 9.7694e-05 6.2236e-05 8.0369e-05 v CourantNb 2.0608e-09 0.0002283 1.4073e-05 7.7569e-06 v FourierNb 0.11914 0.6281 0.19834 0.16893 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9379 4.938 0.00048413 -4.6742e-07 v volume_forces[Z] -4.9379 4.938 -0.00048399 5.6195e-07 v ǁvolume_forcesǁ 2.9009e-08 4.9393 0.49082 0.22462 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.63 290.64 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.016381 5.7677e-05 3.2411e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.11915 0.6281 0.19835 0.16893 INSTANT 0.518094000E+00 TIME STEP NUMBER 538 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10855E-04 0.24612E-02 Friction velocity uk : 0.10857E-04 0.24612E-02 Dimensionless distance yplus : 0.72294E-04 0.16374E-01 Friction thermal sca. tstar : -0.20992E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.50775E-04 0.11500E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10855E-04 0.24612E-02 Friction velocity uk : 0.10857E-04 0.24612E-02 Dimensionless distance yplus : 0.72294E-04 0.16374E-01 Friction thermal sca. tstar : -0.20992E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.50775E-04 0.11500E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34286E-08 3 0.20407E-06 0.35005E-12 0.11895E+01 c Velocity[X] 0.18310E-31 c Velocity[Y] 0.17502E-12 c Velocity[Z] 0.17503E-12 c Pressure 0.12937E-13 23 0.88675E-08 0.10104E-06 0.14999E+01 c k 0.46786E-06 2 0.56950E-07 0.63365E-08 0.18624E+01 c omega 0.13153E+02 1 0.23321E-08 0.68383E+00 0.43051E-02 c TempK 0.94564E+02 1 0.14734E-06 0.34315E-01 0.20541E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.1131e-13 9.2502e-14 -1.1406e-17 -2.9294e-18 v Velocity[Y] -0.00013594 0.00013143 -1.0401e-09 -3.5961e-12 v Velocity[Z] -0.00013142 0.00013595 8.3664e-10 -1.5958e-12 v ǁVelocityǁ 8.1251e-10 0.00014598 1.0391e-05 6.4483e-06 v Pressure -0.00090945 0.018722 0.0010149 9.4278e-20 v k 1.9379e-09 0.0015166 0.001052 0.0013176 v omega 18.595 1.0313e+05 2669 503.01 v TempK 288 341.9 293.41 290.5 v Density 1.205 1.205 1.205 1.205 v TurbVisc 2.2752e-14 9.768e-05 6.2209e-05 8.034e-05 v CourantNb 2.0645e-09 0.00022812 1.407e-05 7.759e-06 v FourierNb 0.11905 0.6281 0.19827 0.16887 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.938 4.9381 0.00048441 -4.6787e-07 v volume_forces[Z] -4.938 4.9381 -0.00048427 5.6245e-07 v ǁvolume_forcesǁ 2.9191e-08 4.9394 0.4911 0.22483 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.63 290.64 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.016374 5.7656e-05 3.2398e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.11905 0.6281 0.19829 0.16888 INSTANT 0.519057000E+00 TIME STEP NUMBER 539 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10890E-04 0.24601E-02 Friction velocity uk : 0.10892E-04 0.24601E-02 Dimensionless distance yplus : 0.72528E-04 0.16367E-01 Friction thermal sca. tstar : -0.20296E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.50939E-04 0.11495E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10890E-04 0.24601E-02 Friction velocity uk : 0.10892E-04 0.24601E-02 Dimensionless distance yplus : 0.72528E-04 0.16367E-01 Friction thermal sca. tstar : -0.20296E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.50939E-04 0.11495E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34289E-08 3 0.20351E-06 0.34921E-12 0.11883E+01 c Velocity[X] 0.18214E-31 c Velocity[Y] 0.17460E-12 c Velocity[Z] 0.17461E-12 c Pressure 0.12904E-13 23 0.88494E-08 0.10077E-06 0.14970E+01 c k 0.46705E-06 2 0.56809E-07 0.62957E-08 0.18596E+01 c omega 0.13153E+02 1 0.23238E-08 0.67975E+00 0.42922E-02 c TempK 0.94565E+02 1 0.14696E-06 0.34220E-01 0.20512E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.1121e-13 9.2425e-14 -1.1396e-17 -2.9272e-18 v Velocity[Y] -0.00013586 0.00013135 -1.0391e-09 -3.5881e-12 v Velocity[Z] -0.00013134 0.00013587 8.3526e-10 -1.598e-12 v ǁVelocityǁ 8.1754e-10 0.00014588 1.0392e-05 6.4534e-06 v Pressure -0.00091115 0.018739 0.0010161 9.1287e-20 v k 1.9286e-09 0.0015139 0.00105 0.0013152 v omega 18.568 1.0313e+05 2668.9 502.98 v TempK 288 341.9 293.42 290.5 v Density 1.205 1.205 1.205 1.205 v TurbVisc 2.2643e-14 9.7665e-05 6.2182e-05 8.031e-05 v CourantNb 2.0681e-09 0.00022795 1.4067e-05 7.7611e-06 v FourierNb 0.11896 0.6281 0.19821 0.16882 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9381 4.9381 0.00048469 -4.6832e-07 v volume_forces[Z] -4.9381 4.9381 -0.00048455 5.6295e-07 v ǁvolume_forcesǁ 2.9372e-08 4.9395 0.49138 0.22504 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.63 290.64 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.016367 5.7635e-05 3.2385e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.11896 0.6281 0.19823 0.16882 INSTANT 0.520020000E+00 TIME STEP NUMBER 540 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10925E-04 0.24591E-02 Friction velocity uk : 0.10927E-04 0.24590E-02 Dimensionless distance yplus : 0.72760E-04 0.16360E-01 Friction thermal sca. tstar : -0.19664E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.51102E-04 0.11490E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10925E-04 0.24591E-02 Friction velocity uk : 0.10927E-04 0.24590E-02 Dimensionless distance yplus : 0.72760E-04 0.16360E-01 Friction thermal sca. tstar : -0.19664E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.51102E-04 0.11490E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34292E-08 3 0.20295E-06 0.34838E-12 0.11871E+01 c Velocity[X] 0.18119E-31 c Velocity[Y] 0.17419E-12 c Velocity[Z] 0.17419E-12 c Pressure 0.12870E-13 23 0.88313E-08 0.10051E-06 0.14941E+01 c k 0.46623E-06 2 0.56669E-07 0.62552E-08 0.18569E+01 c omega 0.13153E+02 1 0.23156E-08 0.67569E+00 0.42794E-02 c TempK 0.94565E+02 1 0.14658E-06 0.34126E-01 0.20484E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.1111e-13 9.2348e-14 -1.1387e-17 -2.9249e-18 v Velocity[Y] -0.00013579 0.00013126 -1.0382e-09 -3.5801e-12 v Velocity[Z] -0.00013125 0.00013579 8.3387e-10 -1.6003e-12 v ǁVelocityǁ 8.2257e-10 0.00014579 1.0394e-05 6.4586e-06 v Pressure -0.00091284 0.018756 0.0010173 -7.2363e-20 v k 1.9194e-09 0.0015112 0.001048 0.0013128 v omega 18.541 1.0313e+05 2668.9 502.96 v TempK 288 341.9 293.42 290.5 v Density 1.205 1.205 1.205 1.205 v TurbVisc 2.2534e-14 9.7651e-05 6.2156e-05 8.028e-05 v CourantNb 2.0718e-09 0.00022777 1.4064e-05 7.7632e-06 v FourierNb 0.11887 0.6281 0.19816 0.16876 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9382 4.9382 0.00048497 -4.6876e-07 v volume_forces[Z] -4.9382 4.9382 -0.00048483 5.6345e-07 v ǁvolume_forcesǁ 2.9554e-08 4.9395 0.49166 0.22525 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.63 290.64 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.01636 5.7613e-05 3.2373e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.11887 0.6281 0.19817 0.16877 INSTANT 0.520983000E+00 TIME STEP NUMBER 541 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10960E-04 0.24580E-02 Friction velocity uk : 0.10962E-04 0.24579E-02 Dimensionless distance yplus : 0.72992E-04 0.16353E-01 Friction thermal sca. tstar : -0.19087E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.51265E-04 0.11485E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10960E-04 0.24580E-02 Friction velocity uk : 0.10962E-04 0.24579E-02 Dimensionless distance yplus : 0.72992E-04 0.16353E-01 Friction thermal sca. tstar : -0.19087E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.51265E-04 0.11485E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34295E-08 3 0.20240E-06 0.34755E-12 0.11859E+01 c Velocity[X] 0.18024E-31 c Velocity[Y] 0.17377E-12 c Velocity[Z] 0.17378E-12 c Pressure 0.12858E-13 23 0.88176E-08 0.10041E-06 0.14912E+01 c k 0.46542E-06 2 0.56529E-07 0.62150E-08 0.18542E+01 c omega 0.13153E+02 1 0.23073E-08 0.67167E+00 0.42666E-02 c TempK 0.94566E+02 1 0.14620E-06 0.34032E-01 0.20456E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.1102e-13 9.2271e-14 -1.1378e-17 -2.9226e-18 v Velocity[Y] -0.00013571 0.00013118 -1.0372e-09 -3.5724e-12 v Velocity[Z] -0.00013117 0.00013571 8.3247e-10 -1.6025e-12 v ǁVelocityǁ 8.2761e-10 0.0001457 1.0395e-05 6.4638e-06 v Pressure -0.00091453 0.018773 0.0010185 3.4318e-21 v k 1.9103e-09 0.0015085 0.001046 0.0013104 v omega 18.514 1.0313e+05 2668.9 502.94 v TempK 288 341.9 293.42 290.5 v Density 1.205 1.205 1.205 1.205 v TurbVisc 2.2427e-14 9.7636e-05 6.2129e-05 8.0251e-05 v CourantNb 2.0754e-09 0.0002276 1.4061e-05 7.7653e-06 v FourierNb 0.11878 0.6281 0.1981 0.1687 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9383 4.9383 0.00048525 -4.692e-07 v volume_forces[Z] -4.9383 4.9383 -0.0004851 5.6395e-07 v ǁvolume_forcesǁ 2.9736e-08 4.9396 0.49194 0.22546 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.64 290.65 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.016353 5.7592e-05 3.236e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.11879 0.6281 0.19811 0.16871 INSTANT 0.521946000E+00 TIME STEP NUMBER 542 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10995E-04 0.24569E-02 Friction velocity uk : 0.10996E-04 0.24568E-02 Dimensionless distance yplus : 0.73224E-04 0.16346E-01 Friction thermal sca. tstar : -0.18557E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.51428E-04 0.11480E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10995E-04 0.24569E-02 Friction velocity uk : 0.10996E-04 0.24568E-02 Dimensionless distance yplus : 0.73224E-04 0.16346E-01 Friction thermal sca. tstar : -0.18557E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.51428E-04 0.11480E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34299E-08 3 0.20182E-06 0.34674E-12 0.11847E+01 c Velocity[X] 0.15605E-31 c Velocity[Y] 0.17337E-12 c Velocity[Z] 0.17337E-12 c Pressure 0.12802E-13 20 0.99969E-07 0.99969E-07 0.14882E+01 c k 0.46461E-06 2 0.56390E-07 0.61752E-08 0.18515E+01 c omega 0.13153E+02 1 0.22992E-08 0.66768E+00 0.42539E-02 c TempK 0.94566E+02 1 0.14582E-06 0.33939E-01 0.20427E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.1092e-13 9.2205e-14 -1.1389e-17 -2.9252e-18 v Velocity[Y] -0.00013563 0.0001311 -1.0367e-09 -4.1031e-12 v Velocity[Z] -0.00013108 0.00013564 8.312e-10 -1.2915e-12 v ǁVelocityǁ 8.2761e-10 0.0001456 1.0397e-05 6.469e-06 v Pressure -0.00091623 0.018791 0.0010197 -3.0543e-20 v k 1.9012e-09 0.0015058 0.0010441 0.0013081 v omega 18.487 1.0313e+05 2668.9 502.91 v TempK 288 341.9 293.43 290.51 v Density 1.205 1.205 1.205 1.205 v TurbVisc 2.232e-14 9.7622e-05 6.2103e-05 8.0221e-05 v CourantNb 2.0854e-09 0.00022742 1.4057e-05 7.7674e-06 v FourierNb 0.11869 0.6281 0.19804 0.16865 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9384 4.9384 0.00048553 -4.6964e-07 v volume_forces[Z] -4.9384 4.9384 -0.00048538 5.6445e-07 v ǁvolume_forcesǁ 2.9918e-08 4.9397 0.49222 0.22567 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.64 290.65 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.016346 5.7571e-05 3.2347e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.1187 0.6281 0.19805 0.16866 INSTANT 0.522909000E+00 TIME STEP NUMBER 543 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10993E-04 0.24558E-02 Friction velocity uk : 0.10994E-04 0.24558E-02 Dimensionless distance yplus : 0.73207E-04 0.16338E-01 Friction thermal sca. tstar : -0.18067E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.51416E-04 0.11475E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10993E-04 0.24558E-02 Friction velocity uk : 0.10994E-04 0.24558E-02 Dimensionless distance yplus : 0.73207E-04 0.16338E-01 Friction thermal sca. tstar : -0.18067E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.51416E-04 0.11475E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34302E-08 3 0.23472E-06 0.34592E-12 0.11835E+01 c Velocity[X] 0.20098E-31 c Velocity[Y] 0.17295E-12 c Velocity[Z] 0.17296E-12 c Pressure 0.14745E-13 23 0.95085E-08 0.11514E-06 0.14857E+01 c k 0.46380E-06 2 0.56252E-07 0.61356E-08 0.18488E+01 c omega 0.13153E+02 1 0.22910E-08 0.66371E+00 0.42413E-02 c TempK 0.94567E+02 1 0.14544E-06 0.33846E-01 0.20399E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.1083e-13 9.212e-14 -1.1363e-17 -2.919e-18 v Velocity[Y] -0.00013556 0.00013101 -1.0352e-09 -3.5601e-12 v Velocity[Z] -0.000131 0.00013556 8.2967e-10 -1.5914e-12 v ǁVelocityǁ 8.3817e-10 0.00014551 1.0398e-05 6.4742e-06 v Pressure -0.00091792 0.018808 0.0010209 -1.1766e-20 v k 1.8921e-09 0.0015032 0.0010421 0.0013057 v omega 18.46 1.0313e+05 2668.9 502.89 v TempK 288 341.9 293.43 290.51 v Density 1.205 1.205 1.205 1.205 v TurbVisc 2.2214e-14 9.7608e-05 6.2076e-05 8.0192e-05 v CourantNb 2.0826e-09 0.00022725 1.4054e-05 7.7695e-06 v FourierNb 0.1186 0.6281 0.19798 0.16859 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9385 4.9385 0.00048581 -4.7007e-07 v volume_forces[Z] -4.9385 4.9385 -0.00048566 5.6497e-07 v ǁvolume_forcesǁ 2.9918e-08 4.9398 0.49249 0.22588 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.64 290.65 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.016338 5.755e-05 3.2334e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.11861 0.6281 0.19799 0.1686 INSTANT 0.523872000E+00 TIME STEP NUMBER 544 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11067E-04 0.24548E-02 Friction velocity uk : 0.11068E-04 0.24547E-02 Dimensionless distance yplus : 0.73704E-04 0.16331E-01 Friction thermal sca. tstar : -0.17615E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.51765E-04 0.11470E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11067E-04 0.24548E-02 Friction velocity uk : 0.11068E-04 0.24547E-02 Dimensionless distance yplus : 0.73704E-04 0.16331E-01 Friction thermal sca. tstar : -0.17615E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.51765E-04 0.11470E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34306E-08 3 0.18851E-06 0.34511E-12 0.11823E+01 c Velocity[X] 0.15826E-31 c Velocity[Y] 0.17255E-12 c Velocity[Z] 0.17256E-12 c Pressure 0.12121E-13 20 0.94649E-07 0.94649E-07 0.14824E+01 c k 0.46300E-06 2 0.56114E-07 0.60964E-08 0.18461E+01 c omega 0.13153E+02 1 0.22829E-08 0.65978E+00 0.42287E-02 c TempK 0.94568E+02 1 0.14507E-06 0.33754E-01 0.20371E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.1073e-13 9.2052e-14 -1.1371e-17 -2.9209e-18 v Velocity[Y] -0.00013548 0.00013093 -1.0347e-09 -4.0911e-12 v Velocity[Z] -0.00013092 0.00013548 8.2836e-10 -1.3053e-12 v ǁVelocityǁ 8.3784e-10 0.00014542 1.04e-05 6.4795e-06 v Pressure -0.00091961 0.018825 0.0010221 3.1965e-20 v k 1.8832e-09 0.0015006 0.0010401 0.0013034 v omega 18.433 1.0313e+05 2668.8 502.86 v TempK 288 341.9 293.43 290.51 v Density 1.205 1.205 1.205 1.205 v TurbVisc 2.2108e-14 9.7593e-05 6.205e-05 8.0163e-05 v CourantNb 2.0927e-09 0.00022708 1.4051e-05 7.7716e-06 v FourierNb 0.11851 0.6281 0.19792 0.16854 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9386 4.9386 0.00048608 -4.7053e-07 v volume_forces[Z] -4.9386 4.9386 -0.00048594 5.6544e-07 v ǁvolume_forcesǁ 3.03e-08 4.9399 0.49277 0.22608 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.65 290.65 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.016331 5.7529e-05 3.2321e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.11852 0.6281 0.19793 0.16855 INSTANT 0.524835000E+00 TIME STEP NUMBER 545 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11063E-04 0.24537E-02 Friction velocity uk : 0.11064E-04 0.24536E-02 Dimensionless distance yplus : 0.73675E-04 0.16324E-01 Friction thermal sca. tstar : -0.17193E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.51745E-04 0.11465E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11063E-04 0.24537E-02 Friction velocity uk : 0.11064E-04 0.24536E-02 Dimensionless distance yplus : 0.73675E-04 0.16324E-01 Friction thermal sca. tstar : -0.17193E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.51745E-04 0.11465E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34310E-08 3 0.22876E-06 0.34430E-12 0.11811E+01 c Velocity[X] 0.19858E-31 c Velocity[Y] 0.17215E-12 c Velocity[Z] 0.17216E-12 c Pressure 0.14424E-13 23 0.93712E-08 0.11263E-06 0.14800E+01 c k 0.46220E-06 2 0.55977E-07 0.60575E-08 0.18434E+01 c omega 0.13153E+02 1 0.22749E-08 0.65588E+00 0.42162E-02 c TempK 0.94568E+02 1 0.14469E-06 0.33662E-01 0.20343E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.1063e-13 9.1968e-14 -1.1345e-17 -2.9146e-18 v Velocity[Y] -0.0001354 0.00013085 -1.0332e-09 -3.544e-12 v Velocity[Z] -0.00013084 0.00013541 8.2682e-10 -1.5963e-12 v ǁVelocityǁ 8.4836e-10 0.00014533 1.0402e-05 6.4847e-06 v Pressure -0.0009213 0.018842 0.0010233 -1.5002e-20 v k 1.8743e-09 0.001498 0.0010382 0.001301 v omega 18.406 1.0313e+05 2668.8 502.84 v TempK 288 341.9 293.44 290.51 v Density 1.205 1.205 1.205 1.205 v TurbVisc 2.2004e-14 9.7579e-05 6.2023e-05 8.0133e-05 v CourantNb 2.0898e-09 0.00022691 1.4048e-05 7.7738e-06 v FourierNb 0.11842 0.6281 0.19786 0.16848 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9386 4.9387 0.00048636 -4.7096e-07 v volume_forces[Z] -4.9386 4.9387 -0.00048621 5.6596e-07 v ǁvolume_forcesǁ 3.0288e-08 4.94 0.49305 0.22629 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.65 290.66 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.016324 5.7508e-05 3.2309e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.11843 0.6281 0.19787 0.16849 INSTANT 0.525798000E+00 TIME STEP NUMBER 546 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11137E-04 0.24526E-02 Friction velocity uk : 0.11138E-04 0.24526E-02 Dimensionless distance yplus : 0.74166E-04 0.16317E-01 Friction thermal sca. tstar : -0.16800E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.52090E-04 0.11460E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11137E-04 0.24526E-02 Friction velocity uk : 0.11138E-04 0.24526E-02 Dimensionless distance yplus : 0.74166E-04 0.16317E-01 Friction thermal sca. tstar : -0.16800E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.52090E-04 0.11460E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34314E-08 3 0.18747E-06 0.34350E-12 0.11800E+01 c Velocity[X] 0.15680E-31 c Velocity[Y] 0.17175E-12 c Velocity[Z] 0.17175E-12 c Pressure 0.11983E-13 20 0.93568E-07 0.93568E-07 0.14767E+01 c k 0.46140E-06 2 0.55841E-07 0.60189E-08 0.18408E+01 c omega 0.13153E+02 1 0.22669E-08 0.65200E+00 0.42037E-02 c TempK 0.94569E+02 1 0.14432E-06 0.33570E-01 0.20316E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.1054e-13 9.1901e-14 -1.1353e-17 -2.9164e-18 v Velocity[Y] -0.00013533 0.00013077 -1.0327e-09 -4.0744e-12 v Velocity[Z] -0.00013075 0.00013533 8.255e-10 -1.3097e-12 v ǁVelocityǁ 8.4802e-10 0.00014523 1.0403e-05 6.4899e-06 v Pressure -0.00092299 0.01886 0.0010245 6.8343e-20 v k 1.8654e-09 0.0014954 0.0010362 0.0012987 v omega 18.379 1.0313e+05 2668.8 502.82 v TempK 288 341.9 293.44 290.52 v Density 1.205 1.205 1.205 1.205 v TurbVisc 2.1899e-14 9.7564e-05 6.1997e-05 8.0104e-05 v CourantNb 2.1e-09 0.00022674 1.4045e-05 7.776e-06 v FourierNb 0.11834 0.6281 0.1978 0.16843 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9387 4.9387 0.00048664 -4.714e-07 v volume_forces[Z] -4.9387 4.9387 -0.00048649 5.6643e-07 v ǁvolume_forcesǁ 3.0668e-08 4.9401 0.49332 0.2265 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.65 290.66 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.016317 5.7487e-05 3.2296e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.11834 0.6281 0.19781 0.16844 INSTANT 0.526761000E+00 TIME STEP NUMBER 547 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11132E-04 0.24516E-02 Friction velocity uk : 0.11134E-04 0.24515E-02 Dimensionless distance yplus : 0.74138E-04 0.16310E-01 Friction thermal sca. tstar : -0.16431E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.52070E-04 0.11455E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11132E-04 0.24516E-02 Friction velocity uk : 0.11134E-04 0.24515E-02 Dimensionless distance yplus : 0.74138E-04 0.16310E-01 Friction thermal sca. tstar : -0.16431E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.52070E-04 0.11455E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34317E-08 3 0.22743E-06 0.34270E-12 0.11788E+01 c Velocity[X] 0.19665E-31 c Velocity[Y] 0.17135E-12 c Velocity[Z] 0.17136E-12 c Pressure 0.14299E-13 23 0.93184E-08 0.11165E-06 0.14743E+01 c k 0.46060E-06 2 0.55705E-07 0.59806E-08 0.18381E+01 c omega 0.13153E+02 1 0.22589E-08 0.64815E+00 0.41913E-02 c TempK 0.94569E+02 1 0.14395E-06 0.33479E-01 0.20288E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.1044e-13 9.1816e-14 -1.1326e-17 -2.9102e-18 v Velocity[Y] -0.00013525 0.00013068 -1.0312e-09 -3.5284e-12 v Velocity[Z] -0.00013067 0.00013525 8.2395e-10 -1.6005e-12 v ǁVelocityǁ 8.5853e-10 0.00014514 1.0405e-05 6.4952e-06 v Pressure -0.00092469 0.018877 0.0010257 -7.5403e-20 v k 1.8566e-09 0.0014929 0.0010343 0.0012964 v omega 18.353 1.0313e+05 2668.8 502.79 v TempK 288 341.9 293.44 290.52 v Density 1.205 1.205 1.205 1.205 v TurbVisc 2.1796e-14 9.755e-05 6.1971e-05 8.0075e-05 v CourantNb 2.0971e-09 0.00022657 1.4042e-05 7.7781e-06 v FourierNb 0.11825 0.6281 0.19774 0.16837 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9388 4.9388 0.00048691 -4.7183e-07 v volume_forces[Z] -4.9388 4.9388 -0.00048677 5.6694e-07 v ǁvolume_forcesǁ 3.0656e-08 4.9401 0.4936 0.22671 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.66 290.66 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.01631 5.7466e-05 3.2283e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.11825 0.6281 0.19775 0.16838 INSTANT 0.527724000E+00 TIME STEP NUMBER 548 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11206E-04 0.24505E-02 Friction velocity uk : 0.11207E-04 0.24504E-02 Dimensionless distance yplus : 0.74626E-04 0.16303E-01 Friction thermal sca. tstar : -0.16086E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.52412E-04 0.11450E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11206E-04 0.24505E-02 Friction velocity uk : 0.11207E-04 0.24504E-02 Dimensionless distance yplus : 0.74626E-04 0.16303E-01 Friction thermal sca. tstar : -0.16086E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.52412E-04 0.11450E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34321E-08 3 0.18638E-06 0.34191E-12 0.11776E+01 c Velocity[X] 0.15523E-31 c Velocity[Y] 0.17095E-12 c Velocity[Z] 0.17096E-12 c Pressure 0.11920E-13 20 0.93067E-07 0.93067E-07 0.14711E+01 c k 0.45980E-06 2 0.55569E-07 0.59426E-08 0.18354E+01 c omega 0.13153E+02 1 0.22509E-08 0.64433E+00 0.41789E-02 c TempK 0.94570E+02 1 0.14358E-06 0.33388E-01 0.20260E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.1035e-13 9.175e-14 -1.1334e-17 -2.912e-18 v Velocity[Y] -0.00013518 0.0001306 -1.0306e-09 -4.058e-12 v Velocity[Z] -0.00013059 0.00013518 8.2262e-10 -1.314e-12 v ǁVelocityǁ 8.5822e-10 0.00014505 1.0407e-05 6.5005e-06 v Pressure -0.00092638 0.018894 0.0010269 -1.2149e-19 v k 1.8479e-09 0.0014903 0.0010324 0.0012941 v omega 18.326 1.0313e+05 2668.8 502.77 v TempK 288 341.9 293.44 290.52 v Density 1.205 1.205 1.205 1.205 v TurbVisc 2.1693e-14 9.7536e-05 6.1945e-05 8.0046e-05 v CourantNb 2.1072e-09 0.00022639 1.4039e-05 7.7803e-06 v FourierNb 0.11816 0.6281 0.19768 0.16832 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9389 4.9389 0.00048719 -4.7228e-07 v volume_forces[Z] -4.9389 4.9389 -0.00048704 5.6741e-07 v ǁvolume_forcesǁ 3.1036e-08 4.9402 0.49387 0.22692 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.66 290.66 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.016303 5.7445e-05 3.227e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.11816 0.6281 0.1977 0.16833 INSTANT 0.528687000E+00 TIME STEP NUMBER 549 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11202E-04 0.24495E-02 Friction velocity uk : 0.11203E-04 0.24494E-02 Dimensionless distance yplus : 0.74598E-04 0.16296E-01 Friction thermal sca. tstar : -0.15760E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.52393E-04 0.11445E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11202E-04 0.24495E-02 Friction velocity uk : 0.11203E-04 0.24494E-02 Dimensionless distance yplus : 0.74598E-04 0.16296E-01 Friction thermal sca. tstar : -0.15760E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.52393E-04 0.11445E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34325E-08 3 0.22616E-06 0.34112E-12 0.11764E+01 c Velocity[X] 0.19464E-31 c Velocity[Y] 0.17056E-12 c Velocity[Z] 0.17057E-12 c Pressure 0.14223E-13 23 0.92811E-08 0.11105E-06 0.14687E+01 c k 0.45901E-06 2 0.55435E-07 0.59049E-08 0.18328E+01 c omega 0.13153E+02 1 0.22430E-08 0.64054E+00 0.41666E-02 c TempK 0.94571E+02 1 0.14322E-06 0.33298E-01 0.20232E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.1026e-13 9.1666e-14 -1.1308e-17 -2.9058e-18 v Velocity[Y] -0.0001351 0.00013052 -1.0291e-09 -3.5127e-12 v Velocity[Z] -0.00013051 0.0001351 8.2106e-10 -1.6048e-12 v ǁVelocityǁ 8.6875e-10 0.00014496 1.0408e-05 6.5057e-06 v Pressure -0.00092807 0.018911 0.0010281 3.2357e-21 v k 1.8392e-09 0.0014877 0.0010304 0.0012917 v omega 18.3 1.0313e+05 2668.7 502.74 v TempK 288 341.91 293.45 290.52 v Density 1.205 1.205 1.205 1.205 v TurbVisc 2.1591e-14 9.7522e-05 6.1918e-05 8.0017e-05 v CourantNb 2.1043e-09 0.00022622 1.4037e-05 7.7825e-06 v FourierNb 0.11807 0.6281 0.19762 0.16826 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.939 4.939 0.00048746 -4.727e-07 v volume_forces[Z] -4.939 4.939 -0.00048732 5.6792e-07 v ǁvolume_forcesǁ 3.1025e-08 4.9403 0.49415 0.22713 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.66 290.67 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.016296 5.7424e-05 3.2258e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.11807 0.6281 0.19764 0.16827 INSTANT 0.529650000E+00 TIME STEP NUMBER 550 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11275E-04 0.24484E-02 Friction velocity uk : 0.11276E-04 0.24483E-02 Dimensionless distance yplus : 0.75084E-04 0.16289E-01 Friction thermal sca. tstar : -0.15658E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.52734E-04 0.11440E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11275E-04 0.24484E-02 Friction velocity uk : 0.11276E-04 0.24483E-02 Dimensionless distance yplus : 0.75084E-04 0.16289E-01 Friction thermal sca. tstar : -0.15658E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.52734E-04 0.11440E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34329E-08 3 0.18535E-06 0.34034E-12 0.11753E+01 c Velocity[X] 0.15365E-31 c Velocity[Y] 0.17017E-12 c Velocity[Z] 0.17017E-12 c Pressure 0.11855E-13 20 0.92556E-07 0.92556E-07 0.14655E+01 c k 0.45822E-06 2 0.55301E-07 0.58675E-08 0.18302E+01 c omega 0.13153E+02 1 0.22352E-08 0.63677E+00 0.41543E-02 c TempK 0.94571E+02 1 0.14285E-06 0.33208E-01 0.20205E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.1016e-13 9.1599e-14 -1.1316e-17 -2.9076e-18 v Velocity[Y] -0.00013503 0.00013044 -1.0285e-09 -4.0416e-12 v Velocity[Z] -0.00013043 0.00013503 8.1971e-10 -1.3182e-12 v ǁVelocityǁ 8.6846e-10 0.00014487 1.041e-05 6.511e-06 v Pressure -0.00092976 0.018928 0.0010293 4.1084e-20 v k 1.8305e-09 0.0014852 0.0010285 0.0012894 v omega 18.273 1.0313e+05 2668.7 502.72 v TempK 288 341.91 293.45 290.52 v Density 1.205 1.205 1.205 1.205 v TurbVisc 2.1489e-14 9.7507e-05 6.1892e-05 7.9987e-05 v CourantNb 2.1145e-09 0.00022605 1.4034e-05 7.7847e-06 v FourierNb 0.11798 0.6281 0.19756 0.16821 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9391 4.9391 0.00048774 -4.7315e-07 v volume_forces[Z] -4.9391 4.9391 -0.00048759 5.6839e-07 v ǁvolume_forcesǁ 3.1405e-08 4.9404 0.49442 0.22733 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.67 290.67 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.016289 5.7403e-05 3.2245e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.11798 0.6281 0.19758 0.16822 INSTANT 0.530613000E+00 TIME STEP NUMBER 551 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11271E-04 0.24474E-02 Friction velocity uk : 0.11272E-04 0.24473E-02 Dimensionless distance yplus : 0.75058E-04 0.16282E-01 Friction thermal sca. tstar : -0.15854E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.52716E-04 0.11435E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11271E-04 0.24474E-02 Friction velocity uk : 0.11272E-04 0.24473E-02 Dimensionless distance yplus : 0.75058E-04 0.16282E-01 Friction thermal sca. tstar : -0.15854E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.52716E-04 0.11435E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34334E-08 3 0.22493E-06 0.33956E-12 0.11741E+01 c Velocity[X] 0.19265E-31 c Velocity[Y] 0.16978E-12 c Velocity[Z] 0.16979E-12 c Pressure 0.14150E-13 23 0.92465E-08 0.11047E-06 0.14632E+01 c k 0.45744E-06 2 0.55167E-07 0.58304E-08 0.18275E+01 c omega 0.13153E+02 1 0.22274E-08 0.63303E+00 0.41421E-02 c TempK 0.94572E+02 1 0.14249E-06 0.33119E-01 0.20178E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.1007e-13 9.1516e-14 -1.129e-17 -2.9014e-18 v Velocity[Y] -0.00013495 0.00013036 -1.027e-09 -3.4972e-12 v Velocity[Z] -0.00013035 0.00013495 8.1813e-10 -1.6091e-12 v ǁVelocityǁ 8.79e-10 0.00014478 1.0412e-05 6.5163e-06 v Pressure -0.00093145 0.018945 0.0010305 -2.7749e-20 v k 1.822e-09 0.0014826 0.0010266 0.0012872 v omega 18.247 1.0313e+05 2668.7 502.7 v TempK 288 341.91 293.45 290.53 v Density 1.205 1.205 1.205 1.205 v TurbVisc 2.1389e-14 9.7493e-05 6.1866e-05 7.9958e-05 v CourantNb 2.1116e-09 0.00022589 1.4031e-05 7.787e-06 v FourierNb 0.11789 0.6281 0.19751 0.16816 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9391 4.9392 0.00048801 -4.7357e-07 v volume_forces[Z] -4.9391 4.9392 -0.00048787 5.689e-07 v ǁvolume_forcesǁ 3.1395e-08 4.9405 0.4947 0.22754 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.67 290.67 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.016282 5.7382e-05 3.2233e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.1179 0.6281 0.19752 0.16816 INSTANT 0.531576000E+00 TIME STEP NUMBER 552 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11343E-04 0.24463E-02 Friction velocity uk : 0.11344E-04 0.24462E-02 Dimensionless distance yplus : 0.75541E-04 0.16275E-01 Friction thermal sca. tstar : -0.16059E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.53055E-04 0.11430E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11343E-04 0.24463E-02 Friction velocity uk : 0.11344E-04 0.24462E-02 Dimensionless distance yplus : 0.75541E-04 0.16275E-01 Friction thermal sca. tstar : -0.16059E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.53055E-04 0.11430E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34338E-08 3 0.18434E-06 0.33879E-12 0.11729E+01 c Velocity[X] 0.15208E-31 c Velocity[Y] 0.16939E-12 c Velocity[Z] 0.16940E-12 c Pressure 0.11798E-13 20 0.92105E-07 0.92105E-07 0.14599E+01 c k 0.45665E-06 2 0.55034E-07 0.57935E-08 0.18249E+01 c omega 0.13153E+02 1 0.22196E-08 0.62932E+00 0.41299E-02 c TempK 0.94573E+02 1 0.14212E-06 0.33030E-01 0.20150E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.0997e-13 9.145e-14 -1.1297e-17 -2.9031e-18 v Velocity[Y] -0.00013488 0.00013028 -1.0264e-09 -4.0254e-12 v Velocity[Z] -0.00013026 0.00013488 8.1677e-10 -1.3225e-12 v ǁVelocityǁ 8.7874e-10 0.00014469 1.0413e-05 6.5216e-06 v Pressure -0.00093314 0.018962 0.0010317 2.7749e-20 v k 1.8134e-09 0.0014801 0.0010247 0.0012849 v omega 18.221 1.0313e+05 2668.7 502.67 v TempK 288 341.91 293.46 290.53 v Density 1.205 1.205 1.205 1.205 v TurbVisc 2.1288e-14 9.7479e-05 6.184e-05 7.9929e-05 v CourantNb 2.1217e-09 0.00022572 1.4028e-05 7.7892e-06 v FourierNb 0.11781 0.6281 0.19745 0.1681 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9392 4.9393 0.00048829 -4.7402e-07 v volume_forces[Z] -4.9392 4.9393 -0.00048814 5.6937e-07 v ǁvolume_forcesǁ 3.1776e-08 4.9406 0.49497 0.22775 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.67 290.67 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.016275 5.7361e-05 3.222e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.11781 0.6281 0.19746 0.16811 INSTANT 0.532539000E+00 TIME STEP NUMBER 553 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11340E-04 0.24453E-02 Friction velocity uk : 0.11341E-04 0.24452E-02 Dimensionless distance yplus : 0.75517E-04 0.16268E-01 Friction thermal sca. tstar : -0.16271E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.53038E-04 0.11426E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11340E-04 0.24453E-02 Friction velocity uk : 0.11341E-04 0.24452E-02 Dimensionless distance yplus : 0.75517E-04 0.16268E-01 Friction thermal sca. tstar : -0.16271E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.53038E-04 0.11426E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34342E-08 3 0.22369E-06 0.33802E-12 0.11718E+01 c Velocity[X] 0.19068E-31 c Velocity[Y] 0.16900E-12 c Velocity[Z] 0.16901E-12 c Pressure 0.14079E-13 23 0.92114E-08 0.10991E-06 0.14576E+01 c k 0.45587E-06 2 0.54902E-07 0.57570E-08 0.18223E+01 c omega 0.13153E+02 1 0.22118E-08 0.62564E+00 0.41178E-02 c TempK 0.94573E+02 1 0.14176E-06 0.32941E-01 0.20123E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.0988e-13 9.1367e-14 -1.1271e-17 -2.897e-18 v Velocity[Y] -0.0001348 0.0001302 -1.0248e-09 -3.4819e-12 v Velocity[Z] -0.00013018 0.0001348 8.1518e-10 -1.6133e-12 v ǁVelocityǁ 8.893e-10 0.0001446 1.0415e-05 6.5269e-06 v Pressure -0.00093483 0.01898 0.0010329 8.7169e-20 v k 1.805e-09 0.0014776 0.0010228 0.0012826 v omega 18.194 1.0313e+05 2668.7 502.65 v TempK 288 341.91 293.46 290.53 v Density 1.205 1.205 1.205 1.205 v TurbVisc 2.1189e-14 9.7465e-05 6.1814e-05 7.99e-05 v CourantNb 2.1188e-09 0.00022555 1.4025e-05 7.7915e-06 v FourierNb 0.11772 0.6281 0.19739 0.16805 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9393 4.9393 0.00048856 -4.7444e-07 v volume_forces[Z] -4.9393 4.9393 -0.00048842 5.6987e-07 v ǁvolume_forcesǁ 3.1767e-08 4.9406 0.49524 0.22796 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.67 290.67 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.016268 5.734e-05 3.2207e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.11772 0.6281 0.1974 0.16805 INSTANT 0.533502000E+00 TIME STEP NUMBER 554 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11412E-04 0.24442E-02 Friction velocity uk : 0.11413E-04 0.24441E-02 Dimensionless distance yplus : 0.75997E-04 0.16261E-01 Friction thermal sca. tstar : -0.16493E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.53375E-04 0.11421E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11412E-04 0.24442E-02 Friction velocity uk : 0.11413E-04 0.24441E-02 Dimensionless distance yplus : 0.75997E-04 0.16261E-01 Friction thermal sca. tstar : -0.16493E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.53375E-04 0.11421E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34346E-08 3 0.18332E-06 0.33725E-12 0.11706E+01 c Velocity[X] 0.15053E-31 c Velocity[Y] 0.16862E-12 c Velocity[Z] 0.16863E-12 c Pressure 0.11738E-13 20 0.91632E-07 0.91632E-07 0.14544E+01 c k 0.45509E-06 2 0.54770E-07 0.57207E-08 0.18197E+01 c omega 0.13153E+02 1 0.22041E-08 0.62198E+00 0.41058E-02 c TempK 0.94574E+02 1 0.14140E-06 0.32852E-01 0.20096E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.0979e-13 9.1301e-14 -1.1279e-17 -2.8987e-18 v Velocity[Y] -0.00013473 0.00013012 -1.0242e-09 -4.0093e-12 v Velocity[Z] -0.0001301 0.00013473 8.1381e-10 -1.3267e-12 v ǁVelocityǁ 8.8907e-10 0.00014451 1.0417e-05 6.5323e-06 v Pressure -0.00093653 0.018997 0.0010341 -5.0105e-20 v k 1.7966e-09 0.0014751 0.0010209 0.0012803 v omega 18.168 1.0313e+05 2668.7 502.63 v TempK 288 341.91 293.46 290.53 v Density 1.205 1.205 1.205 1.205 v TurbVisc 2.109e-14 9.745e-05 6.1788e-05 7.9871e-05 v CourantNb 2.1289e-09 0.00022538 1.4022e-05 7.7937e-06 v FourierNb 0.11763 0.6281 0.19733 0.16799 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9394 4.9394 0.00048883 -4.7488e-07 v volume_forces[Z] -4.9394 4.9394 -0.00048869 5.7034e-07 v ǁvolume_forcesǁ 3.2148e-08 4.9407 0.49552 0.22816 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.68 290.68 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.016261 5.7319e-05 3.2195e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.11763 0.6281 0.19735 0.168 INSTANT 0.534465000E+00 TIME STEP NUMBER 555 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11408E-04 0.24432E-02 Friction velocity uk : 0.11409E-04 0.24431E-02 Dimensionless distance yplus : 0.75974E-04 0.16254E-01 Friction thermal sca. tstar : -0.16723E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.53359E-04 0.11416E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11408E-04 0.24432E-02 Friction velocity uk : 0.11409E-04 0.24431E-02 Dimensionless distance yplus : 0.75974E-04 0.16254E-01 Friction thermal sca. tstar : -0.16723E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.53359E-04 0.11416E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34351E-08 3 0.22246E-06 0.33649E-12 0.11695E+01 c Velocity[X] 0.18874E-31 c Velocity[Y] 0.16824E-12 c Velocity[Z] 0.16825E-12 c Pressure 0.14007E-13 23 0.91757E-08 0.10934E-06 0.14522E+01 c k 0.45431E-06 2 0.54639E-07 0.56848E-08 0.18171E+01 c omega 0.13153E+02 1 0.21965E-08 0.61835E+00 0.40938E-02 c TempK 0.94574E+02 1 0.14105E-06 0.32765E-01 0.20069E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.097e-13 9.1218e-14 -1.1253e-17 -2.8926e-18 v Velocity[Y] -0.00013465 0.00013004 -1.0227e-09 -3.4665e-12 v Velocity[Z] -0.00013002 0.00013466 8.1221e-10 -1.6176e-12 v ǁVelocityǁ 8.9964e-10 0.00014442 1.0419e-05 6.5376e-06 v Pressure -0.00093822 0.019014 0.0010353 1.5296e-20 v k 1.7882e-09 0.0014725 0.001019 0.001278 v omega 18.142 1.0313e+05 2668.6 502.6 v TempK 288 341.91 293.47 290.54 v Density 1.205 1.205 1.205 1.205 v TurbVisc 2.0991e-14 9.7436e-05 6.1762e-05 7.9843e-05 v CourantNb 2.1261e-09 0.00022521 1.402e-05 7.796e-06 v FourierNb 0.11754 0.6281 0.19728 0.16794 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9395 4.9395 0.00048911 -4.753e-07 v volume_forces[Z] -4.9395 4.9395 -0.00048896 5.7084e-07 v ǁvolume_forcesǁ 3.214e-08 4.9408 0.49579 0.22837 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.68 290.68 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.016254 5.7299e-05 3.2182e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.11754 0.6281 0.19729 0.16795 INSTANT 0.535428000E+00 TIME STEP NUMBER 556 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11480E-04 0.24421E-02 Friction velocity uk : 0.11481E-04 0.24421E-02 Dimensionless distance yplus : 0.76452E-04 0.16247E-01 Friction thermal sca. tstar : -0.16964E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.53695E-04 0.11411E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11480E-04 0.24421E-02 Friction velocity uk : 0.11481E-04 0.24421E-02 Dimensionless distance yplus : 0.76452E-04 0.16247E-01 Friction thermal sca. tstar : -0.16964E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.53695E-04 0.11411E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34355E-08 3 0.18231E-06 0.33574E-12 0.11683E+01 c Velocity[X] 0.14900E-31 c Velocity[Y] 0.16787E-12 c Velocity[Z] 0.16787E-12 c Pressure 0.11673E-13 20 0.91124E-07 0.91124E-07 0.14490E+01 c k 0.45354E-06 2 0.54508E-07 0.56491E-08 0.18145E+01 c omega 0.13153E+02 1 0.21888E-08 0.61475E+00 0.40818E-02 c TempK 0.94575E+02 1 0.14069E-06 0.32677E-01 0.20042E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.096e-13 9.1153e-14 -1.1261e-17 -2.8944e-18 v Velocity[Y] -0.00013458 0.00012996 -1.0221e-09 -3.9933e-12 v Velocity[Z] -0.00012994 0.00013458 8.1082e-10 -1.3309e-12 v ǁVelocityǁ 8.9943e-10 0.00014433 1.0421e-05 6.5429e-06 v Pressure -0.00093991 0.019031 0.0010364 -6.5793e-20 v k 1.7799e-09 0.00147 0.0010171 0.0012758 v omega 18.116 1.0313e+05 2668.6 502.58 v TempK 288 341.91 293.47 290.54 v Density 1.205 1.205 1.205 1.205 v TurbVisc 2.0894e-14 9.7422e-05 6.1737e-05 7.9814e-05 v CourantNb 2.1361e-09 0.00022505 1.4017e-05 7.7983e-06 v FourierNb 0.11745 0.6281 0.19722 0.16789 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9396 4.9396 0.00048938 -4.7574e-07 v volume_forces[Z] -4.9396 4.9396 -0.00048923 5.7131e-07 v ǁvolume_forcesǁ 3.2522e-08 4.9409 0.49606 0.22858 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.68 290.68 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.016247 5.7278e-05 3.2169e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.11746 0.6281 0.19723 0.16789 INSTANT 0.536391000E+00 TIME STEP NUMBER 557 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11477E-04 0.24411E-02 Friction velocity uk : 0.11478E-04 0.24410E-02 Dimensionless distance yplus : 0.76431E-04 0.16240E-01 Friction thermal sca. tstar : -0.17215E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.53680E-04 0.11406E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11477E-04 0.24411E-02 Friction velocity uk : 0.11478E-04 0.24410E-02 Dimensionless distance yplus : 0.76431E-04 0.16240E-01 Friction thermal sca. tstar : -0.17215E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.53680E-04 0.11406E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34360E-08 3 0.22125E-06 0.33498E-12 0.11672E+01 c Velocity[X] 0.18683E-31 c Velocity[Y] 0.16749E-12 c Velocity[Z] 0.16749E-12 c Pressure 0.13944E-13 23 0.91402E-08 0.10885E-06 0.14467E+01 c k 0.45277E-06 2 0.54378E-07 0.56136E-08 0.18119E+01 c omega 0.13153E+02 1 0.21812E-08 0.61117E+00 0.40699E-02 c TempK 0.94576E+02 1 0.14034E-06 0.32590E-01 0.20015E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.0951e-13 9.107e-14 -1.1235e-17 -2.8883e-18 v Velocity[Y] -0.00013451 0.00012988 -1.0205e-09 -3.4512e-12 v Velocity[Z] -0.00012986 0.00013451 8.092e-10 -1.6219e-12 v ǁVelocityǁ 9.1002e-10 0.00014425 1.0422e-05 6.5483e-06 v Pressure -0.0009416 0.019048 0.0010376 -7.3981e-20 v k 1.7716e-09 0.0014675 0.0010153 0.0012735 v omega 18.091 1.0313e+05 2668.6 502.56 v TempK 288 341.91 293.47 290.54 v Density 1.205 1.205 1.205 1.205 v TurbVisc 2.0797e-14 9.7408e-05 6.1711e-05 7.9785e-05 v CourantNb 2.1333e-09 0.00022488 1.4014e-05 7.8006e-06 v FourierNb 0.11737 0.6281 0.19716 0.16783 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9396 4.9397 0.00048965 -4.7616e-07 v volume_forces[Z] -4.9396 4.9397 -0.00048951 5.7181e-07 v ǁvolume_forcesǁ 3.2514e-08 4.941 0.49633 0.22878 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.69 290.68 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.01624 5.7258e-05 3.2157e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.11737 0.6281 0.19717 0.16784 INSTANT 0.537354000E+00 TIME STEP NUMBER 558 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11548E-04 0.24400E-02 Friction velocity uk : 0.11549E-04 0.24400E-02 Dimensionless distance yplus : 0.76906E-04 0.16233E-01 Friction thermal sca. tstar : -0.17478E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.54014E-04 0.11401E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11548E-04 0.24400E-02 Friction velocity uk : 0.11549E-04 0.24400E-02 Dimensionless distance yplus : 0.76906E-04 0.16233E-01 Friction thermal sca. tstar : -0.17478E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.54014E-04 0.11401E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34365E-08 3 0.18131E-06 0.33423E-12 0.11660E+01 c Velocity[X] 0.14749E-31 c Velocity[Y] 0.16711E-12 c Velocity[Z] 0.16712E-12 c Pressure 0.11618E-13 20 0.90688E-07 0.90688E-07 0.14436E+01 c k 0.45200E-06 2 0.54249E-07 0.55785E-08 0.18093E+01 c omega 0.13153E+02 1 0.21737E-08 0.60762E+00 0.40581E-02 c TempK 0.94576E+02 1 0.13998E-06 0.32503E-01 0.19988E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.0942e-13 9.1005e-14 -1.1243e-17 -2.89e-18 v Velocity[Y] -0.00013443 0.0001298 -1.0199e-09 -3.9774e-12 v Velocity[Z] -0.00012978 0.00013444 8.078e-10 -1.3351e-12 v ǁVelocityǁ 9.0983e-10 0.00014416 1.0424e-05 6.5537e-06 v Pressure -0.00094329 0.019065 0.0010388 1.6179e-21 v k 1.7634e-09 0.001465 0.0010134 0.0012713 v omega 18.065 1.0313e+05 2668.6 502.53 v TempK 288 341.91 293.47 290.54 v Density 1.205 1.205 1.205 1.205 v TurbVisc 2.07e-14 9.7394e-05 6.1685e-05 7.9756e-05 v CourantNb 2.1434e-09 0.00022471 1.4011e-05 7.8029e-06 v FourierNb 0.11728 0.6281 0.1971 0.16778 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9397 4.9398 0.00048992 -4.766e-07 v volume_forces[Z] -4.9397 4.9398 -0.00048978 5.7227e-07 v ǁvolume_forcesǁ 3.2897e-08 4.9411 0.4966 0.22899 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.69 290.69 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.016233 5.7237e-05 3.2144e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.11728 0.6281 0.19712 0.16779 INSTANT 0.538317000E+00 TIME STEP NUMBER 559 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11545E-04 0.24390E-02 Friction velocity uk : 0.11546E-04 0.24390E-02 Dimensionless distance yplus : 0.76886E-04 0.16227E-01 Friction thermal sca. tstar : -0.17752E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.54000E-04 0.11396E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11545E-04 0.24390E-02 Friction velocity uk : 0.11546E-04 0.24390E-02 Dimensionless distance yplus : 0.76886E-04 0.16227E-01 Friction thermal sca. tstar : -0.17752E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.54000E-04 0.11396E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34369E-08 3 0.22004E-06 0.33349E-12 0.11649E+01 c Velocity[X] 0.18493E-31 c Velocity[Y] 0.16674E-12 c Velocity[Z] 0.16675E-12 c Pressure 0.13862E-13 23 0.91062E-08 0.10820E-06 0.14413E+01 c k 0.45123E-06 2 0.54120E-07 0.55436E-08 0.18067E+01 c omega 0.13153E+02 1 0.21661E-08 0.60409E+00 0.40463E-02 c TempK 0.94577E+02 1 0.13963E-06 0.32417E-01 0.19961E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.0933e-13 9.0923e-14 -1.1217e-17 -2.884e-18 v Velocity[Y] -0.00013436 0.00012972 -1.0183e-09 -3.4362e-12 v Velocity[Z] -0.0001297 0.00013436 8.0617e-10 -1.626e-12 v ǁVelocityǁ 9.2043e-10 0.00014407 1.0426e-05 6.559e-06 v Pressure -0.00094498 0.019082 0.00104 4.3143e-20 v k 1.7553e-09 0.0014626 0.0010115 0.0012691 v omega 18.039 1.0313e+05 2668.6 502.51 v TempK 288 341.91 293.48 290.55 v Density 1.205 1.205 1.205 1.205 v TurbVisc 2.0604e-14 9.738e-05 6.1659e-05 7.9728e-05 v CourantNb 2.1405e-09 0.00022455 1.4009e-05 7.8053e-06 v FourierNb 0.11719 0.6281 0.19705 0.16772 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9398 4.9398 0.00049019 -4.7701e-07 v volume_forces[Z] -4.9398 4.9398 -0.00049005 5.7277e-07 v ǁvolume_forcesǁ 3.2891e-08 4.9411 0.49687 0.2292 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.69 290.69 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.016227 5.7216e-05 3.2132e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.1172 0.6281 0.19706 0.16773 INSTANT 0.539280000E+00 TIME STEP NUMBER 560 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11616E-04 0.24380E-02 Friction velocity uk : 0.11617E-04 0.24379E-02 Dimensionless distance yplus : 0.77359E-04 0.16220E-01 Friction thermal sca. tstar : -0.18042E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.54332E-04 0.11392E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11616E-04 0.24380E-02 Friction velocity uk : 0.11617E-04 0.24379E-02 Dimensionless distance yplus : 0.77359E-04 0.16220E-01 Friction thermal sca. tstar : -0.18042E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.54332E-04 0.11392E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34374E-08 3 0.18032E-06 0.33275E-12 0.11638E+01 c Velocity[X] 0.14600E-31 c Velocity[Y] 0.16637E-12 c Velocity[Z] 0.16637E-12 c Pressure 0.11559E-13 20 0.90226E-07 0.90226E-07 0.14382E+01 c k 0.45046E-06 2 0.53991E-07 0.55090E-08 0.18042E+01 c omega 0.13153E+02 1 0.21586E-08 0.60059E+00 0.40346E-02 c TempK 0.94577E+02 1 0.13928E-06 0.32330E-01 0.19934E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.0924e-13 9.0858e-14 -1.1225e-17 -2.8857e-18 v Velocity[Y] -0.00013429 0.00012964 -1.0176e-09 -3.9616e-12 v Velocity[Z] -0.00012963 0.00013429 8.0476e-10 -1.3393e-12 v ǁVelocityǁ 9.2028e-10 0.00014398 1.0428e-05 6.5644e-06 v Pressure -0.00094667 0.019099 0.0010412 2.7847e-20 v k 1.7471e-09 0.0014601 0.0010097 0.0012668 v omega 18.013 1.0313e+05 2668.5 502.49 v TempK 288 341.92 293.48 290.55 v Density 1.205 1.205 1.205 1.205 v TurbVisc 2.0509e-14 9.7366e-05 6.1634e-05 7.9699e-05 v CourantNb 2.1506e-09 0.00022438 1.4006e-05 7.8076e-06 v FourierNb 0.11711 0.6281 0.19699 0.16767 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9399 4.9399 0.00049047 -4.7745e-07 v volume_forces[Z] -4.9399 4.9399 -0.00049032 5.7323e-07 v ǁvolume_forcesǁ 3.3274e-08 4.9412 0.49714 0.2294 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.7 290.69 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.01622 5.7195e-05 3.212e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.11711 0.6281 0.197 0.16768 INSTANT 0.540243000E+00 TIME STEP NUMBER 561 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11614E-04 0.24370E-02 Friction velocity uk : 0.11615E-04 0.24369E-02 Dimensionless distance yplus : 0.77341E-04 0.16213E-01 Friction thermal sca. tstar : -0.18344E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.54319E-04 0.11387E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11614E-04 0.24370E-02 Friction velocity uk : 0.11615E-04 0.24369E-02 Dimensionless distance yplus : 0.77341E-04 0.16213E-01 Friction thermal sca. tstar : -0.18344E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.54319E-04 0.11387E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34379E-08 3 0.21884E-06 0.33201E-12 0.11626E+01 c Velocity[X] 0.18307E-31 c Velocity[Y] 0.16600E-12 c Velocity[Z] 0.16601E-12 c Pressure 0.13794E-13 23 0.90715E-08 0.10767E-06 0.14359E+01 c k 0.44970E-06 2 0.53864E-07 0.54746E-08 0.18016E+01 c omega 0.13153E+02 1 0.21512E-08 0.59711E+00 0.40229E-02 c TempK 0.94578E+02 1 0.13893E-06 0.32245E-01 0.19908E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.0915e-13 9.0777e-14 -1.1199e-17 -2.8797e-18 v Velocity[Y] -0.00013421 0.00012956 -1.016e-09 -3.4212e-12 v Velocity[Z] -0.00012955 0.00013422 8.0312e-10 -1.6299e-12 v ǁVelocityǁ 9.3089e-10 0.00014389 1.043e-05 6.5698e-06 v Pressure -0.00094836 0.019116 0.0010424 5.3929e-21 v k 1.7391e-09 0.0014576 0.0010078 0.0012646 v omega 17.988 1.0313e+05 2668.5 502.46 v TempK 288 341.92 293.48 290.55 v Density 1.205 1.205 1.205 1.205 v TurbVisc 2.0414e-14 9.7352e-05 6.1608e-05 7.967e-05 v CourantNb 2.1477e-09 0.00022422 1.4003e-05 7.81e-06 v FourierNb 0.11702 0.6281 0.19693 0.16762 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.94 4.94 0.00049074 -4.7786e-07 v volume_forces[Z] -4.94 4.94 -0.00049059 5.7373e-07 v ǁvolume_forcesǁ 3.3268e-08 4.9413 0.49741 0.22961 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.7 290.69 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.016213 5.7175e-05 3.2107e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.11702 0.6281 0.19695 0.16763 INSTANT 0.541206000E+00 TIME STEP NUMBER 562 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+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-04 0.24359E-02 Friction velocity uk : 0.11685E-04 0.24359E-02 Dimensionless distance yplus : 0.77811E-04 0.16206E-01 Friction thermal sca. tstar : -0.18664E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.54650E-04 0.11382E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+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-04 0.24359E-02 Friction velocity uk : 0.11685E-04 0.24359E-02 Dimensionless distance yplus : 0.77811E-04 0.16206E-01 Friction thermal sca. tstar : -0.18664E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.54650E-04 0.11382E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34384E-08 3 0.17935E-06 0.33127E-12 0.11615E+01 c Velocity[X] 0.14453E-31 c Velocity[Y] 0.16564E-12 c Velocity[Z] 0.16564E-12 c Pressure 0.11533E-13 20 0.90018E-07 0.90018E-07 0.14328E+01 c k 0.44894E-06 2 0.53736E-07 0.54406E-08 0.17991E+01 c omega 0.13153E+02 1 0.21438E-08 0.59366E+00 0.40112E-02 c TempK 0.94579E+02 1 0.13858E-06 0.32160E-01 0.19881E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.0905e-13 9.0712e-14 -1.1207e-17 -2.8814e-18 v Velocity[Y] -0.00013414 0.00012948 -1.0153e-09 -3.9459e-12 v Velocity[Z] -0.00012947 0.00013414 8.0169e-10 -1.3433e-12 v ǁVelocityǁ 9.3076e-10 0.00014381 1.0432e-05 6.5752e-06 v Pressure -0.00095005 0.019132 0.0010435 2.4023e-21 v k 1.7311e-09 0.0014551 0.001006 0.0012624 v omega 17.962 1.0313e+05 2668.5 502.44 v TempK 288 341.92 293.49 290.55 v Density 1.205 1.205 1.205 1.205 v TurbVisc 2.032e-14 9.7338e-05 6.1582e-05 7.9642e-05 v CourantNb 2.1577e-09 0.00022406 1.4001e-05 7.8124e-06 v FourierNb 0.11693 0.6281 0.19688 0.16756 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9401 4.9401 0.00049101 -4.783e-07 v volume_forces[Z] -4.9401 4.9401 -0.00049086 5.7418e-07 v ǁvolume_forcesǁ 3.3652e-08 4.9414 0.49768 0.22981 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.7 290.7 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.016206 5.7154e-05 3.2095e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.11694 0.6281 0.19689 0.16757 INSTANT 0.542169000E+00 TIME STEP NUMBER 563 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11682E-04 0.24349E-02 Friction velocity uk : 0.11683E-04 0.24348E-02 Dimensionless distance yplus : 0.77794E-04 0.16199E-01 Friction thermal sca. tstar : -0.18999E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.54638E-04 0.11377E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11682E-04 0.24349E-02 Friction velocity uk : 0.11683E-04 0.24348E-02 Dimensionless distance yplus : 0.77794E-04 0.16199E-01 Friction thermal sca. tstar : -0.18999E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.54638E-04 0.11377E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34389E-08 3 0.21769E-06 0.33054E-12 0.11604E+01 c Velocity[X] 0.18122E-31 c Velocity[Y] 0.16527E-12 c Velocity[Z] 0.16528E-12 c Pressure 0.13727E-13 23 0.90358E-08 0.10714E-06 0.14306E+01 c k 0.44818E-06 2 0.53610E-07 0.54067E-08 0.17965E+01 c omega 0.13153E+02 1 0.21364E-08 0.59023E+00 0.39996E-02 c TempK 0.94579E+02 1 0.13824E-06 0.32075E-01 0.19855E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.0896e-13 9.0631e-14 -1.1182e-17 -2.8754e-18 v Velocity[Y] -0.00013407 0.0001294 -1.0137e-09 -3.4062e-12 v Velocity[Z] -0.00012939 0.00013407 8.0004e-10 -1.6343e-12 v ǁVelocityǁ 9.4138e-10 0.00014372 1.0434e-05 6.5806e-06 v Pressure -0.00095174 0.019149 0.0010447 4.9762e-20 v k 1.7231e-09 0.0014527 0.0010041 0.0012602 v omega 17.937 1.0313e+05 2668.5 502.42 v TempK 288 341.92 293.49 290.56 v Density 1.205 1.205 1.205 1.205 v TurbVisc 2.0226e-14 9.7324e-05 6.1557e-05 7.9613e-05 v CourantNb 2.1549e-09 0.00022389 1.3998e-05 7.8147e-06 v FourierNb 0.11685 0.6281 0.19682 0.16751 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9401 4.9402 0.00049128 -4.7871e-07 v volume_forces[Z] -4.9401 4.9402 -0.00049113 5.7468e-07 v ǁvolume_forcesǁ 3.3647e-08 4.9415 0.49795 0.23002 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.7 290.7 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.016199 5.7134e-05 3.2082e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.11685 0.6281 0.19683 0.16752 INSTANT 0.543132000E+00 TIME STEP NUMBER 564 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11752E-04 0.24339E-02 Friction velocity uk : 0.11753E-04 0.24338E-02 Dimensionless distance yplus : 0.78262E-04 0.16192E-01 Friction thermal sca. tstar : -0.19355E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.54966E-04 0.11372E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11752E-04 0.24339E-02 Friction velocity uk : 0.11753E-04 0.24338E-02 Dimensionless distance yplus : 0.78262E-04 0.16192E-01 Friction thermal sca. tstar : -0.19355E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.54966E-04 0.11372E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34394E-08 3 0.17836E-06 0.32982E-12 0.11592E+01 c Velocity[X] 0.14308E-31 c Velocity[Y] 0.16491E-12 c Velocity[Z] 0.16491E-12 c Pressure 0.11443E-13 20 0.89309E-07 0.89309E-07 0.14275E+01 c k 0.44742E-06 2 0.53483E-07 0.53732E-08 0.17940E+01 c omega 0.13153E+02 1 0.21290E-08 0.58683E+00 0.39881E-02 c TempK 0.94580E+02 1 0.13789E-06 0.31990E-01 0.19829E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.0887e-13 9.0567e-14 -1.1189e-17 -2.8771e-18 v Velocity[Y] -0.000134 0.00012933 -1.0131e-09 -3.9303e-12 v Velocity[Z] -0.00012931 0.000134 7.986e-10 -1.3476e-12 v ǁVelocityǁ 9.4128e-10 0.00014363 1.0436e-05 6.5861e-06 v Pressure -0.00095343 0.019166 0.0010459 5.5841e-20 v k 1.7152e-09 0.0014502 0.0010023 0.001258 v omega 17.911 1.0313e+05 2668.5 502.4 v TempK 288 341.92 293.49 290.56 v Density 1.205 1.205 1.205 1.205 v TurbVisc 2.0134e-14 9.731e-05 6.1531e-05 7.9585e-05 v CourantNb 2.1649e-09 0.00022373 1.3996e-05 7.8171e-06 v FourierNb 0.11676 0.6281 0.19676 0.16746 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9402 4.9403 0.00049155 -4.7914e-07 v volume_forces[Z] -4.9402 4.9403 -0.0004914 5.7513e-07 v ǁvolume_forcesǁ 3.4031e-08 4.9415 0.49822 0.23022 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.71 290.7 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.016192 5.7113e-05 3.207e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.11676 0.6281 0.19678 0.16747 INSTANT 0.544095000E+00 TIME STEP NUMBER 565 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11750E-04 0.24329E-02 Friction velocity uk : 0.11751E-04 0.24328E-02 Dimensionless distance yplus : 0.78246E-04 0.16186E-01 Friction thermal sca. tstar : -0.19729E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.54955E-04 0.11368E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11750E-04 0.24329E-02 Friction velocity uk : 0.11751E-04 0.24328E-02 Dimensionless distance yplus : 0.78246E-04 0.16186E-01 Friction thermal sca. tstar : -0.19729E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.54955E-04 0.11368E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34399E-08 3 0.21646E-06 0.32909E-12 0.11581E+01 c Velocity[X] 0.17941E-31 c Velocity[Y] 0.16454E-12 c Velocity[Z] 0.16455E-12 c Pressure 0.13653E-13 23 0.90032E-08 0.10656E-06 0.14253E+01 c k 0.44667E-06 2 0.53358E-07 0.53399E-08 0.17915E+01 c omega 0.13153E+02 1 0.21217E-08 0.58345E+00 0.39766E-02 c TempK 0.94580E+02 1 0.13755E-06 0.31906E-01 0.19802E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.0878e-13 9.0486e-14 -1.1164e-17 -2.8711e-18 v Velocity[Y] -0.00013393 0.00012925 -1.0114e-09 -3.3914e-12 v Velocity[Z] -0.00012923 0.00013393 7.9693e-10 -1.6384e-12 v ǁVelocityǁ 9.5192e-10 0.00014355 1.0438e-05 6.5915e-06 v Pressure -0.00095512 0.019183 0.0010471 7.957e-20 v k 1.7074e-09 0.0014478 0.0010005 0.0012558 v omega 17.886 1.0313e+05 2668.4 502.37 v TempK 288 341.92 293.5 290.56 v Density 1.205 1.205 1.205 1.205 v TurbVisc 2.0041e-14 9.7296e-05 6.1506e-05 7.9556e-05 v CourantNb 2.1621e-09 0.00022357 1.3993e-05 7.8195e-06 v FourierNb 0.11667 0.6281 0.19671 0.16741 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9403 4.9403 0.00049181 -4.7955e-07 v volume_forces[Z] -4.9403 4.9403 -0.00049167 5.7563e-07 v ǁvolume_forcesǁ 3.4027e-08 4.9416 0.49849 0.23043 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.71 290.7 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.016186 5.7093e-05 3.2058e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.11668 0.6281 0.19672 0.16741 INSTANT 0.545058000E+00 TIME STEP NUMBER 566 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11820E-04 0.24318E-02 Friction velocity uk : 0.11821E-04 0.24318E-02 Dimensionless distance yplus : 0.78712E-04 0.16179E-01 Friction thermal sca. tstar : -0.20129E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.55282E-04 0.11363E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11820E-04 0.24318E-02 Friction velocity uk : 0.11821E-04 0.24318E-02 Dimensionless distance yplus : 0.78712E-04 0.16179E-01 Friction thermal sca. tstar : -0.20129E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.55282E-04 0.11363E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34405E-08 3 0.17737E-06 0.32837E-12 0.11570E+01 c Velocity[X] 0.14165E-31 c Velocity[Y] 0.16418E-12 c Velocity[Z] 0.16419E-12 c Pressure 0.11382E-13 20 0.88830E-07 0.88830E-07 0.14222E+01 c k 0.44592E-06 2 0.53233E-07 0.53068E-08 0.17890E+01 c omega 0.13153E+02 1 0.21145E-08 0.58010E+00 0.39651E-02 c TempK 0.94581E+02 1 0.13721E-06 0.31822E-01 0.19776E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.0869e-13 9.0422e-14 -1.1172e-17 -2.8728e-18 v Velocity[Y] -0.00013385 0.00012917 -1.0107e-09 -3.9148e-12 v Velocity[Z] -0.00012916 0.00013386 7.9548e-10 -1.3517e-12 v ǁVelocityǁ 9.5184e-10 0.00014346 1.044e-05 6.5969e-06 v Pressure -0.0009568 0.0192 0.0010483 1.912e-20 v k 1.6996e-09 0.0014454 0.00099865 0.0012536 v omega 17.861 1.0313e+05 2668.4 502.35 v TempK 288 341.92 293.5 290.56 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.9949e-14 9.7282e-05 6.148e-05 7.9528e-05 v CourantNb 2.1721e-09 0.0002234 1.399e-05 7.822e-06 v FourierNb 0.11659 0.6281 0.19665 0.16735 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9404 4.9404 0.00049208 -4.7999e-07 v volume_forces[Z] -4.9404 4.9404 -0.00049194 5.7608e-07 v ǁvolume_forcesǁ 3.4412e-08 4.9417 0.49876 0.23063 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.71 290.7 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.016179 5.7073e-05 3.2045e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.11659 0.6281 0.19666 0.16736 INSTANT 0.546021000E+00 TIME STEP NUMBER 567 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11817E-04 0.24308E-02 Friction velocity uk : 0.11818E-04 0.24308E-02 Dimensionless distance yplus : 0.78698E-04 0.16172E-01 Friction thermal sca. tstar : -0.20551E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.55272E-04 0.11358E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11817E-04 0.24308E-02 Friction velocity uk : 0.11818E-04 0.24308E-02 Dimensionless distance yplus : 0.78698E-04 0.16172E-01 Friction thermal sca. tstar : -0.20551E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.55272E-04 0.11358E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34410E-08 3 0.21529E-06 0.32765E-12 0.11559E+01 c Velocity[X] 0.17761E-31 c Velocity[Y] 0.16382E-12 c Velocity[Z] 0.16383E-12 c Pressure 0.13589E-13 23 0.89704E-08 0.10606E-06 0.14201E+01 c k 0.44517E-06 2 0.53108E-07 0.52740E-08 0.17864E+01 c omega 0.13153E+02 1 0.21072E-08 0.57677E+00 0.39537E-02 c TempK 0.94582E+02 1 0.13687E-06 0.31739E-01 0.19750E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.086e-13 9.0342e-14 -1.1146e-17 -2.8669e-18 v Velocity[Y] -0.00013378 0.00012909 -1.0091e-09 -3.3765e-12 v Velocity[Z] -0.00012908 0.00013379 7.938e-10 -1.6425e-12 v ǁVelocityǁ 9.5567e-10 0.00014337 1.0442e-05 6.6024e-06 v Pressure -0.00095849 0.019217 0.0010494 -3.2554e-20 v k 1.6918e-09 0.0014429 0.00099684 0.0012514 v omega 17.836 1.0313e+05 2668.4 502.33 v TempK 288 341.92 293.5 290.56 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.9858e-14 9.7268e-05 6.1455e-05 7.9499e-05 v CourantNb 2.1693e-09 0.00022324 1.3988e-05 7.8244e-06 v FourierNb 0.1165 0.6281 0.19659 0.1673 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9405 4.9405 0.00049235 -4.8039e-07 v volume_forces[Z] -4.9405 4.9405 -0.00049221 5.7657e-07 v ǁvolume_forcesǁ 3.4409e-08 4.9418 0.49903 0.23084 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.72 290.71 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.016172 5.7053e-05 3.2033e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.1165 0.6281 0.19661 0.16731 INSTANT 0.546984000E+00 TIME STEP NUMBER 568 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11887E-04 0.24298E-02 Friction velocity uk : 0.11888E-04 0.24297E-02 Dimensionless distance yplus : 0.79161E-04 0.16165E-01 Friction thermal sca. tstar : -0.21005E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.55598E-04 0.11353E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11887E-04 0.24298E-02 Friction velocity uk : 0.11888E-04 0.24297E-02 Dimensionless distance yplus : 0.79161E-04 0.16165E-01 Friction thermal sca. tstar : -0.21005E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.55598E-04 0.11353E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34415E-08 3 0.17642E-06 0.32694E-12 0.11548E+01 c Velocity[X] 0.14023E-31 c Velocity[Y] 0.16347E-12 c Velocity[Z] 0.16347E-12 c Pressure 0.11348E-13 20 0.88563E-07 0.88563E-07 0.14170E+01 c k 0.44442E-06 2 0.52984E-07 0.52415E-08 0.17839E+01 c omega 0.13153E+02 1 0.21000E-08 0.57346E+00 0.39424E-02 c TempK 0.94582E+02 1 0.13653E-06 0.31656E-01 0.19724E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.0851e-13 9.0278e-14 -1.1154e-17 -2.8686e-18 v Velocity[Y] -0.00013371 0.00012902 -1.0084e-09 -3.8993e-12 v Velocity[Z] -0.000129 0.00013371 7.9234e-10 -1.3557e-12 v ǁVelocityǁ 9.6087e-10 0.00014329 1.0444e-05 6.6078e-06 v Pressure -0.00096018 0.019234 0.0010506 1.613e-20 v k 1.6841e-09 0.0014405 0.00099503 0.0012492 v omega 17.811 1.0313e+05 2668.4 502.3 v TempK 288 341.92 293.5 290.57 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.9767e-14 9.7254e-05 6.143e-05 7.9471e-05 v CourantNb 2.1792e-09 0.00022308 1.3985e-05 7.8268e-06 v FourierNb 0.11642 0.6281 0.19654 0.16725 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9406 4.9406 0.00049262 -4.8082e-07 v volume_forces[Z] -4.9406 4.9406 -0.00049248 5.7702e-07 v ǁvolume_forcesǁ 3.4547e-08 4.9419 0.49929 0.23104 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.72 290.71 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.016165 5.7032e-05 3.2021e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.11642 0.6281 0.19655 0.16725 INSTANT 0.547947000E+00 TIME STEP NUMBER 569 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11885E-04 0.24288E-02 Friction velocity uk : 0.11886E-04 0.24287E-02 Dimensionless distance yplus : 0.79148E-04 0.16159E-01 Friction thermal sca. tstar : -0.21485E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.55588E-04 0.11349E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11885E-04 0.24288E-02 Friction velocity uk : 0.11886E-04 0.24287E-02 Dimensionless distance yplus : 0.79148E-04 0.16159E-01 Friction thermal sca. tstar : -0.21485E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.55588E-04 0.11349E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34421E-08 3 0.21412E-06 0.32623E-12 0.11536E+01 c Velocity[X] 0.17583E-31 c Velocity[Y] 0.16311E-12 c Velocity[Z] 0.16312E-12 c Pressure 0.13516E-13 23 0.89343E-08 0.10548E-06 0.14149E+01 c k 0.44368E-06 2 0.52860E-07 0.52092E-08 0.17814E+01 c omega 0.13153E+02 1 0.20928E-08 0.57018E+00 0.39311E-02 c TempK 0.94583E+02 1 0.13619E-06 0.31573E-01 0.19698E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.0842e-13 9.0198e-14 -1.1129e-17 -2.8627e-18 v Velocity[Y] -0.00013364 0.00012894 -1.0067e-09 -3.362e-12 v Velocity[Z] -0.00012893 0.00013364 7.9064e-10 -1.6465e-12 v ǁVelocityǁ 9.4788e-10 0.0001432 1.0446e-05 6.6133e-06 v Pressure -0.00096187 0.019251 0.0010518 4.3388e-20 v k 1.6764e-09 0.0014381 0.00099322 0.0012471 v omega 17.786 1.0313e+05 2668.4 502.28 v TempK 288 341.92 293.51 290.57 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.9677e-14 9.724e-05 6.1405e-05 7.9443e-05 v CourantNb 2.1765e-09 0.00022292 1.3983e-05 7.8293e-06 v FourierNb 0.11633 0.6281 0.19648 0.16719 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9406 4.9407 0.00049289 -4.8123e-07 v volume_forces[Z] -4.9406 4.9407 -0.00049275 5.7751e-07 v ǁvolume_forcesǁ 3.4736e-08 4.9419 0.49956 0.23125 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.72 290.71 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.016159 5.7012e-05 3.2008e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.11633 0.6281 0.1965 0.1672 INSTANT 0.548910000E+00 TIME STEP NUMBER 570 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11837E-04 0.24278E-02 Friction velocity uk : 0.11838E-04 0.24277E-02 Dimensionless distance yplus : 0.78830E-04 0.16152E-01 Friction thermal sca. tstar : -0.22005E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.55365E-04 0.11344E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11837E-04 0.24278E-02 Friction velocity uk : 0.11838E-04 0.24277E-02 Dimensionless distance yplus : 0.78830E-04 0.16152E-01 Friction thermal sca. tstar : -0.22005E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.55365E-04 0.11344E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34426E-08 3 0.17544E-06 0.32553E-12 0.11525E+01 c Velocity[X] 0.13884E-31 c Velocity[Y] 0.16276E-12 c Velocity[Z] 0.16277E-12 c Pressure 0.11266E-13 20 0.87917E-07 0.87917E-07 0.14118E+01 c k 0.44294E-06 2 0.52737E-07 0.51771E-08 0.17790E+01 c omega 0.13153E+02 1 0.20857E-08 0.56692E+00 0.39198E-02 c TempK 0.94584E+02 1 0.13586E-06 0.31490E-01 0.19672E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.0833e-13 9.0135e-14 -1.1137e-17 -2.8644e-18 v Velocity[Y] -0.00013357 0.00012886 -1.006e-09 -3.884e-12 v Velocity[Z] -0.00012885 0.00013357 7.8916e-10 -1.3597e-12 v ǁVelocityǁ 9.5304e-10 0.00014312 1.0448e-05 6.6188e-06 v Pressure -0.00096356 0.019267 0.001053 1.1619e-20 v k 1.6688e-09 0.0014357 0.00099142 0.0012449 v omega 17.761 1.0313e+05 2668.4 502.26 v TempK 288 341.92 293.51 290.57 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.9588e-14 9.7226e-05 6.1379e-05 7.9415e-05 v CourantNb 2.1864e-09 0.00022276 1.3981e-05 7.8317e-06 v FourierNb 0.11624 0.6281 0.19643 0.16714 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9407 4.9407 0.00049316 -4.8166e-07 v volume_forces[Z] -4.9407 4.9407 -0.00049301 5.7796e-07 v ǁvolume_forcesǁ 3.4266e-08 4.942 0.49983 0.23145 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.73 290.71 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.016152 5.6991e-05 3.1996e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.11625 0.6281 0.19644 0.16715 INSTANT 0.549873000E+00 TIME STEP NUMBER 571 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11870E-04 0.24268E-02 Friction velocity uk : 0.11871E-04 0.24267E-02 Dimensionless distance yplus : 0.79045E-04 0.16145E-01 Friction thermal sca. tstar : -0.22559E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.55516E-04 0.11339E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11870E-04 0.24268E-02 Friction velocity uk : 0.11871E-04 0.24267E-02 Dimensionless distance yplus : 0.79045E-04 0.16145E-01 Friction thermal sca. tstar : -0.22559E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.55516E-04 0.11339E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34432E-08 3 0.21295E-06 0.32482E-12 0.11514E+01 c Velocity[X] 0.17408E-31 c Velocity[Y] 0.16241E-12 c Velocity[Z] 0.16242E-12 c Pressure 0.13448E-13 23 0.89015E-08 0.10494E-06 0.14097E+01 c k 0.44220E-06 2 0.52615E-07 0.51453E-08 0.17765E+01 c omega 0.13153E+02 1 0.20786E-08 0.56368E+00 0.39086E-02 c TempK 0.94584E+02 1 0.13552E-06 0.31408E-01 0.19646E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.0825e-13 9.0055e-14 -1.1111e-17 -2.8585e-18 v Velocity[Y] -0.0001335 0.00012879 -1.0043e-09 -3.3474e-12 v Velocity[Z] -0.00012877 0.0001335 7.8746e-10 -1.6505e-12 v ǁVelocityǁ 9.4004e-10 0.00014303 1.045e-05 6.6242e-06 v Pressure -0.00096525 0.019284 0.0010541 1.5688e-21 v k 1.6612e-09 0.0014333 0.00098963 0.0012428 v omega 17.736 1.0313e+05 2668.3 502.24 v TempK 288 341.92 293.51 290.57 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.9499e-14 9.7212e-05 6.1354e-05 7.9386e-05 v CourantNb 2.1836e-09 0.0002226 1.3978e-05 7.8342e-06 v FourierNb 0.11616 0.6281 0.19637 0.16709 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9408 4.9408 0.00049342 -4.8207e-07 v volume_forces[Z] -4.9408 4.9408 -0.00049328 5.7845e-07 v ǁvolume_forcesǁ 3.4452e-08 4.9421 0.5001 0.23166 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.73 290.72 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.016145 5.6971e-05 3.1984e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.11616 0.6281 0.19638 0.1671 INSTANT 0.550836000E+00 TIME STEP NUMBER 572 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11786E-04 0.24258E-02 Friction velocity uk : 0.11787E-04 0.24257E-02 Dimensionless distance yplus : 0.78488E-04 0.16138E-01 Friction thermal sca. tstar : -0.23163E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.55125E-04 0.11335E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11786E-04 0.24258E-02 Friction velocity uk : 0.11787E-04 0.24257E-02 Dimensionless distance yplus : 0.78488E-04 0.16138E-01 Friction thermal sca. tstar : -0.23163E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.55125E-04 0.11335E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34437E-08 3 0.17458E-06 0.32413E-12 0.11503E+01 c Velocity[X] 0.13746E-31 c Velocity[Y] 0.16206E-12 c Velocity[Z] 0.16206E-12 c Pressure 0.11337E-13 20 0.88466E-07 0.88466E-07 0.14067E+01 c k 0.44146E-06 2 0.52493E-07 0.51137E-08 0.17740E+01 c omega 0.13153E+02 1 0.20715E-08 0.56047E+00 0.38975E-02 c TempK 0.94585E+02 1 0.13519E-06 0.31327E-01 0.19621E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.0816e-13 8.9992e-14 -1.1119e-17 -2.8602e-18 v Velocity[Y] -0.00013343 0.00012871 -1.0036e-09 -3.8688e-12 v Velocity[Z] -0.0001287 0.00013343 7.8597e-10 -1.3637e-12 v ǁVelocityǁ 9.4515e-10 0.00014295 1.0452e-05 6.6297e-06 v Pressure -0.00096694 0.019301 0.0010553 -1.6355e-19 v k 1.6537e-09 0.0014309 0.00098784 0.0012406 v omega 17.711 1.0313e+05 2668.3 502.22 v TempK 288 341.93 293.52 290.58 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.941e-14 9.7198e-05 6.1329e-05 7.9358e-05 v CourantNb 2.1935e-09 0.00022244 1.3976e-05 7.8366e-06 v FourierNb 0.11607 0.6281 0.19631 0.16704 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9409 4.9409 0.00049369 -4.8249e-07 v volume_forces[Z] -4.9409 4.9409 -0.00049355 5.7889e-07 v ǁvolume_forcesǁ 3.3982e-08 4.9422 0.50036 0.23186 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.73 290.72 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.016138 5.6951e-05 3.1972e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.11608 0.6281 0.19633 0.16705 INSTANT 0.551799000E+00 TIME STEP NUMBER 573 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11818E-04 0.24248E-02 Friction velocity uk : 0.11819E-04 0.24247E-02 Dimensionless distance yplus : 0.78702E-04 0.16132E-01 Friction thermal sca. tstar : -0.23813E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.55275E-04 0.11330E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11818E-04 0.24248E-02 Friction velocity uk : 0.11819E-04 0.24247E-02 Dimensionless distance yplus : 0.78702E-04 0.16132E-01 Friction thermal sca. tstar : -0.23813E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.55275E-04 0.11330E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34443E-08 3 0.21180E-06 0.32343E-12 0.11492E+01 c Velocity[X] 0.17235E-31 c Velocity[Y] 0.16171E-12 c Velocity[Z] 0.16172E-12 c Pressure 0.13400E-13 23 0.88803E-08 0.10456E-06 0.14045E+01 c k 0.44072E-06 2 0.52371E-07 0.50824E-08 0.17715E+01 c omega 0.13153E+02 1 0.20645E-08 0.55728E+00 0.38864E-02 c TempK 0.94585E+02 1 0.13486E-06 0.31245E-01 0.19595E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.0807e-13 8.9913e-14 -1.1094e-17 -2.8543e-18 v Velocity[Y] -0.00013336 0.00012863 -1.0019e-09 -3.3331e-12 v Velocity[Z] -0.00012862 0.00013336 7.8425e-10 -1.6543e-12 v ǁVelocityǁ 9.3213e-10 0.00014286 1.0454e-05 6.6352e-06 v Pressure -0.00096862 0.019318 0.0010565 -3.6034e-20 v k 1.6462e-09 0.0014285 0.00098606 0.0012385 v omega 17.686 1.0313e+05 2668.3 502.19 v TempK 288 341.93 293.52 290.58 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.9322e-14 9.7185e-05 6.1304e-05 7.933e-05 v CourantNb 2.1908e-09 0.00022228 1.3973e-05 7.8391e-06 v FourierNb 0.11599 0.6281 0.19626 0.16699 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.941 4.941 0.00049395 -4.829e-07 v volume_forces[Z] -4.941 4.941 -0.00049381 5.7938e-07 v ǁvolume_forcesǁ 3.4167e-08 4.9423 0.50063 0.23206 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.73 290.72 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.016132 5.6931e-05 3.1959e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.11599 0.6281 0.19627 0.16699 INSTANT 0.552762000E+00 TIME STEP NUMBER 574 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11734E-04 0.24238E-02 Friction velocity uk : 0.11735E-04 0.24237E-02 Dimensionless distance yplus : 0.78142E-04 0.16125E-01 Friction thermal sca. tstar : -0.24526E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.54882E-04 0.11325E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11734E-04 0.24238E-02 Friction velocity uk : 0.11735E-04 0.24237E-02 Dimensionless distance yplus : 0.78142E-04 0.16125E-01 Friction thermal sca. tstar : -0.24526E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.54882E-04 0.11325E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34449E-08 3 0.17355E-06 0.32274E-12 0.11481E+01 c Velocity[X] 0.13609E-31 c Velocity[Y] 0.16137E-12 c Velocity[Z] 0.16137E-12 c Pressure 0.11154E-13 20 0.87040E-07 0.87040E-07 0.14015E+01 c k 0.43999E-06 2 0.52250E-07 0.50513E-08 0.17691E+01 c omega 0.13153E+02 1 0.20575E-08 0.55411E+00 0.38753E-02 c TempK 0.94586E+02 1 0.13453E-06 0.31165E-01 0.19569E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.0798e-13 8.985e-14 -1.1102e-17 -2.856e-18 v Velocity[Y] -0.00013329 0.00012856 -1.0011e-09 -3.8537e-12 v Velocity[Z] -0.00012854 0.00013329 7.8275e-10 -1.3675e-12 v ǁVelocityǁ 9.372e-10 0.00014278 1.0456e-05 6.6407e-06 v Pressure -0.00097031 0.019334 0.0010576 -5.942e-20 v k 1.6388e-09 0.0014261 0.00098429 0.0012363 v omega 17.662 1.0313e+05 2668.3 502.17 v TempK 288 341.93 293.52 290.58 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.9235e-14 9.7171e-05 6.1279e-05 7.9302e-05 v CourantNb 2.2007e-09 0.00022212 1.3971e-05 7.8416e-06 v FourierNb 0.1159 0.6281 0.1962 0.16693 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.941 4.9411 0.00049422 -4.8332e-07 v volume_forces[Z] -4.941 4.9411 -0.00049408 5.7983e-07 v ǁvolume_forcesǁ 3.3697e-08 4.9423 0.50089 0.23227 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.74 290.72 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.016125 5.6911e-05 3.1947e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.11591 0.6281 0.19622 0.16694 INSTANT 0.553725000E+00 TIME STEP NUMBER 575 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11766E-04 0.24228E-02 Friction velocity uk : 0.11767E-04 0.24227E-02 Dimensionless distance yplus : 0.78355E-04 0.16119E-01 Friction thermal sca. tstar : -0.25301E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.55031E-04 0.11321E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11766E-04 0.24228E-02 Friction velocity uk : 0.11767E-04 0.24227E-02 Dimensionless distance yplus : 0.78355E-04 0.16119E-01 Friction thermal sca. tstar : -0.25301E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.55031E-04 0.11321E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34455E-08 3 0.21066E-06 0.32204E-12 0.11470E+01 c Velocity[X] 0.17065E-31 c Velocity[Y] 0.16102E-12 c Velocity[Z] 0.16103E-12 c Pressure 0.13315E-13 23 0.88346E-08 0.10390E-06 0.13994E+01 c k 0.43926E-06 2 0.52130E-07 0.50204E-08 0.17666E+01 c omega 0.13153E+02 1 0.20505E-08 0.55097E+00 0.38643E-02 c TempK 0.94587E+02 1 0.13420E-06 0.31084E-01 0.19544E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.0789e-13 8.9771e-14 -1.1077e-17 -2.8502e-18 v Velocity[Y] -0.00013322 0.00012848 -9.9941e-10 -3.3186e-12 v Velocity[Z] -0.00012847 0.00013322 7.8101e-10 -1.6581e-12 v ǁVelocityǁ 9.2417e-10 0.00014269 1.0458e-05 6.6463e-06 v Pressure -0.000972 0.019351 0.0010588 5.9812e-20 v k 1.6314e-09 0.0014237 0.00098252 0.0012342 v omega 17.637 1.0313e+05 2668.3 502.15 v TempK 288 341.93 293.53 290.58 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.9148e-14 9.7157e-05 6.1254e-05 7.9274e-05 v CourantNb 2.1979e-09 0.00022196 1.3969e-05 7.8441e-06 v FourierNb 0.11582 0.6281 0.19615 0.16688 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9411 4.9411 0.00049449 -4.8372e-07 v volume_forces[Z] -4.9411 4.9411 -0.00049434 5.8031e-07 v ǁvolume_forcesǁ 3.388e-08 4.9424 0.50116 0.23247 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.74 290.73 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.016119 5.6891e-05 3.1935e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.11582 0.6281 0.19616 0.16689 INSTANT 0.554688000E+00 TIME STEP NUMBER 576 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11681E-04 0.24218E-02 Friction velocity uk : 0.11682E-04 0.24217E-02 Dimensionless distance yplus : 0.77791E-04 0.16112E-01 Friction thermal sca. tstar : -0.26162E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.54636E-04 0.11316E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11681E-04 0.24218E-02 Friction velocity uk : 0.11682E-04 0.24217E-02 Dimensionless distance yplus : 0.77791E-04 0.16112E-01 Friction thermal sca. tstar : -0.26162E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.54636E-04 0.11316E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34461E-08 3 0.17259E-06 0.32136E-12 0.11459E+01 c Velocity[X] 0.13475E-31 c Velocity[Y] 0.16068E-12 c Velocity[Z] 0.16068E-12 c Pressure 0.11097E-13 20 0.86591E-07 0.86591E-07 0.13965E+01 c k 0.43853E-06 2 0.52010E-07 0.49898E-08 0.17642E+01 c omega 0.13153E+02 1 0.20436E-08 0.54784E+00 0.38533E-02 c TempK 0.94587E+02 1 0.13387E-06 0.31004E-01 0.19519E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.078e-13 8.9709e-14 -1.1085e-17 -2.8518e-18 v Velocity[Y] -0.00013315 0.00012841 -9.9863e-10 -3.8387e-12 v Velocity[Z] -0.00012839 0.00013315 7.795e-10 -1.3713e-12 v ǁVelocityǁ 9.2919e-10 0.00014261 1.046e-05 6.6518e-06 v Pressure -0.00097369 0.019368 0.00106 7.8933e-20 v k 1.624e-09 0.0014214 0.00098075 0.0012321 v omega 17.613 1.0313e+05 2668.3 502.13 v TempK 288 341.93 293.53 290.59 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.9062e-14 9.7143e-05 6.1229e-05 7.9246e-05 v CourantNb 2.2078e-09 0.0002218 1.3966e-05 7.8466e-06 v FourierNb 0.11574 0.6281 0.19609 0.16683 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9412 4.9412 0.00049475 -4.8414e-07 v volume_forces[Z] -4.9412 4.9412 -0.00049461 5.8075e-07 v ǁvolume_forcesǁ 3.3409e-08 4.9425 0.50142 0.23267 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.74 290.73 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.016112 5.687e-05 3.1923e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.11574 0.6281 0.19611 0.16684 INSTANT 0.555651000E+00 TIME STEP NUMBER 577 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11713E-04 0.24208E-02 Friction velocity uk : 0.11714E-04 0.24207E-02 Dimensionless distance yplus : 0.78003E-04 0.16105E-01 Friction thermal sca. tstar : -0.27109E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.54784E-04 0.11311E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11713E-04 0.24208E-02 Friction velocity uk : 0.11714E-04 0.24207E-02 Dimensionless distance yplus : 0.78003E-04 0.16105E-01 Friction thermal sca. tstar : -0.27109E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.54784E-04 0.11311E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34467E-08 3 0.20952E-06 0.32067E-12 0.11448E+01 c Velocity[X] 0.16896E-31 c Velocity[Y] 0.16033E-12 c Velocity[Z] 0.16034E-12 c Pressure 0.13258E-13 23 0.88062E-08 0.10345E-06 0.13944E+01 c k 0.43780E-06 2 0.51890E-07 0.49594E-08 0.17617E+01 c omega 0.13153E+02 1 0.20367E-08 0.54474E+00 0.38424E-02 c TempK 0.94588E+02 1 0.13355E-06 0.30924E-01 0.19493E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.0772e-13 8.963e-14 -1.106e-17 -2.846e-18 v Velocity[Y] -0.00013308 0.00012833 -9.9692e-10 -3.3043e-12 v Velocity[Z] -0.00012832 0.00013308 7.7775e-10 -1.6621e-12 v ǁVelocityǁ 9.1614e-10 0.00014253 1.0462e-05 6.6573e-06 v Pressure -0.00097537 0.019384 0.0010611 4.9615e-20 v k 1.6168e-09 0.001419 0.000979 0.00123 v omega 17.588 1.0313e+05 2668.2 502.11 v TempK 288 341.93 293.53 290.59 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.8976e-14 9.7129e-05 6.1204e-05 7.9218e-05 v CourantNb 2.205e-09 0.00022164 1.3964e-05 7.8492e-06 v FourierNb 0.11565 0.6281 0.19604 0.16678 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9413 4.9413 0.00049502 -4.8455e-07 v volume_forces[Z] -4.9413 4.9413 -0.00049487 5.8123e-07 v ǁvolume_forcesǁ 3.359e-08 4.9426 0.50169 0.23287 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.75 290.73 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.016105 5.6851e-05 3.1911e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.11565 0.6281 0.19605 0.16679 INSTANT 0.556614000E+00 TIME STEP NUMBER 578 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11628E-04 0.24198E-02 Friction velocity uk : 0.11629E-04 0.24197E-02 Dimensionless distance yplus : 0.77436E-04 0.16099E-01 Friction thermal sca. tstar : -0.28176E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.54386E-04 0.11307E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11628E-04 0.24198E-02 Friction velocity uk : 0.11629E-04 0.24197E-02 Dimensionless distance yplus : 0.77436E-04 0.16099E-01 Friction thermal sca. tstar : -0.28176E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.54386E-04 0.11307E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34473E-08 3 0.18572E-06 0.31999E-12 0.11437E+01 c Velocity[X] 0.13342E-31 c Velocity[Y] 0.15999E-12 c Velocity[Z] 0.16000E-12 c Pressure 0.11045E-13 20 0.86179E-07 0.86179E-07 0.13914E+01 c k 0.43708E-06 2 0.51771E-07 0.49292E-08 0.17593E+01 c omega 0.13153E+02 1 0.20298E-08 0.54166E+00 0.38315E-02 c TempK 0.94588E+02 1 0.13322E-06 0.30844E-01 0.19468E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.0763e-13 8.9568e-14 -1.1067e-17 -2.8477e-18 v Velocity[Y] -0.00013301 0.00012826 -9.9613e-10 -3.8237e-12 v Velocity[Z] -0.00012824 0.00013301 7.7623e-10 -1.375e-12 v ǁVelocityǁ 9.2112e-10 0.00014244 1.0464e-05 6.6629e-06 v Pressure -0.00097706 0.019401 0.0010623 3.6034e-20 v k 1.6095e-09 0.0014166 0.00097724 0.0012279 v omega 17.564 1.0313e+05 2668.2 502.08 v TempK 288 341.93 293.53 290.59 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.8891e-14 9.7116e-05 6.1179e-05 7.919e-05 v CourantNb 2.2149e-09 0.00022149 1.3962e-05 7.8517e-06 v FourierNb 0.11557 0.6281 0.19598 0.16673 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9413 4.9414 0.00049528 -4.8497e-07 v volume_forces[Z] -4.9413 4.9414 -0.00049514 5.8167e-07 v ǁvolume_forcesǁ 3.3119e-08 4.9426 0.50195 0.23308 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.75 290.73 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.016099 5.683e-05 3.1898e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.11557 0.6281 0.196 0.16673 INSTANT 0.557577000E+00 TIME STEP NUMBER 579 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11660E-04 0.24188E-02 Friction velocity uk : 0.11661E-04 0.24188E-02 Dimensionless distance yplus : 0.77647E-04 0.16092E-01 Friction thermal sca. tstar : -0.29369E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.54534E-04 0.11302E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11660E-04 0.24188E-02 Friction velocity uk : 0.11661E-04 0.24188E-02 Dimensionless distance yplus : 0.77647E-04 0.16092E-01 Friction thermal sca. tstar : -0.29369E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.54534E-04 0.11302E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34479E-08 3 0.20838E-06 0.31931E-12 0.11426E+01 c Velocity[X] 0.16729E-31 c Velocity[Y] 0.15965E-12 c Velocity[Z] 0.15966E-12 c Pressure 0.13186E-13 23 0.87735E-08 0.10288E-06 0.13893E+01 c k 0.43636E-06 2 0.51653E-07 0.48992E-08 0.17569E+01 c omega 0.13153E+02 1 0.20230E-08 0.53860E+00 0.38207E-02 c TempK 0.94589E+02 1 0.13290E-06 0.30765E-01 0.19443E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.0754e-13 8.949e-14 -1.1043e-17 -2.8419e-18 v Velocity[Y] -0.00013294 0.00012818 -9.944e-10 -3.2902e-12 v Velocity[Z] -0.00012817 0.00013294 7.7447e-10 -1.6659e-12 v ǁVelocityǁ 9.0806e-10 0.00014236 1.0466e-05 6.6684e-06 v Pressure -0.00097875 0.019418 0.0010635 2.9416e-21 v k 1.6023e-09 0.0014143 0.0009755 0.0012257 v omega 17.539 1.0313e+05 2668.2 502.06 v TempK 288 341.93 293.54 290.59 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.8806e-14 9.7102e-05 6.1154e-05 7.9162e-05 v CourantNb 2.2121e-09 0.00022133 1.3959e-05 7.8542e-06 v FourierNb 0.11548 0.6281 0.19593 0.16667 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9414 4.9415 0.00049554 -4.8537e-07 v volume_forces[Z] -4.9414 4.9415 -0.0004954 5.8215e-07 v ǁvolume_forcesǁ 3.3299e-08 4.9427 0.50221 0.23328 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.75 290.73 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.016092 5.681e-05 3.1886e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.11549 0.6281 0.19594 0.16668 INSTANT 0.558540000E+00 TIME STEP NUMBER 580 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+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-04 0.24178E-02 Friction velocity uk : 0.11575E-04 0.24178E-02 Dimensionless distance yplus : 0.77077E-04 0.16086E-01 Friction thermal sca. tstar : -0.30741E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.54134E-04 0.11297E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+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-04 0.24178E-02 Friction velocity uk : 0.11575E-04 0.24178E-02 Dimensionless distance yplus : 0.77077E-04 0.16086E-01 Friction thermal sca. tstar : -0.30741E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.54134E-04 0.11297E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34485E-08 3 0.17072E-06 0.31863E-12 0.11415E+01 c Velocity[X] 0.13211E-31 c Velocity[Y] 0.15931E-12 c Velocity[Z] 0.15932E-12 c Pressure 0.10997E-13 20 0.85801E-07 0.85801E-07 0.13864E+01 c k 0.43564E-06 2 0.51534E-07 0.48695E-08 0.17545E+01 c omega 0.13153E+02 1 0.20162E-08 0.53556E+00 0.38099E-02 c TempK 0.94590E+02 1 0.13257E-06 0.30686E-01 0.19418E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.0746e-13 8.9428e-14 -1.105e-17 -2.8436e-18 v Velocity[Y] -0.00013287 0.00012811 -9.9359e-10 -3.8089e-12 v Velocity[Z] -0.00012809 0.00013288 7.7293e-10 -1.3788e-12 v ǁVelocityǁ 9.13e-10 0.00014228 1.0469e-05 6.674e-06 v Pressure -0.00098044 0.019434 0.0010646 3.1671e-20 v k 1.5951e-09 0.001412 0.00097375 0.0012237 v omega 17.515 1.0313e+05 2668.2 502.04 v TempK 288 341.93 293.54 290.59 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.8722e-14 9.7088e-05 6.1129e-05 7.9135e-05 v CourantNb 2.222e-09 0.00022117 1.3957e-05 7.8568e-06 v FourierNb 0.1154 0.6281 0.19588 0.16662 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9415 4.9415 0.00049581 -4.8579e-07 v volume_forces[Z] -4.9415 4.9415 -0.00049567 5.8259e-07 v ǁvolume_forcesǁ 3.2827e-08 4.9428 0.50248 0.23348 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.75 290.74 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.016086 5.679e-05 3.1874e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.1154 0.6281 0.19589 0.16663 INSTANT 0.559503000E+00 TIME STEP NUMBER 581 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11606E-04 0.24168E-02 Friction velocity uk : 0.11607E-04 0.24168E-02 Dimensionless distance yplus : 0.77287E-04 0.16079E-01 Friction thermal sca. tstar : -0.32310E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.54281E-04 0.11293E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11606E-04 0.24168E-02 Friction velocity uk : 0.11607E-04 0.24168E-02 Dimensionless distance yplus : 0.77287E-04 0.16079E-01 Friction thermal sca. tstar : -0.32310E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.54281E-04 0.11293E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34491E-08 3 0.20728E-06 0.31796E-12 0.11404E+01 c Velocity[X] 0.16564E-31 c Velocity[Y] 0.15897E-12 c Velocity[Z] 0.15898E-12 c Pressure 0.13155E-13 23 0.87373E-08 0.10264E-06 0.13843E+01 c k 0.43492E-06 2 0.51417E-07 0.48400E-08 0.17520E+01 c omega 0.13153E+02 1 0.20094E-08 0.53255E+00 0.37992E-02 c TempK 0.94590E+02 1 0.13225E-06 0.30607E-01 0.19393E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.0737e-13 8.935e-14 -1.1026e-17 -2.8378e-18 v Velocity[Y] -0.0001328 0.00012804 -9.9185e-10 -3.2763e-12 v Velocity[Z] -0.00012802 0.00013281 7.7116e-10 -1.6693e-12 v ǁVelocityǁ 8.9993e-10 0.0001422 1.0471e-05 6.6795e-06 v Pressure -0.00098212 0.019451 0.0010658 1.8483e-20 v k 1.588e-09 0.0014096 0.00097202 0.0012216 v omega 17.491 1.0313e+05 2668.2 502.02 v TempK 288 341.93 293.54 290.6 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.8638e-14 9.7075e-05 6.1105e-05 7.9107e-05 v CourantNb 2.2192e-09 0.00022102 1.3955e-05 7.8594e-06 v FourierNb 0.11531 0.6281 0.19582 0.16657 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9416 4.9416 0.00049607 -4.8618e-07 v volume_forces[Z] -4.9416 4.9416 -0.00049593 5.8307e-07 v ǁvolume_forcesǁ 3.3005e-08 4.9429 0.50274 0.23368 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.76 290.74 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.016079 5.677e-05 3.1862e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.11532 0.6281 0.19584 0.16658 INSTANT 0.560466000E+00 TIME STEP NUMBER 582 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11520E-04 0.24158E-02 Friction velocity uk : 0.11520E-04 0.24158E-02 Dimensionless distance yplus : 0.76713E-04 0.16072E-01 Friction thermal sca. tstar : -0.34163E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.53878E-04 0.11288E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11520E-04 0.24158E-02 Friction velocity uk : 0.11520E-04 0.24158E-02 Dimensionless distance yplus : 0.76713E-04 0.16072E-01 Friction thermal sca. tstar : -0.34163E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.53878E-04 0.11288E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34498E-08 3 0.16981E-06 0.31729E-12 0.11393E+01 c Velocity[X] 0.13081E-31 c Velocity[Y] 0.15864E-12 c Velocity[Z] 0.15865E-12 c Pressure 0.10973E-13 20 0.85609E-07 0.85609E-07 0.13814E+01 c k 0.43420E-06 2 0.51300E-07 0.48107E-08 0.17496E+01 c omega 0.13153E+02 1 0.20026E-08 0.52955E+00 0.37885E-02 c TempK 0.94591E+02 1 0.13193E-06 0.30529E-01 0.19368E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.0728e-13 8.9289e-14 -1.1033e-17 -2.8395e-18 v Velocity[Y] -0.00013274 0.00012796 -9.9103e-10 -3.7941e-12 v Velocity[Z] -0.00012795 0.00013274 7.6961e-10 -1.3825e-12 v ǁVelocityǁ 9.0482e-10 0.00014212 1.0473e-05 6.6851e-06 v Pressure -0.00098381 0.019468 0.0010669 -5.4615e-20 v k 1.5809e-09 0.0014073 0.00097029 0.0012195 v omega 17.467 1.0313e+05 2668.1 502 v TempK 288 341.93 293.55 290.6 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.8555e-14 9.7061e-05 6.108e-05 7.9079e-05 v CourantNb 2.2291e-09 0.00022086 1.3953e-05 7.8619e-06 v FourierNb 0.11523 0.6281 0.19577 0.16652 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9417 4.9417 0.00049634 -4.866e-07 v volume_forces[Z] -4.9417 4.9417 -0.00049619 5.8351e-07 v ǁvolume_forcesǁ 3.2532e-08 4.943 0.503 0.23388 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.76 290.74 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.016072 5.675e-05 3.185e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.11523 0.6281 0.19578 0.16653 INSTANT 0.561429000E+00 TIME STEP NUMBER 583 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11551E-04 0.24149E-02 Friction velocity uk : 0.11552E-04 0.24148E-02 Dimensionless distance yplus : 0.76922E-04 0.16066E-01 Friction thermal sca. tstar : -0.36356E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.54025E-04 0.11284E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11551E-04 0.24149E-02 Friction velocity uk : 0.11552E-04 0.24148E-02 Dimensionless distance yplus : 0.76922E-04 0.16066E-01 Friction thermal sca. tstar : -0.36356E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.54025E-04 0.11284E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34504E-08 3 0.20611E-06 0.31662E-12 0.11382E+01 c Velocity[X] 0.16401E-31 c Velocity[Y] 0.15831E-12 c Velocity[Z] 0.15831E-12 c Pressure 0.13054E-13 23 0.87009E-08 0.10184E-06 0.13794E+01 c k 0.43349E-06 2 0.51183E-07 0.47816E-08 0.17472E+01 c omega 0.13153E+02 1 0.19959E-08 0.52658E+00 0.37778E-02 c TempK 0.94591E+02 1 0.13161E-06 0.30451E-01 0.19343E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.072e-13 8.9211e-14 -1.1009e-17 -2.8338e-18 v Velocity[Y] -0.00013267 0.00012789 -9.8927e-10 -3.2621e-12 v Velocity[Z] -0.00012787 0.00013267 7.6783e-10 -1.6732e-12 v ǁVelocityǁ 8.9173e-10 0.00014205 1.0475e-05 6.6907e-06 v Pressure -0.0009855 0.019484 0.0010681 6.2018e-20 v k 1.5739e-09 0.001405 0.00096856 0.0012174 v omega 17.443 1.0313e+05 2668.1 501.97 v TempK 288 341.94 293.55 290.6 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.8472e-14 9.7047e-05 6.1055e-05 7.9051e-05 v CourantNb 2.2263e-09 0.0002207 1.395e-05 7.8645e-06 v FourierNb 0.11515 0.6281 0.19571 0.16647 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9417 4.9418 0.0004966 -4.87e-07 v volume_forces[Z] -4.9417 4.9418 -0.00049646 5.8398e-07 v ǁvolume_forcesǁ 3.2709e-08 4.943 0.50326 0.23409 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.76 290.74 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.016066 5.673e-05 3.1838e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.11515 0.6281 0.19573 0.16648 INSTANT 0.562392000E+00 TIME STEP NUMBER 584 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11464E-04 0.24139E-02 Friction velocity uk : 0.11465E-04 0.24138E-02 Dimensionless distance yplus : 0.76344E-04 0.16059E-01 Friction thermal sca. tstar : -0.39060E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.53619E-04 0.11279E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11464E-04 0.24139E-02 Friction velocity uk : 0.11465E-04 0.24138E-02 Dimensionless distance yplus : 0.76344E-04 0.16059E-01 Friction thermal sca. tstar : -0.39060E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.53619E-04 0.11279E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34510E-08 3 0.16888E-06 0.31595E-12 0.11371E+01 c Velocity[X] 0.12952E-31 c Velocity[Y] 0.15798E-12 c Velocity[Z] 0.15798E-12 c Pressure 0.10881E-13 20 0.84885E-07 0.84885E-07 0.13765E+01 c k 0.43278E-06 2 0.51067E-07 0.47528E-08 0.17448E+01 c omega 0.13153E+02 1 0.19892E-08 0.52363E+00 0.37672E-02 c TempK 0.94592E+02 1 0.13130E-06 0.30374E-01 0.19318E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.0711e-13 8.915e-14 -1.1017e-17 -2.8354e-18 v Velocity[Y] -0.0001326 0.00012781 -9.8844e-10 -3.7794e-12 v Velocity[Z] -0.0001278 0.0001326 7.6627e-10 -1.3862e-12 v ǁVelocityǁ 8.9658e-10 0.00014197 1.0478e-05 6.6963e-06 v Pressure -0.00098718 0.019501 0.0010692 4.4712e-20 v k 1.5669e-09 0.0014026 0.00096684 0.0012153 v omega 17.419 1.0313e+05 2668.1 501.95 v TempK 288 341.94 293.55 290.6 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.839e-14 9.7034e-05 6.1031e-05 7.9024e-05 v CourantNb 2.2362e-09 0.00022055 1.3948e-05 7.8671e-06 v FourierNb 0.11506 0.6281 0.19566 0.16642 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9418 4.9418 0.00049686 -4.8741e-07 v volume_forces[Z] -4.9418 4.9418 -0.00049672 5.8442e-07 v ǁvolume_forcesǁ 3.2236e-08 4.9431 0.50352 0.23429 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.77 290.75 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.016059 5.671e-05 3.1826e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.11507 0.6281 0.19567 0.16643 INSTANT 0.563355000E+00 TIME STEP NUMBER 585 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11495E-04 0.24129E-02 Friction velocity uk : 0.11496E-04 0.24129E-02 Dimensionless distance yplus : 0.76552E-04 0.16053E-01 Friction thermal sca. tstar : -0.42441E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.53765E-04 0.11275E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11495E-04 0.24129E-02 Friction velocity uk : 0.11496E-04 0.24129E-02 Dimensionless distance yplus : 0.76552E-04 0.16053E-01 Friction thermal sca. tstar : -0.42441E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.53765E-04 0.11275E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34517E-08 3 0.20502E-06 0.31529E-12 0.11361E+01 c Velocity[X] 0.16241E-31 c Velocity[Y] 0.15764E-12 c Velocity[Z] 0.15765E-12 c Pressure 0.12988E-13 23 0.86710E-08 0.10133E-06 0.13744E+01 c k 0.43207E-06 2 0.50951E-07 0.47242E-08 0.17425E+01 c omega 0.13153E+02 1 0.19826E-08 0.52069E+00 0.37566E-02 c TempK 0.94593E+02 1 0.13098E-06 0.30296E-01 0.19293E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.0703e-13 8.9073e-14 -1.0992e-17 -2.8297e-18 v Velocity[Y] -0.00013253 0.00012774 -9.8667e-10 -3.248e-12 v Velocity[Z] -0.00012773 0.00013253 7.6448e-10 -1.6768e-12 v ǁVelocityǁ 8.8348e-10 0.0001419 1.048e-05 6.7019e-06 v Pressure -0.00098887 0.019517 0.0010704 -2.4562e-20 v k 1.5599e-09 0.0014004 0.00096513 0.0012133 v omega 17.395 1.0313e+05 2668.1 501.93 v TempK 288 341.94 293.56 290.61 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.8308e-14 9.702e-05 6.1006e-05 7.8996e-05 v CourantNb 2.2334e-09 0.00022039 1.3946e-05 7.8697e-06 v FourierNb 0.11498 0.6281 0.19561 0.16637 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9419 4.9419 0.00049712 -4.8781e-07 v volume_forces[Z] -4.9419 4.9419 -0.00049698 5.8489e-07 v ǁvolume_forcesǁ 3.2411e-08 4.9432 0.50379 0.23449 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.77 290.75 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.016053 5.669e-05 3.1814e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.11498 0.6281 0.19562 0.16637 INSTANT 0.564318000E+00 TIME STEP NUMBER 586 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11408E-04 0.24119E-02 Friction velocity uk : 0.11409E-04 0.24119E-02 Dimensionless distance yplus : 0.75971E-04 0.16046E-01 Friction thermal sca. tstar : -0.46930E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.53357E-04 0.11270E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11408E-04 0.24119E-02 Friction velocity uk : 0.11409E-04 0.24119E-02 Dimensionless distance yplus : 0.75971E-04 0.16046E-01 Friction thermal sca. tstar : -0.46930E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.53357E-04 0.11270E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34523E-08 3 0.16796E-06 0.31463E-12 0.11350E+01 c Velocity[X] 0.12826E-31 c Velocity[Y] 0.15731E-12 c Velocity[Z] 0.15732E-12 c Pressure 0.10827E-13 20 0.84464E-07 0.84464E-07 0.13716E+01 c k 0.43136E-06 2 0.50836E-07 0.46957E-08 0.17401E+01 c omega 0.13153E+02 1 0.19760E-08 0.51778E+00 0.37461E-02 c TempK 0.94593E+02 1 0.13067E-06 0.30219E-01 0.19269E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.0694e-13 8.9012e-14 -1.1e-17 -2.8314e-18 v Velocity[Y] -0.00013246 0.00012767 -9.8582e-10 -3.7647e-12 v Velocity[Z] -0.00012765 0.00013247 7.629e-10 -1.3898e-12 v ǁVelocityǁ 8.8828e-10 0.00014183 1.0482e-05 6.7075e-06 v Pressure -0.00099055 0.019534 0.0010716 -3.3338e-21 v k 1.553e-09 0.0013983 0.00096342 0.0012112 v omega 17.371 1.0313e+05 2668.1 501.91 v TempK 288 341.94 293.56 290.61 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.8227e-14 9.7007e-05 6.0982e-05 7.8968e-05 v CourantNb 2.2432e-09 0.00022024 1.3944e-05 7.8724e-06 v FourierNb 0.1149 0.6281 0.19555 0.16632 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.942 4.942 0.00049738 -4.8822e-07 v volume_forces[Z] -4.942 4.942 -0.00049724 5.8533e-07 v ǁvolume_forcesǁ 3.1938e-08 4.9433 0.50405 0.23469 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.77 290.75 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.016046 5.667e-05 3.1801e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.1149 0.6281 0.19557 0.16632 INSTANT 0.565281000E+00 TIME STEP NUMBER 587 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11439E-04 0.24110E-02 Friction velocity uk : 0.11440E-04 0.24109E-02 Dimensionless distance yplus : 0.76178E-04 0.16040E-01 Friction thermal sca. tstar : -0.53167E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.53503E-04 0.11265E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11439E-04 0.24110E-02 Friction velocity uk : 0.11440E-04 0.24109E-02 Dimensionless distance yplus : 0.76178E-04 0.16040E-01 Friction thermal sca. tstar : -0.53167E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.53503E-04 0.11265E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34530E-08 3 0.20395E-06 0.31397E-12 0.11339E+01 c Velocity[X] 0.16082E-31 c Velocity[Y] 0.15698E-12 c Velocity[Z] 0.15699E-12 c Pressure 0.12985E-13 23 0.86779E-08 0.10130E-06 0.13695E+01 c k 0.43066E-06 2 0.50721E-07 0.46675E-08 0.17377E+01 c omega 0.13153E+02 1 0.19694E-08 0.51489E+00 0.37356E-02 c TempK 0.94594E+02 1 0.13035E-06 0.30143E-01 0.19244E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.0685e-13 8.8935e-14 -1.0976e-17 -2.8257e-18 v Velocity[Y] -0.0001324 0.0001276 -9.8403e-10 -3.234e-12 v Velocity[Z] -0.00012758 0.0001324 7.611e-10 -1.6801e-12 v ǁVelocityǁ 8.7517e-10 0.00014175 1.0484e-05 6.7131e-06 v Pressure -0.00099224 0.01955 0.0010727 9.3738e-20 v k 1.5461e-09 0.0013961 0.00096172 0.0012092 v omega 17.347 1.0313e+05 2668.1 501.89 v TempK 288 341.94 293.56 290.61 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.8146e-14 9.6993e-05 6.0957e-05 7.8941e-05 v CourantNb 2.2405e-09 0.00022009 1.3942e-05 7.875e-06 v FourierNb 0.11481 0.6281 0.1955 0.16626 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.942 4.9421 0.00049765 -4.8861e-07 v volume_forces[Z] -4.942 4.9421 -0.0004975 5.858e-07 v ǁvolume_forcesǁ 3.2111e-08 4.9433 0.50431 0.23489 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.77 290.75 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.01604 5.665e-05 3.1789e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.11482 0.6281 0.19551 0.16627 INSTANT 0.566244000E+00 TIME STEP NUMBER 588 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11351E-04 0.24100E-02 Friction velocity uk : 0.11352E-04 0.24099E-02 Dimensionless distance yplus : 0.75594E-04 0.16033E-01 Friction thermal sca. tstar : -0.62910E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.53092E-04 0.11261E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11351E-04 0.24100E-02 Friction velocity uk : 0.11352E-04 0.24099E-02 Dimensionless distance yplus : 0.75594E-04 0.16033E-01 Friction thermal sca. tstar : -0.62910E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.53092E-04 0.11261E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34537E-08 3 0.16705E-06 0.31332E-12 0.11328E+01 c Velocity[X] 0.12701E-31 c Velocity[Y] 0.15666E-12 c Velocity[Z] 0.15666E-12 c Pressure 0.10781E-13 20 0.84104E-07 0.84104E-07 0.13667E+01 c k 0.42995E-06 2 0.50607E-07 0.46395E-08 0.17353E+01 c omega 0.13153E+02 1 0.19628E-08 0.51202E+00 0.37252E-02 c TempK 0.94594E+02 1 0.13004E-06 0.30066E-01 0.19219E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.0677e-13 8.8874e-14 -1.0983e-17 -2.8274e-18 v Velocity[Y] -0.00013233 0.00012752 -9.8317e-10 -3.7501e-12 v Velocity[Z] -0.00012751 0.00013233 7.5951e-10 -1.3933e-12 v ǁVelocityǁ 8.7992e-10 0.00014168 1.0487e-05 6.7187e-06 v Pressure -0.00099393 0.019567 0.0010739 6.4911e-20 v k 1.5393e-09 0.001394 0.00096002 0.0012071 v omega 17.324 1.0313e+05 2668 501.87 v TempK 288 341.94 293.56 290.61 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.8065e-14 9.698e-05 6.0933e-05 7.8913e-05 v CourantNb 2.2503e-09 0.00021993 1.394e-05 7.8776e-06 v FourierNb 0.11473 0.6281 0.19544 0.16621 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9421 4.9422 0.00049791 -4.8903e-07 v volume_forces[Z] -4.9421 4.9422 -0.00049777 5.8623e-07 v ǁvolume_forcesǁ 3.1638e-08 4.9434 0.50457 0.23509 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.78 290.76 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.016033 5.6629e-05 3.1777e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.11473 0.6281 0.19546 0.16622 INSTANT 0.567207000E+00 TIME STEP NUMBER 589 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11382E-04 0.24090E-02 Friction velocity uk : 0.11383E-04 0.24090E-02 Dimensionless distance yplus : 0.75800E-04 0.16027E-01 Friction thermal sca. tstar : -0.99728E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.53237E-04 0.11256E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11382E-04 0.24090E-02 Friction velocity uk : 0.11383E-04 0.24090E-02 Dimensionless distance yplus : 0.75800E-04 0.16027E-01 Friction thermal sca. tstar : -0.99728E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.53237E-04 0.11256E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34543E-08 3 0.20281E-06 0.31266E-12 0.11317E+01 c Velocity[X] 0.15925E-31 c Velocity[Y] 0.15633E-12 c Velocity[Z] 0.15633E-12 c Pressure 0.12861E-13 23 0.86068E-08 0.10033E-06 0.13647E+01 c k 0.42925E-06 2 0.50493E-07 0.46117E-08 0.17330E+01 c omega 0.13153E+02 1 0.19563E-08 0.50916E+00 0.37148E-02 c TempK 0.94595E+02 1 0.12973E-06 0.29990E-01 0.19195E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.0668e-13 8.8798e-14 -1.0959e-17 -2.8217e-18 v Velocity[Y] -0.00013226 0.00012745 -9.8137e-10 -3.2203e-12 v Velocity[Z] -0.00012743 0.00013227 7.5769e-10 -1.6839e-12 v ǁVelocityǁ 8.668e-10 0.0001416 1.0489e-05 6.7243e-06 v Pressure -0.00099561 0.019583 0.001075 3.726e-20 v k 1.5325e-09 0.0013919 0.00095833 0.0012051 v omega 17.3 1.0313e+05 2668 501.85 v TempK 288 341.94 293.57 290.61 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.7986e-14 9.6966e-05 6.0908e-05 7.8886e-05 v CourantNb 2.2476e-09 0.00021978 1.3938e-05 7.8803e-06 v FourierNb 0.11465 0.6281 0.19539 0.16616 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9422 4.9422 0.00049817 -4.8942e-07 v volume_forces[Z] -4.9422 4.9422 -0.00049803 5.867e-07 v ǁvolume_forcesǁ 3.1809e-08 4.9435 0.50483 0.23529 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.78 290.76 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.016027 5.6609e-05 3.1765e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.11465 0.6281 0.1954 0.16617 INSTANT 0.568170000E+00 TIME STEP NUMBER 590 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11294E-04 0.24081E-02 Friction velocity uk : 0.11295E-04 0.24080E-02 Dimensionless distance yplus : 0.75211E-04 0.16021E-01 Friction thermal sca. tstar : -0.13965E+05 0.00000E+00 Dim-less thermal sca. tplus : 0.52824E-04 0.11252E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11294E-04 0.24081E-02 Friction velocity uk : 0.11295E-04 0.24080E-02 Dimensionless distance yplus : 0.75211E-04 0.16021E-01 Friction thermal sca. tstar : -0.13965E+05 0.00000E+00 Dim-less thermal sca. tplus : 0.52824E-04 0.11252E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34550E-08 3 0.20268E-06 0.31201E-12 0.11306E+01 c Velocity[X] 0.12577E-31 c Velocity[Y] 0.15601E-12 c Velocity[Z] 0.15601E-12 c Pressure 0.10722E-13 20 0.83639E-07 0.83639E-07 0.13618E+01 c k 0.42855E-06 2 0.50380E-07 0.45841E-08 0.17306E+01 c omega 0.13153E+02 1 0.19498E-08 0.50633E+00 0.37045E-02 c TempK 0.94596E+02 1 0.12942E-06 0.29915E-01 0.19171E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.066e-13 8.8737e-14 -1.0966e-17 -2.8234e-18 v Velocity[Y] -0.0001322 0.00012738 -9.805e-10 -3.7356e-12 v Velocity[Z] -0.00012736 0.0001322 7.561e-10 -1.3968e-12 v ǁVelocityǁ 8.7151e-10 0.00014153 1.0491e-05 6.7299e-06 v Pressure -0.0009973 0.0196 0.0010762 1.2257e-20 v k 1.5258e-09 0.0013899 0.00095664 0.001203 v omega 17.276 1.0313e+05 2668 501.83 v TempK 288 341.94 293.57 290.62 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.7906e-14 9.6953e-05 6.0884e-05 7.8858e-05 v CourantNb 2.2573e-09 0.00021962 1.3936e-05 7.8829e-06 v FourierNb 0.11456 0.6281 0.19534 0.16611 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9423 4.9423 0.00049843 -4.8983e-07 v volume_forces[Z] -4.9423 4.9423 -0.00049829 5.8713e-07 v ǁvolume_forcesǁ 3.1335e-08 4.9436 0.50509 0.23549 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.78 290.76 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.016021 5.6589e-05 3.1752e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.11457 0.6281 0.19535 0.16612 INSTANT 0.569133000E+00 TIME STEP NUMBER 591 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11325E-04 0.24071E-02 Friction velocity uk : 0.11326E-04 0.24070E-02 Dimensionless distance yplus : 0.75417E-04 0.16014E-01 Friction thermal sca. tstar : -0.14284E+05 0.00000E+00 Dim-less thermal sca. tplus : 0.52968E-04 0.11247E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11325E-04 0.24071E-02 Friction velocity uk : 0.11326E-04 0.24070E-02 Dimensionless distance yplus : 0.75417E-04 0.16014E-01 Friction thermal sca. tstar : -0.14284E+05 0.00000E+00 Dim-less thermal sca. tplus : 0.52968E-04 0.11247E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34557E-08 3 0.20175E-06 0.31137E-12 0.11296E+01 c Velocity[X] 0.13395E-31 c Velocity[Y] 0.15568E-12 c Velocity[Z] 0.15568E-12 c Pressure 0.12800E-13 20 0.99844E-07 0.99844E-07 0.13598E+01 c k 0.42786E-06 2 0.50267E-07 0.45567E-08 0.17283E+01 c omega 0.13153E+02 1 0.19433E-08 0.50352E+00 0.36942E-02 c TempK 0.94596E+02 1 0.12911E-06 0.29839E-01 0.19146E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.0652e-13 8.8672e-14 -1.0963e-17 -2.8225e-18 v Velocity[Y] -0.00013213 0.00012731 -9.7914e-10 -3.717e-12 v Velocity[Z] -0.00012729 0.00013213 7.5441e-10 -1.3682e-12 v ǁVelocityǁ 8.6663e-10 0.00014146 1.0494e-05 6.7356e-06 v Pressure -0.00099898 0.019616 0.0010773 5.0987e-21 v k 1.5191e-09 0.0013878 0.00095496 0.001201 v omega 17.253 1.0313e+05 2668 501.8 v TempK 288 341.94 293.57 290.62 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.7827e-14 9.6939e-05 6.086e-05 7.8831e-05 v CourantNb 2.2607e-09 0.00021947 1.3934e-05 7.8856e-06 v FourierNb 0.11448 0.6281 0.19528 0.16606 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9424 4.9424 0.00049869 -4.9022e-07 v volume_forces[Z] -4.9424 4.9424 -0.00049855 5.876e-07 v ǁvolume_forcesǁ 3.1505e-08 4.9436 0.50535 0.23569 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.79 290.76 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.016014 5.6571e-05 3.1742e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.11449 0.6281 0.1953 0.16607 INSTANT 0.570096000E+00 TIME STEP NUMBER 592 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11291E-04 0.24062E-02 Friction velocity uk : 0.11292E-04 0.24061E-02 Dimensionless distance yplus : 0.75193E-04 0.16008E-01 Friction thermal sca. tstar : -0.81798E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.52810E-04 0.11243E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11291E-04 0.24062E-02 Friction velocity uk : 0.11292E-04 0.24061E-02 Dimensionless distance yplus : 0.75193E-04 0.16008E-01 Friction thermal sca. tstar : -0.81798E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.52810E-04 0.11243E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34564E-08 3 0.19876E-06 0.31072E-12 0.11285E+01 c Velocity[X] 0.13834E-31 c Velocity[Y] 0.15536E-12 c Velocity[Z] 0.15536E-12 c Pressure 0.12671E-13 20 0.98834E-07 0.98834E-07 0.13572E+01 c k 0.42716E-06 2 0.50154E-07 0.45295E-08 0.17259E+01 c omega 0.13153E+02 1 0.19369E-08 0.50072E+00 0.36839E-02 c TempK 0.94597E+02 1 0.12881E-06 0.29764E-01 0.19122E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.0643e-13 8.8604e-14 -1.0956e-17 -2.8207e-18 v Velocity[Y] -0.00013206 0.00012723 -9.7779e-10 -3.7132e-12 v Velocity[Z] -0.00012722 0.00013207 7.5268e-10 -1.3798e-12 v ǁVelocityǁ 8.6249e-10 0.00014139 1.0496e-05 6.7412e-06 v Pressure -0.0010007 0.019633 0.0010785 -1.1962e-20 v k 1.5124e-09 0.0013857 0.00095328 0.001199 v omega 17.229 1.0313e+05 2668 501.78 v TempK 288 341.94 293.58 290.62 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.7749e-14 9.6926e-05 6.0835e-05 7.8804e-05 v CourantNb 2.2646e-09 0.00021932 1.3932e-05 7.8882e-06 v FourierNb 0.1144 0.6281 0.19523 0.16601 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9424 4.9425 0.00049895 -4.9062e-07 v volume_forces[Z] -4.9424 4.9425 -0.00049881 5.8805e-07 v ǁvolume_forcesǁ 3.1329e-08 4.9437 0.50561 0.23589 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.79 290.76 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.016008 5.6553e-05 3.1731e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.1144 0.6281 0.19525 0.16602 INSTANT 0.571059000E+00 TIME STEP NUMBER 593 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11263E-04 0.24052E-02 Friction velocity uk : 0.11263E-04 0.24052E-02 Dimensionless distance yplus : 0.75002E-04 0.16002E-01 Friction thermal sca. tstar : -0.63224E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.52677E-04 0.11239E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11263E-04 0.24052E-02 Friction velocity uk : 0.11263E-04 0.24052E-02 Dimensionless distance yplus : 0.75002E-04 0.16002E-01 Friction thermal sca. tstar : -0.63224E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.52677E-04 0.11239E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34571E-08 3 0.19398E-06 0.31007E-12 0.11274E+01 c Velocity[X] 0.13887E-31 c Velocity[Y] 0.15504E-12 c Velocity[Z] 0.15504E-12 c Pressure 0.12387E-13 20 0.96622E-07 0.96622E-07 0.13549E+01 c k 0.42647E-06 2 0.50042E-07 0.45025E-08 0.17236E+01 c omega 0.13153E+02 1 0.19305E-08 0.49795E+00 0.36737E-02 c TempK 0.94597E+02 1 0.12850E-06 0.29690E-01 0.19098E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.0635e-13 8.8536e-14 -1.0947e-17 -2.8188e-18 v Velocity[Y] -0.000132 0.00012716 -9.7643e-10 -3.7072e-12 v Velocity[Z] -0.00012715 0.000132 7.5095e-10 -1.3811e-12 v ǁVelocityǁ 8.5835e-10 0.00014131 1.0498e-05 6.7469e-06 v Pressure -0.0010024 0.019649 0.0010796 -5.9028e-20 v k 1.5058e-09 0.0013836 0.00095161 0.001197 v omega 17.206 1.0313e+05 2668 501.76 v TempK 288 341.94 293.58 290.62 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.7671e-14 9.6912e-05 6.0811e-05 7.8776e-05 v CourantNb 2.268e-09 0.00021917 1.393e-05 7.8909e-06 v FourierNb 0.11432 0.6281 0.19518 0.16596 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9425 4.9425 0.00049921 -4.9101e-07 v volume_forces[Z] -4.9425 4.9425 -0.00049907 5.8849e-07 v ǁvolume_forcesǁ 3.1179e-08 4.9438 0.50586 0.23609 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.79 290.77 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.016002 5.6535e-05 3.172e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.11432 0.6281 0.19519 0.16597 INSTANT 0.572022000E+00 TIME STEP NUMBER 594 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11234E-04 0.24043E-02 Friction velocity uk : 0.11235E-04 0.24043E-02 Dimensionless distance yplus : 0.74811E-04 0.15996E-01 Friction thermal sca. tstar : -0.53385E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.52542E-04 0.11235E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11234E-04 0.24043E-02 Friction velocity uk : 0.11235E-04 0.24043E-02 Dimensionless distance yplus : 0.74811E-04 0.15996E-01 Friction thermal sca. tstar : -0.53385E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.52542E-04 0.11235E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34578E-08 3 0.19190E-06 0.30943E-12 0.11263E+01 c Velocity[X] 0.13827E-31 c Velocity[Y] 0.15471E-12 c Velocity[Z] 0.15472E-12 c Pressure 0.12256E-13 20 0.95600E-07 0.95600E-07 0.13525E+01 c k 0.42578E-06 2 0.49931E-07 0.44757E-08 0.17213E+01 c omega 0.13153E+02 1 0.19241E-08 0.49519E+00 0.36635E-02 c TempK 0.94598E+02 1 0.12820E-06 0.29615E-01 0.19074E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.0626e-13 8.8469e-14 -1.0939e-17 -2.8168e-18 v Velocity[Y] -0.00013193 0.00012709 -9.7507e-10 -3.7e-12 v Velocity[Z] -0.00012708 0.00013193 7.4921e-10 -1.3828e-12 v ǁVelocityǁ 8.5412e-10 0.00014124 1.0501e-05 6.7525e-06 v Pressure -0.001004 0.019666 0.0010807 -9.5356e-20 v k 1.4992e-09 0.0013815 0.00094994 0.001195 v omega 17.183 1.0313e+05 2667.9 501.74 v TempK 288 341.94 293.58 290.63 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.7594e-14 9.6899e-05 6.0787e-05 7.8749e-05 v CourantNb 2.2714e-09 0.00021902 1.3928e-05 7.8936e-06 v FourierNb 0.11424 0.6281 0.19513 0.16591 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9426 4.9426 0.00049946 -4.9141e-07 v volume_forces[Z] -4.9426 4.9426 -0.00049932 5.8894e-07 v ǁvolume_forcesǁ 3.1029e-08 4.9439 0.50612 0.23629 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.79 290.77 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015996 5.6517e-05 3.1709e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.11424 0.6281 0.19514 0.16592 INSTANT 0.572985000E+00 TIME STEP NUMBER 595 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11205E-04 0.24034E-02 Friction velocity uk : 0.11205E-04 0.24034E-02 Dimensionless distance yplus : 0.74616E-04 0.15990E-01 Friction thermal sca. tstar : -0.47060E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.52405E-04 0.11230E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11205E-04 0.24034E-02 Friction velocity uk : 0.11205E-04 0.24034E-02 Dimensionless distance yplus : 0.74616E-04 0.15990E-01 Friction thermal sca. tstar : -0.47060E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.52405E-04 0.11230E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34585E-08 3 0.19109E-06 0.30879E-12 0.11252E+01 c Velocity[X] 0.13752E-31 c Velocity[Y] 0.15439E-12 c Velocity[Z] 0.15440E-12 c Pressure 0.12204E-13 20 0.95191E-07 0.95191E-07 0.13501E+01 c k 0.42509E-06 2 0.49820E-07 0.44492E-08 0.17190E+01 c omega 0.13153E+02 1 0.19177E-08 0.49246E+00 0.36533E-02 c TempK 0.94599E+02 1 0.12789E-06 0.29541E-01 0.19050E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.0618e-13 8.8401e-14 -1.0931e-17 -2.8148e-18 v Velocity[Y] -0.00013187 0.00012702 -9.737e-10 -3.6928e-12 v Velocity[Z] -0.000127 0.00013187 7.4747e-10 -1.3846e-12 v ǁVelocityǁ 8.4987e-10 0.00014117 1.0503e-05 6.7582e-06 v Pressure -0.0010057 0.019682 0.0010819 2.8828e-20 v k 1.4926e-09 0.0013795 0.00094828 0.001193 v omega 17.159 1.0313e+05 2667.9 501.72 v TempK 288 341.95 293.58 290.63 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.7517e-14 9.6885e-05 6.0763e-05 7.8722e-05 v CourantNb 2.2749e-09 0.00021887 1.3926e-05 7.8963e-06 v FourierNb 0.11415 0.6281 0.19507 0.16586 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9427 4.9427 0.00049972 -4.9181e-07 v volume_forces[Z] -4.9427 4.9427 -0.00049958 5.8938e-07 v ǁvolume_forcesǁ 3.0876e-08 4.9439 0.50638 0.23649 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.8 290.77 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.01599 5.6499e-05 3.1698e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.11416 0.6281 0.19509 0.16587 INSTANT 0.573948000E+00 TIME STEP NUMBER 596 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11175E-04 0.24025E-02 Friction velocity uk : 0.11176E-04 0.24025E-02 Dimensionless distance yplus : 0.74419E-04 0.15984E-01 Friction thermal sca. tstar : -0.42555E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.52267E-04 0.11226E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11175E-04 0.24025E-02 Friction velocity uk : 0.11176E-04 0.24025E-02 Dimensionless distance yplus : 0.74419E-04 0.15984E-01 Friction thermal sca. tstar : -0.42555E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.52267E-04 0.11226E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34592E-08 3 0.19293E-06 0.30816E-12 0.11242E+01 c Velocity[X] 0.13682E-31 c Velocity[Y] 0.15408E-12 c Velocity[Z] 0.15408E-12 c Pressure 0.12174E-13 20 0.94951E-07 0.94951E-07 0.13477E+01 c k 0.42440E-06 2 0.49709E-07 0.44228E-08 0.17167E+01 c omega 0.13153E+02 1 0.19114E-08 0.48974E+00 0.36433E-02 c TempK 0.94599E+02 1 0.12759E-06 0.29467E-01 0.19026E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.061e-13 8.8334e-14 -1.0923e-17 -2.8129e-18 v Velocity[Y] -0.0001318 0.00012695 -9.7232e-10 -3.6858e-12 v Velocity[Z] -0.00012693 0.0001318 7.4573e-10 -1.3864e-12 v ǁVelocityǁ 8.4559e-10 0.0001411 1.0505e-05 6.7639e-06 v Pressure -0.0010074 0.019698 0.001083 -1.0884e-20 v k 1.4861e-09 0.0013774 0.00094662 0.001191 v omega 17.136 1.0313e+05 2667.9 501.7 v TempK 288 341.95 293.59 290.63 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.744e-14 9.6872e-05 6.0739e-05 7.8695e-05 v CourantNb 2.2784e-09 0.00021871 1.3924e-05 7.899e-06 v FourierNb 0.11402 0.6281 0.19502 0.16581 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9427 4.9428 0.00049998 -4.9221e-07 v volume_forces[Z] -4.9427 4.9428 -0.00049984 5.8983e-07 v ǁvolume_forcesǁ 3.0723e-08 4.944 0.50664 0.23669 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.8 290.77 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015984 5.648e-05 3.1687e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.11407 0.6281 0.19503 0.16582 INSTANT 0.574911000E+00 TIME STEP NUMBER 597 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11145E-04 0.24016E-02 Friction velocity uk : 0.11146E-04 0.24016E-02 Dimensionless distance yplus : 0.74220E-04 0.15978E-01 Friction thermal sca. tstar : -0.39136E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.52128E-04 0.11222E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11145E-04 0.24016E-02 Friction velocity uk : 0.11146E-04 0.24016E-02 Dimensionless distance yplus : 0.74220E-04 0.15978E-01 Friction thermal sca. tstar : -0.39136E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.52128E-04 0.11222E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34599E-08 3 0.19009E-06 0.30752E-12 0.11231E+01 c Velocity[X] 0.13615E-31 c Velocity[Y] 0.15376E-12 c Velocity[Z] 0.15376E-12 c Pressure 0.12146E-13 17 0.94731E-07 0.94731E-07 0.13454E+01 c k 0.42372E-06 2 0.49599E-07 0.43965E-08 0.17144E+01 c omega 0.13153E+02 1 0.19051E-08 0.48704E+00 0.36332E-02 c TempK 0.94600E+02 1 0.12729E-06 0.29394E-01 0.19002E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.0601e-13 8.8266e-14 -1.0915e-17 -2.8109e-18 v Velocity[Y] -0.00013173 0.00012688 -9.7094e-10 -3.684e-12 v Velocity[Z] -0.00012686 0.00013174 7.4393e-10 -1.4258e-12 v ǁVelocityǁ 8.4125e-10 0.00014102 1.0508e-05 6.7696e-06 v Pressure -0.0010091 0.019715 0.0010842 1.8483e-20 v k 1.4796e-09 0.0013754 0.00094497 0.001189 v omega 17.113 1.0313e+05 2667.9 501.68 v TempK 288 341.95 293.59 290.63 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.7364e-14 9.6859e-05 6.0714e-05 7.8668e-05 v CourantNb 2.2819e-09 0.00021856 1.3922e-05 7.9017e-06 v FourierNb 0.11389 0.6281 0.19497 0.16576 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9428 4.9428 0.00050024 -4.926e-07 v volume_forces[Z] -4.9428 4.9428 -0.0005001 5.9027e-07 v ǁvolume_forcesǁ 3.0568e-08 4.9441 0.50689 0.23689 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.8 290.78 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015978 5.6462e-05 3.1675e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.11393 0.6281 0.19498 0.16577 INSTANT 0.575874000E+00 TIME STEP NUMBER 598 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11115E-04 0.24007E-02 Friction velocity uk : 0.11116E-04 0.24007E-02 Dimensionless distance yplus : 0.74018E-04 0.15972E-01 Friction thermal sca. tstar : -0.36428E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.51985E-04 0.11218E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11115E-04 0.24007E-02 Friction velocity uk : 0.11116E-04 0.24007E-02 Dimensionless distance yplus : 0.74018E-04 0.15972E-01 Friction thermal sca. tstar : -0.36428E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.51985E-04 0.11218E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34607E-08 3 0.18958E-06 0.30689E-12 0.11220E+01 c Velocity[X] 0.13548E-31 c Velocity[Y] 0.15344E-12 c Velocity[Z] 0.15345E-12 c Pressure 0.12118E-13 17 0.94514E-07 0.94514E-07 0.13430E+01 c k 0.42303E-06 2 0.49489E-07 0.43705E-08 0.17121E+01 c omega 0.13153E+02 1 0.18989E-08 0.48436E+00 0.36232E-02 c TempK 0.94600E+02 1 0.12699E-06 0.29321E-01 0.18978E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.0593e-13 8.8199e-14 -1.0907e-17 -2.809e-18 v Velocity[Y] -0.00013167 0.00012681 -9.6955e-10 -3.6783e-12 v Velocity[Z] -0.00012679 0.00013167 7.4218e-10 -1.4275e-12 v ǁVelocityǁ 8.3696e-10 0.00014095 1.051e-05 6.7753e-06 v Pressure -0.0010108 0.019731 0.0010853 1.6277e-20 v k 1.4732e-09 0.0013733 0.00094333 0.001187 v omega 17.09 1.0313e+05 2667.9 501.66 v TempK 288 341.95 293.59 290.63 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.7288e-14 9.6845e-05 6.069e-05 7.864e-05 v CourantNb 2.2855e-09 0.00021841 1.392e-05 7.9045e-06 v FourierNb 0.11376 0.6281 0.19492 0.16571 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9429 4.9429 0.0005005 -4.93e-07 v volume_forces[Z] -4.9429 4.9429 -0.00050036 5.9071e-07 v ǁvolume_forcesǁ 3.0411e-08 4.9442 0.50715 0.23709 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.81 290.78 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015972 5.6443e-05 3.1664e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.11381 0.6281 0.19493 0.16572 INSTANT 0.576837000E+00 TIME STEP NUMBER 599 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11085E-04 0.23998E-02 Friction velocity uk : 0.11085E-04 0.23998E-02 Dimensionless distance yplus : 0.73817E-04 0.15966E-01 Friction thermal sca. tstar : -0.34213E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.51844E-04 0.11214E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11085E-04 0.23998E-02 Friction velocity uk : 0.11085E-04 0.23998E-02 Dimensionless distance yplus : 0.73817E-04 0.15966E-01 Friction thermal sca. tstar : -0.34213E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.51844E-04 0.11214E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34614E-08 3 0.18910E-06 0.30626E-12 0.11209E+01 c Velocity[X] 0.13483E-31 c Velocity[Y] 0.15313E-12 c Velocity[Z] 0.15313E-12 c Pressure 0.12093E-13 17 0.94314E-07 0.94314E-07 0.13407E+01 c k 0.42235E-06 2 0.49380E-07 0.43447E-08 0.17098E+01 c omega 0.13153E+02 1 0.18926E-08 0.48169E+00 0.36132E-02 c TempK 0.94601E+02 1 0.12669E-06 0.29248E-01 0.18954E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.0585e-13 8.8132e-14 -1.0899e-17 -2.807e-18 v Velocity[Y] -0.0001316 0.00012674 -9.6815e-10 -3.6705e-12 v Velocity[Z] -0.00012672 0.00013161 7.4041e-10 -1.4291e-12 v ǁVelocityǁ 8.3264e-10 0.00014088 1.0513e-05 6.781e-06 v Pressure -0.0010125 0.019747 0.0010865 2.8435e-20 v k 1.4668e-09 0.0013713 0.00094169 0.001185 v omega 17.067 1.0313e+05 2667.9 501.64 v TempK 288 341.95 293.6 290.64 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.7213e-14 9.6832e-05 6.0666e-05 7.8613e-05 v CourantNb 2.2889e-09 0.00021826 1.3918e-05 7.9072e-06 v FourierNb 0.11363 0.6281 0.19486 0.16566 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.943 4.943 0.00050075 -4.9339e-07 v volume_forces[Z] -4.943 4.943 -0.00050061 5.9115e-07 v ǁvolume_forcesǁ 3.0256e-08 4.9442 0.50741 0.23729 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.81 290.78 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015966 5.6425e-05 3.1653e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.11368 0.6281 0.19488 0.16567 INSTANT 0.577800000E+00 TIME STEP NUMBER 600 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11054E-04 0.23990E-02 Friction velocity uk : 0.11055E-04 0.23989E-02 Dimensionless distance yplus : 0.73615E-04 0.15960E-01 Friction thermal sca. tstar : -0.33286E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.51702E-04 0.11209E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11054E-04 0.23990E-02 Friction velocity uk : 0.11055E-04 0.23989E-02 Dimensionless distance yplus : 0.73615E-04 0.15960E-01 Friction thermal sca. tstar : -0.33286E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.51702E-04 0.11209E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34621E-08 3 0.18858E-06 0.30563E-12 0.11199E+01 c Velocity[X] 0.13418E-31 c Velocity[Y] 0.15281E-12 c Velocity[Z] 0.15282E-12 c Pressure 0.12063E-13 17 0.94079E-07 0.94079E-07 0.13383E+01 c k 0.42167E-06 2 0.49271E-07 0.43191E-08 0.17075E+01 c omega 0.13153E+02 1 0.18864E-08 0.47905E+00 0.36033E-02 c TempK 0.94602E+02 1 0.12639E-06 0.29175E-01 0.18931E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.0576e-13 8.8065e-14 -1.0891e-17 -2.8051e-18 v Velocity[Y] -0.00013154 0.00012667 -9.6674e-10 -3.6634e-12 v Velocity[Z] -0.00012665 0.00013154 7.3865e-10 -1.4308e-12 v ǁVelocityǁ 8.2831e-10 0.00014081 1.0515e-05 6.7867e-06 v Pressure -0.0010142 0.019764 0.0010876 3.7456e-20 v k 1.4604e-09 0.0013693 0.00094005 0.001183 v omega 17.044 1.0313e+05 2667.8 501.62 v TempK 288 341.95 293.6 290.64 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.7138e-14 9.6819e-05 6.0642e-05 7.8586e-05 v CourantNb 2.2924e-09 0.00021811 1.3916e-05 7.9099e-06 v FourierNb 0.1135 0.6281 0.19481 0.16561 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.943 4.9431 0.00050101 -4.9378e-07 v volume_forces[Z] -4.943 4.9431 -0.00050087 5.9159e-07 v ǁvolume_forcesǁ 3.01e-08 4.9443 0.50766 0.23749 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.81 290.78 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.01596 5.6407e-05 3.1642e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.11355 0.6281 0.19483 0.16562 INSTANT 0.578763000E+00 TIME STEP NUMBER 601 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11024E-04 0.23981E-02 Friction velocity uk : 0.11024E-04 0.23980E-02 Dimensionless distance yplus : 0.73411E-04 0.15954E-01 Friction thermal sca. tstar : -0.35103E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.51559E-04 0.11205E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11024E-04 0.23981E-02 Friction velocity uk : 0.11024E-04 0.23980E-02 Dimensionless distance yplus : 0.73411E-04 0.15954E-01 Friction thermal sca. tstar : -0.35103E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.51559E-04 0.11205E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34629E-08 3 0.18805E-06 0.30500E-12 0.11188E+01 c Velocity[X] 0.13352E-31 c Velocity[Y] 0.15250E-12 c Velocity[Z] 0.15250E-12 c Pressure 0.12031E-13 17 0.93824E-07 0.93824E-07 0.13360E+01 c k 0.42100E-06 2 0.49162E-07 0.42936E-08 0.17052E+01 c omega 0.13153E+02 1 0.18802E-08 0.47642E+00 0.35934E-02 c TempK 0.94602E+02 1 0.12610E-06 0.29103E-01 0.18907E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.0568e-13 8.7999e-14 -1.0882e-17 -2.8031e-18 v Velocity[Y] -0.00013148 0.0001266 -9.6533e-10 -3.6563e-12 v Velocity[Z] -0.00012658 0.00013148 7.3687e-10 -1.4325e-12 v ǁVelocityǁ 8.2396e-10 0.00014074 1.0518e-05 6.7924e-06 v Pressure -0.0010158 0.01978 0.0010887 5.4223e-20 v k 1.4541e-09 0.0013672 0.00093842 0.0011811 v omega 17.021 1.0313e+05 2667.8 501.6 v TempK 288 341.95 293.6 290.64 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.7064e-14 9.6805e-05 6.0618e-05 7.8559e-05 v CourantNb 2.2959e-09 0.00021797 1.3914e-05 7.9127e-06 v FourierNb 0.11337 0.6281 0.19476 0.16556 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9431 4.9431 0.00050127 -4.9417e-07 v volume_forces[Z] -4.9431 4.9431 -0.00050113 5.9203e-07 v ǁvolume_forcesǁ 2.9943e-08 4.9444 0.50792 0.23769 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.81 290.78 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015954 5.6388e-05 3.1631e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.11342 0.6281 0.19477 0.16557 INSTANT 0.579726000E+00 TIME STEP NUMBER 602 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10993E-04 0.23972E-02 Friction velocity uk : 0.10994E-04 0.23971E-02 Dimensionless distance yplus : 0.73205E-04 0.15948E-01 Friction thermal sca. tstar : -0.37254E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.51415E-04 0.11201E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10993E-04 0.23972E-02 Friction velocity uk : 0.10994E-04 0.23971E-02 Dimensionless distance yplus : 0.73205E-04 0.15948E-01 Friction thermal sca. tstar : -0.37254E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.51415E-04 0.11201E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34636E-08 3 0.18755E-06 0.30438E-12 0.11177E+01 c Velocity[X] 0.13288E-31 c Velocity[Y] 0.15219E-12 c Velocity[Z] 0.15219E-12 c Pressure 0.12000E-13 17 0.93586E-07 0.93586E-07 0.13337E+01 c k 0.42032E-06 2 0.49054E-07 0.42683E-08 0.17029E+01 c omega 0.13153E+02 1 0.18741E-08 0.47381E+00 0.35835E-02 c TempK 0.94603E+02 1 0.12580E-06 0.29031E-01 0.18883E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.056e-13 8.7932e-14 -1.0874e-17 -2.8012e-18 v Velocity[Y] -0.00013141 0.00012653 -9.6391e-10 -3.6493e-12 v Velocity[Z] -0.00012651 0.00013141 7.3509e-10 -1.4341e-12 v ǁVelocityǁ 8.1959e-10 0.00014067 1.052e-05 6.7981e-06 v Pressure -0.0010175 0.019796 0.0010899 -2.4954e-20 v k 1.4478e-09 0.0013652 0.00093679 0.0011791 v omega 16.998 1.0313e+05 2667.8 501.58 v TempK 288 341.95 293.6 290.64 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.699e-14 9.6792e-05 6.0595e-05 7.8532e-05 v CourantNb 2.2994e-09 0.00021782 1.3912e-05 7.9154e-06 v FourierNb 0.11325 0.6281 0.19471 0.16551 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9432 4.9432 0.00050152 -4.9457e-07 v volume_forces[Z] -4.9432 4.9432 -0.00050138 5.9247e-07 v ǁvolume_forcesǁ 2.9786e-08 4.9445 0.50818 0.23788 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.82 290.79 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015948 5.637e-05 3.162e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.11329 0.6281 0.19472 0.16552 INSTANT 0.580689000E+00 TIME STEP NUMBER 603 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10962E-04 0.23963E-02 Friction velocity uk : 0.10963E-04 0.23962E-02 Dimensionless distance yplus : 0.72999E-04 0.15942E-01 Friction thermal sca. tstar : -0.39856E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.51270E-04 0.11197E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10962E-04 0.23963E-02 Friction velocity uk : 0.10963E-04 0.23962E-02 Dimensionless distance yplus : 0.72999E-04 0.15942E-01 Friction thermal sca. tstar : -0.39856E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.51270E-04 0.11197E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34644E-08 3 0.18709E-06 0.30376E-12 0.11167E+01 c Velocity[X] 0.13223E-31 c Velocity[Y] 0.15188E-12 c Velocity[Z] 0.15188E-12 c Pressure 0.12074E-13 17 0.94159E-07 0.94159E-07 0.13314E+01 c k 0.41965E-06 2 0.48946E-07 0.42432E-08 0.17006E+01 c omega 0.13153E+02 1 0.18680E-08 0.47122E+00 0.35737E-02 c TempK 0.94603E+02 1 0.12551E-06 0.28959E-01 0.18860E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.0552e-13 8.7866e-14 -1.0866e-17 -2.7992e-18 v Velocity[Y] -0.00013135 0.00012646 -9.6248e-10 -3.6423e-12 v Velocity[Z] -0.00012644 0.00013135 7.3331e-10 -1.4357e-12 v ǁVelocityǁ 8.1521e-10 0.0001406 1.0523e-05 6.8038e-06 v Pressure -0.0010192 0.019813 0.001091 7.5991e-20 v k 1.4416e-09 0.0013632 0.00093517 0.0011772 v omega 16.975 1.0313e+05 2667.8 501.56 v TempK 288 341.95 293.61 290.65 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.6917e-14 9.6779e-05 6.0571e-05 7.8505e-05 v CourantNb 2.3029e-09 0.00021767 1.3911e-05 7.9182e-06 v FourierNb 0.11312 0.6281 0.19466 0.16546 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9433 4.9433 0.00050178 -4.9496e-07 v volume_forces[Z] -4.9433 4.9433 -0.00050164 5.9291e-07 v ǁvolume_forcesǁ 2.9628e-08 4.9445 0.50843 0.23808 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.82 290.79 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015942 5.6352e-05 3.1609e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.11316 0.6281 0.19467 0.16547 INSTANT 0.581652000E+00 TIME STEP NUMBER 604 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10931E-04 0.23954E-02 Friction velocity uk : 0.10931E-04 0.23953E-02 Dimensionless distance yplus : 0.72791E-04 0.15936E-01 Friction thermal sca. tstar : -0.43092E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.51123E-04 0.11193E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10931E-04 0.23954E-02 Friction velocity uk : 0.10931E-04 0.23953E-02 Dimensionless distance yplus : 0.72791E-04 0.15936E-01 Friction thermal sca. tstar : -0.43092E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.51123E-04 0.11193E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34652E-08 3 0.18655E-06 0.30314E-12 0.11156E+01 c Velocity[X] 0.13159E-31 c Velocity[Y] 0.15157E-12 c Velocity[Z] 0.15157E-12 c Pressure 0.11947E-13 17 0.93169E-07 0.93169E-07 0.13291E+01 c k 0.41898E-06 2 0.48839E-07 0.42183E-08 0.16984E+01 c omega 0.13153E+02 1 0.18619E-08 0.46865E+00 0.35640E-02 c TempK 0.94604E+02 1 0.12522E-06 0.28888E-01 0.18837E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.0544e-13 8.78e-14 -1.0858e-17 -2.7973e-18 v Velocity[Y] -0.00013128 0.00012639 -9.6105e-10 -3.6353e-12 v Velocity[Z] -0.00012637 0.00013129 7.3152e-10 -1.4373e-12 v ǁVelocityǁ 8.1082e-10 0.00014053 1.0525e-05 6.8095e-06 v Pressure -0.0010209 0.019829 0.0010921 7.153e-20 v k 1.4353e-09 0.0013612 0.00093356 0.0011752 v omega 16.953 1.0313e+05 2667.8 501.54 v TempK 288 341.95 293.61 290.65 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.6844e-14 9.6766e-05 6.0547e-05 7.8479e-05 v CourantNb 2.3064e-09 0.00021752 1.3909e-05 7.921e-06 v FourierNb 0.11299 0.6281 0.1946 0.16541 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9433 4.9434 0.00050203 -4.9535e-07 v volume_forces[Z] -4.9433 4.9434 -0.0005019 5.9335e-07 v ǁvolume_forcesǁ 2.947e-08 4.9446 0.50869 0.23828 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.82 290.79 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015936 5.6333e-05 3.1597e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.11304 0.6281 0.19462 0.16542 INSTANT 0.582615000E+00 TIME STEP NUMBER 605 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10899E-04 0.23945E-02 Friction velocity uk : 0.10900E-04 0.23945E-02 Dimensionless distance yplus : 0.72581E-04 0.15931E-01 Friction thermal sca. tstar : -0.47271E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.50976E-04 0.11189E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10899E-04 0.23945E-02 Friction velocity uk : 0.10900E-04 0.23945E-02 Dimensionless distance yplus : 0.72581E-04 0.15931E-01 Friction thermal sca. tstar : -0.47271E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.50976E-04 0.11189E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34659E-08 3 0.18609E-06 0.30252E-12 0.11145E+01 c Velocity[X] 0.13096E-31 c Velocity[Y] 0.15126E-12 c Velocity[Z] 0.15126E-12 c Pressure 0.11947E-13 17 0.93162E-07 0.93162E-07 0.13268E+01 c k 0.41831E-06 2 0.48732E-07 0.41936E-08 0.16961E+01 c omega 0.13153E+02 1 0.18558E-08 0.46609E+00 0.35542E-02 c TempK 0.94605E+02 1 0.12492E-06 0.28817E-01 0.18813E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.0535e-13 8.7733e-14 -1.085e-17 -2.7954e-18 v Velocity[Y] -0.00013122 0.00012632 -9.5961e-10 -3.6283e-12 v Velocity[Z] -0.0001263 0.00013122 7.2972e-10 -1.439e-12 v ǁVelocityǁ 8.0641e-10 0.00014046 1.0528e-05 6.8153e-06 v Pressure -0.0010226 0.019845 0.0010933 1.7159e-21 v k 1.4292e-09 0.0013592 0.00093195 0.0011733 v omega 16.93 1.0313e+05 2667.8 501.52 v TempK 288 341.95 293.61 290.65 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.6771e-14 9.6752e-05 6.0523e-05 7.8452e-05 v CourantNb 2.3099e-09 0.00021737 1.3907e-05 7.9238e-06 v FourierNb 0.11287 0.6281 0.19455 0.16536 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9434 4.9434 0.00050229 -4.9574e-07 v volume_forces[Z] -4.9434 4.9434 -0.00050215 5.9378e-07 v ǁvolume_forcesǁ 2.9311e-08 4.9447 0.50894 0.23848 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.83 290.79 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015931 5.6315e-05 3.1586e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.11291 0.6281 0.19457 0.16537 INSTANT 0.583578000E+00 TIME STEP NUMBER 606 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10867E-04 0.23936E-02 Friction velocity uk : 0.10868E-04 0.23936E-02 Dimensionless distance yplus : 0.72370E-04 0.15925E-01 Friction thermal sca. tstar : -0.52960E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.50828E-04 0.11185E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10867E-04 0.23936E-02 Friction velocity uk : 0.10868E-04 0.23936E-02 Dimensionless distance yplus : 0.72370E-04 0.15925E-01 Friction thermal sca. tstar : -0.52960E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.50828E-04 0.11185E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34667E-08 3 0.18557E-06 0.30190E-12 0.11134E+01 c Velocity[X] 0.13033E-31 c Velocity[Y] 0.15095E-12 c Velocity[Z] 0.15095E-12 c Pressure 0.11948E-13 17 0.93171E-07 0.93171E-07 0.13245E+01 c k 0.41764E-06 2 0.48626E-07 0.41691E-08 0.16939E+01 c omega 0.13153E+02 1 0.18498E-08 0.46355E+00 0.35445E-02 c TempK 0.94605E+02 1 0.12463E-06 0.28746E-01 0.18790E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.0527e-13 8.7668e-14 -1.0842e-17 -2.7935e-18 v Velocity[Y] -0.00013116 0.00012625 -9.5816e-10 -3.6214e-12 v Velocity[Z] -0.00012624 0.00013116 7.2792e-10 -1.4406e-12 v ǁVelocityǁ 8.0199e-10 0.00014039 1.053e-05 6.821e-06 v Pressure -0.0010243 0.019861 0.0010944 1.1958e-19 v k 1.423e-09 0.0013572 0.00093034 0.0011713 v omega 16.907 1.0313e+05 2667.7 501.5 v TempK 288 341.95 293.62 290.65 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.6699e-14 9.6739e-05 6.0499e-05 7.8425e-05 v CourantNb 2.3133e-09 0.00021723 1.3905e-05 7.9266e-06 v FourierNb 0.11274 0.6281 0.1945 0.16532 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9435 4.9435 0.00050255 -4.9612e-07 v volume_forces[Z] -4.9435 4.9435 -0.00050241 5.9422e-07 v ǁvolume_forcesǁ 2.9152e-08 4.9447 0.50919 0.23867 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.83 290.8 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015925 5.6297e-05 3.1575e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.11278 0.6281 0.19452 0.16532 INSTANT 0.584541000E+00 TIME STEP NUMBER 607 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10836E-04 0.23928E-02 Friction velocity uk : 0.10836E-04 0.23927E-02 Dimensionless distance yplus : 0.72158E-04 0.15919E-01 Friction thermal sca. tstar : -0.61365E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.50679E-04 0.11180E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10836E-04 0.23928E-02 Friction velocity uk : 0.10836E-04 0.23927E-02 Dimensionless distance yplus : 0.72158E-04 0.15919E-01 Friction thermal sca. tstar : -0.61365E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.50679E-04 0.11180E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34675E-08 3 0.18503E-06 0.30129E-12 0.11124E+01 c Velocity[X] 0.12970E-31 c Velocity[Y] 0.15064E-12 c Velocity[Z] 0.15065E-12 c Pressure 0.11871E-13 17 0.92565E-07 0.92565E-07 0.13222E+01 c k 0.41698E-06 2 0.48519E-07 0.41447E-08 0.16916E+01 c omega 0.13153E+02 1 0.18437E-08 0.46103E+00 0.35349E-02 c TempK 0.94606E+02 1 0.12434E-06 0.28675E-01 0.18767E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.0519e-13 8.7602e-14 -1.0834e-17 -2.7916e-18 v Velocity[Y] -0.00013109 0.00012618 -9.5671e-10 -3.6145e-12 v Velocity[Z] -0.00012617 0.00013109 7.2611e-10 -1.4422e-12 v ǁVelocityǁ 7.9755e-10 0.00014032 1.0533e-05 6.8268e-06 v Pressure -0.001026 0.019878 0.0010955 9.5798e-20 v k 1.4169e-09 0.0013552 0.00092874 0.0011694 v omega 16.885 1.0313e+05 2667.7 501.48 v TempK 288 341.95 293.62 290.66 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.6627e-14 9.6726e-05 6.0476e-05 7.8398e-05 v CourantNb 2.3168e-09 0.00021708 1.3904e-05 7.9294e-06 v FourierNb 0.11261 0.6281 0.19445 0.16527 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9436 4.9436 0.0005028 -4.9651e-07 v volume_forces[Z] -4.9436 4.9436 -0.00050266 5.9465e-07 v ǁvolume_forcesǁ 2.8992e-08 4.9448 0.50945 0.23887 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.83 290.8 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015919 5.6278e-05 3.1564e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.11266 0.6281 0.19446 0.16527 INSTANT 0.585504000E+00 TIME STEP NUMBER 608 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10804E-04 0.23919E-02 Friction velocity uk : 0.10804E-04 0.23918E-02 Dimensionless distance yplus : 0.71945E-04 0.15913E-01 Friction thermal sca. tstar : -0.75684E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.50529E-04 0.11176E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10804E-04 0.23919E-02 Friction velocity uk : 0.10804E-04 0.23918E-02 Dimensionless distance yplus : 0.71945E-04 0.15913E-01 Friction thermal sca. tstar : -0.75684E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.50529E-04 0.11176E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34683E-08 3 0.18455E-06 0.30067E-12 0.11113E+01 c Velocity[X] 0.12908E-31 c Velocity[Y] 0.15034E-12 c Velocity[Z] 0.15034E-12 c Pressure 0.11836E-13 17 0.92290E-07 0.92290E-07 0.13199E+01 c k 0.41631E-06 2 0.48414E-07 0.41205E-08 0.16894E+01 c omega 0.13153E+02 1 0.18378E-08 0.45853E+00 0.35253E-02 c TempK 0.94606E+02 1 0.12406E-06 0.28605E-01 0.18744E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.0511e-13 8.7536e-14 -1.0826e-17 -2.7896e-18 v Velocity[Y] -0.00013103 0.00012612 -9.5525e-10 -3.6075e-12 v Velocity[Z] -0.0001261 0.00013103 7.243e-10 -1.4438e-12 v ǁVelocityǁ 7.931e-10 0.00014025 1.0535e-05 6.8325e-06 v Pressure -0.0010276 0.019894 0.0010967 7.5648e-20 v k 1.4108e-09 0.0013532 0.00092715 0.0011675 v omega 16.862 1.0313e+05 2667.7 501.46 v TempK 288 341.96 293.62 290.66 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.6556e-14 9.6713e-05 6.0452e-05 7.8371e-05 v CourantNb 2.3203e-09 0.00021693 1.3902e-05 7.9322e-06 v FourierNb 0.11249 0.6281 0.1944 0.16522 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9436 4.9436 0.00050305 -4.969e-07 v volume_forces[Z] -4.9436 4.9436 -0.00050291 5.9509e-07 v ǁvolume_forcesǁ 2.8831e-08 4.9449 0.5097 0.23907 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.83 290.8 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015913 5.626e-05 3.1553e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.11253 0.6281 0.19441 0.16523 INSTANT 0.586467000E+00 TIME STEP NUMBER 609 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10771E-04 0.23910E-02 Friction velocity uk : 0.10772E-04 0.23910E-02 Dimensionless distance yplus : 0.71730E-04 0.15907E-01 Friction thermal sca. tstar : -0.10936E+05 0.00000E+00 Dim-less thermal sca. tplus : 0.50378E-04 0.11172E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10771E-04 0.23910E-02 Friction velocity uk : 0.10772E-04 0.23910E-02 Dimensionless distance yplus : 0.71730E-04 0.15907E-01 Friction thermal sca. tstar : -0.10936E+05 0.00000E+00 Dim-less thermal sca. tplus : 0.50378E-04 0.11172E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34691E-08 3 0.18405E-06 0.30006E-12 0.11102E+01 c Velocity[X] 0.12846E-31 c Velocity[Y] 0.15003E-12 c Velocity[Z] 0.15003E-12 c Pressure 0.11803E-13 17 0.92036E-07 0.92036E-07 0.13177E+01 c k 0.41565E-06 2 0.48309E-07 0.40965E-08 0.16872E+01 c omega 0.13153E+02 1 0.18318E-08 0.45604E+00 0.35157E-02 c TempK 0.94607E+02 1 0.12377E-06 0.28535E-01 0.18720E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.0503e-13 8.7471e-14 -1.0819e-17 -2.7877e-18 v Velocity[Y] -0.00013097 0.00012605 -9.5379e-10 -3.6006e-12 v Velocity[Z] -0.00012603 0.00013097 7.2248e-10 -1.4452e-12 v ǁVelocityǁ 7.8864e-10 0.00014018 1.0538e-05 6.8383e-06 v Pressure -0.0010293 0.01991 0.0010978 -5.3488e-20 v k 1.4048e-09 0.0013512 0.00092556 0.0011655 v omega 16.84 1.0313e+05 2667.7 501.44 v TempK 288 341.96 293.62 290.66 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.6485e-14 9.67e-05 6.0428e-05 7.8345e-05 v CourantNb 2.3237e-09 0.00021679 1.39e-05 7.935e-06 v FourierNb 0.11236 0.6281 0.19435 0.16517 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9437 4.9437 0.00050331 -4.9728e-07 v volume_forces[Z] -4.9437 4.9437 -0.00050317 5.9552e-07 v ǁvolume_forcesǁ 2.8671e-08 4.945 0.50995 0.23927 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.84 290.8 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015907 5.6241e-05 3.1542e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.11241 0.6281 0.19436 0.16518 INSTANT 0.587430000E+00 TIME STEP NUMBER 610 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.54247E-05 0.23901E-02 Friction velocity uk : 0.54263E-05 0.23901E-02 Dimensionless distance yplus : 0.36110E-04 0.15901E-01 Friction thermal sca. tstar : -0.36852E+05 0.00000E+00 Dim-less thermal sca. tplus : 0.25361E-04 0.11168E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.54247E-05 0.23901E-02 Friction velocity uk : 0.54263E-05 0.23901E-02 Dimensionless distance yplus : 0.36110E-04 0.15901E-01 Friction thermal sca. tstar : -0.36852E+05 0.00000E+00 Dim-less thermal sca. tplus : 0.25361E-04 0.11168E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34699E-08 3 0.18357E-06 0.29945E-12 0.11092E+01 c Velocity[X] 0.12784E-31 c Velocity[Y] 0.14973E-12 c Velocity[Z] 0.14973E-12 c Pressure 0.11772E-13 17 0.91794E-07 0.91794E-07 0.13154E+01 c k 0.41499E-06 2 0.48204E-07 0.40726E-08 0.16849E+01 c omega 0.13153E+02 1 0.18259E-08 0.45357E+00 0.35061E-02 c TempK 0.94608E+02 1 0.12348E-06 0.28465E-01 0.18697E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.0495e-13 8.7405e-14 -1.0811e-17 -2.7858e-18 v Velocity[Y] -0.0001309 0.00012598 -9.5231e-10 -3.5935e-12 v Velocity[Z] -0.00012596 0.00013091 7.2066e-10 -1.4469e-12 v ǁVelocityǁ 7.8416e-10 0.00014011 1.054e-05 6.8441e-06 v Pressure -0.001031 0.019926 0.0010989 1.1139e-19 v k 1.3988e-09 0.0013492 0.00092397 0.0011636 v omega 16.818 1.0313e+05 2667.7 501.42 v TempK 288 341.96 293.63 290.66 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.6414e-14 9.6687e-05 6.0405e-05 7.8318e-05 v CourantNb 2.3272e-09 0.00021664 1.3898e-05 7.9378e-06 v FourierNb 0.11224 0.6281 0.1943 0.16512 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9438 4.9438 0.00050356 -4.9767e-07 v volume_forces[Z] -4.9438 4.9438 -0.00050342 5.9595e-07 v ǁvolume_forcesǁ 2.8509e-08 4.945 0.51021 0.23946 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.84 290.8 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015901 5.6223e-05 3.1531e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.11228 0.6281 0.19431 0.16513 INSTANT 0.588393000E+00 TIME STEP NUMBER 611 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10706E-04 0.23893E-02 Friction velocity uk : 0.10707E-04 0.23892E-02 Dimensionless distance yplus : 0.71296E-04 0.15896E-01 Friction thermal sca. tstar : -0.10085E+05 0.00000E+00 Dim-less thermal sca. tplus : 0.50073E-04 0.11164E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10706E-04 0.23893E-02 Friction velocity uk : 0.10707E-04 0.23892E-02 Dimensionless distance yplus : 0.71296E-04 0.15896E-01 Friction thermal sca. tstar : -0.10085E+05 0.00000E+00 Dim-less thermal sca. tplus : 0.50073E-04 0.11164E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34707E-08 3 0.18306E-06 0.29885E-12 0.11081E+01 c Velocity[X] 0.12723E-31 c Velocity[Y] 0.14942E-12 c Velocity[Z] 0.14943E-12 c Pressure 0.11744E-13 17 0.91570E-07 0.91570E-07 0.13132E+01 c k 0.41434E-06 2 0.48099E-07 0.40490E-08 0.16827E+01 c omega 0.13153E+02 1 0.18200E-08 0.45111E+00 0.34966E-02 c TempK 0.94608E+02 1 0.12320E-06 0.28396E-01 0.18674E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.0487e-13 8.734e-14 -1.0803e-17 -2.7839e-18 v Velocity[Y] -0.00013084 0.00012591 -9.5083e-10 -3.5866e-12 v Velocity[Z] -0.00012589 0.00013084 7.1883e-10 -1.4484e-12 v ǁVelocityǁ 7.7967e-10 0.00014004 1.0543e-05 6.8498e-06 v Pressure -0.0010327 0.019942 0.0011001 1.6375e-20 v k 1.3928e-09 0.0013473 0.00092239 0.0011617 v omega 16.795 1.0313e+05 2667.7 501.4 v TempK 288 341.96 293.63 290.66 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.6344e-14 9.6673e-05 6.0381e-05 7.8291e-05 v CourantNb 2.3307e-09 0.00021649 1.3897e-05 7.9407e-06 v FourierNb 0.11212 0.6281 0.19425 0.16507 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9438 4.9439 0.00050381 -4.9805e-07 v volume_forces[Z] -4.9438 4.9439 -0.00050368 5.9638e-07 v ǁvolume_forcesǁ 2.8347e-08 4.9451 0.51046 0.23966 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.84 290.81 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015896 5.6205e-05 3.152e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.11216 0.6281 0.19426 0.16508 INSTANT 0.589356000E+00 TIME STEP NUMBER 612 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10673E-04 0.23884E-02 Friction velocity uk : 0.10674E-04 0.23883E-02 Dimensionless distance yplus : 0.71076E-04 0.15890E-01 Friction thermal sca. tstar : -0.72683E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.49920E-04 0.11160E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10673E-04 0.23884E-02 Friction velocity uk : 0.10674E-04 0.23883E-02 Dimensionless distance yplus : 0.71076E-04 0.15890E-01 Friction thermal sca. tstar : -0.72683E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.49920E-04 0.11160E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34715E-08 3 0.18259E-06 0.29824E-12 0.11070E+01 c Velocity[X] 0.12662E-31 c Velocity[Y] 0.14912E-12 c Velocity[Z] 0.14912E-12 c Pressure 0.11747E-13 17 0.91595E-07 0.91595E-07 0.13109E+01 c k 0.41368E-06 2 0.47995E-07 0.40254E-08 0.16805E+01 c omega 0.13153E+02 1 0.18141E-08 0.44868E+00 0.34872E-02 c TempK 0.94609E+02 1 0.12291E-06 0.28327E-01 0.18652E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.0479e-13 8.7275e-14 -1.0795e-17 -2.782e-18 v Velocity[Y] -0.00013078 0.00012584 -9.4935e-10 -3.5797e-12 v Velocity[Z] -0.00012583 0.00013078 7.17e-10 -1.45e-12 v ǁVelocityǁ 7.7517e-10 0.00013997 1.0546e-05 6.8556e-06 v Pressure -0.0010344 0.019958 0.0011012 1.0766e-19 v k 1.3869e-09 0.0013453 0.00092081 0.0011598 v omega 16.773 1.0313e+05 2667.7 501.38 v TempK 288 341.96 293.63 290.67 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.6274e-14 9.666e-05 6.0358e-05 7.8265e-05 v CourantNb 2.3341e-09 0.00021635 1.3895e-05 7.9435e-06 v FourierNb 0.11199 0.6281 0.1942 0.16502 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9439 4.9439 0.00050407 -4.9844e-07 v volume_forces[Z] -4.9439 4.9439 -0.00050393 5.9681e-07 v ǁvolume_forcesǁ 2.8185e-08 4.9452 0.51071 0.23986 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.85 290.81 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.01589 5.6188e-05 3.1509e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.11204 0.6281 0.19421 0.16503 INSTANT 0.590319000E+00 TIME STEP NUMBER 613 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+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-04 0.23875E-02 Friction velocity uk : 0.10641E-04 0.23875E-02 Dimensionless distance yplus : 0.70856E-04 0.15884E-01 Friction thermal sca. tstar : -0.59734E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.49765E-04 0.11156E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+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-04 0.23875E-02 Friction velocity uk : 0.10641E-04 0.23875E-02 Dimensionless distance yplus : 0.70856E-04 0.15884E-01 Friction thermal sca. tstar : -0.59734E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.49765E-04 0.11156E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34723E-08 3 0.18259E-06 0.29764E-12 0.11060E+01 c Velocity[X] 0.12600E-31 c Velocity[Y] 0.14882E-12 c Velocity[Z] 0.14882E-12 c Pressure 0.11693E-13 17 0.91172E-07 0.91172E-07 0.13087E+01 c k 0.41303E-06 2 0.47892E-07 0.40021E-08 0.16783E+01 c omega 0.13153E+02 1 0.18082E-08 0.44625E+00 0.34778E-02 c TempK 0.94609E+02 1 0.12263E-06 0.28258E-01 0.18629E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.0471e-13 8.721e-14 -1.0787e-17 -2.7802e-18 v Velocity[Y] -0.00013072 0.00012578 -9.4786e-10 -3.5729e-12 v Velocity[Z] -0.00012576 0.00013072 7.1516e-10 -1.4515e-12 v ǁVelocityǁ 7.7065e-10 0.0001399 1.0548e-05 6.8614e-06 v Pressure -0.0010361 0.019975 0.0011023 4.6771e-20 v k 1.381e-09 0.0013433 0.00091924 0.0011579 v omega 16.751 1.0313e+05 2667.6 501.36 v TempK 288 341.96 293.64 290.67 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.6205e-14 9.6647e-05 6.0334e-05 7.8238e-05 v CourantNb 2.3376e-09 0.0002162 1.3893e-05 7.9464e-06 v FourierNb 0.11187 0.6281 0.19414 0.16497 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.944 4.944 0.00050432 -4.9882e-07 v volume_forces[Z] -4.944 4.944 -0.00050418 5.9724e-07 v ǁvolume_forcesǁ 2.8022e-08 4.9452 0.51096 0.24005 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.85 290.81 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015884 5.617e-05 3.1498e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.11191 0.6281 0.19416 0.16498 INSTANT 0.591282000E+00 TIME STEP NUMBER 614 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10607E-04 0.23867E-02 Friction velocity uk : 0.10607E-04 0.23866E-02 Dimensionless distance yplus : 0.70634E-04 0.15878E-01 Friction thermal sca. tstar : -0.51902E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.49609E-04 0.11152E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10607E-04 0.23867E-02 Friction velocity uk : 0.10607E-04 0.23866E-02 Dimensionless distance yplus : 0.70634E-04 0.15878E-01 Friction thermal sca. tstar : -0.51902E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.49609E-04 0.11152E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34731E-08 3 0.18161E-06 0.29704E-12 0.11049E+01 c Velocity[X] 0.12541E-31 c Velocity[Y] 0.14852E-12 c Velocity[Z] 0.14852E-12 c Pressure 0.11682E-13 17 0.91081E-07 0.91081E-07 0.13064E+01 c k 0.41237E-06 2 0.47788E-07 0.39789E-08 0.16761E+01 c omega 0.13153E+02 1 0.18024E-08 0.44385E+00 0.34684E-02 c TempK 0.94610E+02 1 0.12235E-06 0.28189E-01 0.18606E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.0463e-13 8.7146e-14 -1.0779e-17 -2.7783e-18 v Velocity[Y] -0.00013065 0.00012571 -9.4636e-10 -3.5661e-12 v Velocity[Z] -0.00012569 0.00013066 7.1331e-10 -1.4531e-12 v ǁVelocityǁ 7.6612e-10 0.00013983 1.0551e-05 6.8672e-06 v Pressure -0.0010377 0.019991 0.0011034 9.1826e-20 v k 1.3751e-09 0.0013414 0.00091767 0.001156 v omega 16.729 1.0313e+05 2667.6 501.34 v TempK 288 341.96 293.64 290.67 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.6136e-14 9.6634e-05 6.0311e-05 7.8212e-05 v CourantNb 2.341e-09 0.00021606 1.3892e-05 7.9492e-06 v FourierNb 0.11175 0.6281 0.19409 0.16493 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9441 4.9441 0.00050457 -4.992e-07 v volume_forces[Z] -4.9441 4.9441 -0.00050443 5.9767e-07 v ǁvolume_forcesǁ 2.7859e-08 4.9453 0.51121 0.24025 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.85 290.81 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015878 5.6152e-05 3.1488e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.11179 0.6281 0.19411 0.16493 INSTANT 0.592245000E+00 TIME STEP NUMBER 615 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10573E-04 0.23858E-02 Friction velocity uk : 0.10574E-04 0.23857E-02 Dimensionless distance yplus : 0.70410E-04 0.15873E-01 Friction thermal sca. tstar : -0.46515E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.49452E-04 0.11148E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10573E-04 0.23858E-02 Friction velocity uk : 0.10574E-04 0.23857E-02 Dimensionless distance yplus : 0.70410E-04 0.15873E-01 Friction thermal sca. tstar : -0.46515E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.49452E-04 0.11148E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34739E-08 3 0.18173E-06 0.29644E-12 0.11038E+01 c Velocity[X] 0.12481E-31 c Velocity[Y] 0.14822E-12 c Velocity[Z] 0.14822E-12 c Pressure 0.11650E-13 17 0.90827E-07 0.90827E-07 0.13042E+01 c k 0.41172E-06 2 0.47685E-07 0.39559E-08 0.16739E+01 c omega 0.13153E+02 1 0.17966E-08 0.44146E+00 0.34590E-02 c TempK 0.94611E+02 1 0.12207E-06 0.28121E-01 0.18583E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.0455e-13 8.7081e-14 -1.0771e-17 -2.7764e-18 v Velocity[Y] -0.00013059 0.00012564 -9.4485e-10 -3.5593e-12 v Velocity[Z] -0.00012562 0.00013059 7.1146e-10 -1.4547e-12 v ǁVelocityǁ 7.6158e-10 0.00013976 1.0553e-05 6.873e-06 v Pressure -0.0010394 0.020007 0.0011046 -3.2357e-20 v k 1.3693e-09 0.0013394 0.00091611 0.0011541 v omega 16.707 1.0313e+05 2667.6 501.32 v TempK 288 341.96 293.64 290.67 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.6068e-14 9.6621e-05 6.0288e-05 7.8185e-05 v CourantNb 2.3445e-09 0.00021592 1.389e-05 7.9521e-06 v FourierNb 0.11163 0.6281 0.19404 0.16488 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9441 4.9442 0.00050482 -4.9959e-07 v volume_forces[Z] -4.9441 4.9442 -0.00050469 5.9809e-07 v ǁvolume_forcesǁ 2.7695e-08 4.9454 0.51147 0.24045 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.85 290.82 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015873 5.6134e-05 3.1477e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.11167 0.6281 0.19406 0.16488 INSTANT 0.593208000E+00 TIME STEP NUMBER 616 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10539E-04 0.23849E-02 Friction velocity uk : 0.10540E-04 0.23849E-02 Dimensionless distance yplus : 0.70185E-04 0.15867E-01 Friction thermal sca. tstar : -0.42518E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.49294E-04 0.11144E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10539E-04 0.23849E-02 Friction velocity uk : 0.10540E-04 0.23849E-02 Dimensionless distance yplus : 0.70185E-04 0.15867E-01 Friction thermal sca. tstar : -0.42518E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.49294E-04 0.11144E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34748E-08 3 0.18062E-06 0.29584E-12 0.11028E+01 c Velocity[X] 0.12421E-31 c Velocity[Y] 0.14792E-12 c Velocity[Z] 0.14792E-12 c Pressure 0.11613E-13 17 0.90544E-07 0.90544E-07 0.13020E+01 c k 0.41108E-06 2 0.47583E-07 0.39331E-08 0.16717E+01 c omega 0.13153E+02 1 0.17908E-08 0.43909E+00 0.34497E-02 c TempK 0.94611E+02 1 0.12179E-06 0.28053E-01 0.18561E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.0447e-13 8.7017e-14 -1.0764e-17 -2.7745e-18 v Velocity[Y] -0.00013053 0.00012558 -9.4334e-10 -3.5526e-12 v Velocity[Z] -0.00012556 0.00013053 7.0961e-10 -1.4562e-12 v ǁVelocityǁ 7.5703e-10 0.0001397 1.0556e-05 6.8788e-06 v Pressure -0.0010411 0.020023 0.0011057 1.132e-19 v k 1.3635e-09 0.0013375 0.00091455 0.0011523 v omega 16.685 1.0313e+05 2667.6 501.3 v TempK 288 341.96 293.64 290.68 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.5999e-14 9.6608e-05 6.0264e-05 7.8159e-05 v CourantNb 2.3479e-09 0.00021577 1.3889e-05 7.955e-06 v FourierNb 0.11151 0.6281 0.19399 0.16483 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9442 4.9442 0.00050508 -4.9997e-07 v volume_forces[Z] -4.9442 4.9442 -0.00050494 5.9852e-07 v ǁvolume_forcesǁ 2.7531e-08 4.9455 0.51172 0.24064 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.86 290.82 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015867 5.6117e-05 3.1466e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.11155 0.6281 0.19401 0.16484 INSTANT 0.594171000E+00 TIME STEP NUMBER 617 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10505E-04 0.23841E-02 Friction velocity uk : 0.10506E-04 0.23840E-02 Dimensionless distance yplus : 0.69959E-04 0.15861E-01 Friction thermal sca. tstar : -0.39402E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.49135E-04 0.11140E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10505E-04 0.23841E-02 Friction velocity uk : 0.10506E-04 0.23840E-02 Dimensionless distance yplus : 0.69959E-04 0.15861E-01 Friction thermal sca. tstar : -0.39402E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.49135E-04 0.11140E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34756E-08 3 0.18014E-06 0.29524E-12 0.11017E+01 c Velocity[X] 0.12361E-31 c Velocity[Y] 0.14762E-12 c Velocity[Z] 0.14762E-12 c Pressure 0.11601E-13 17 0.90447E-07 0.90447E-07 0.12998E+01 c k 0.41043E-06 2 0.47481E-07 0.39104E-08 0.16695E+01 c omega 0.13153E+02 1 0.17851E-08 0.43673E+00 0.34404E-02 c TempK 0.94612E+02 1 0.12151E-06 0.27985E-01 0.18538E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.0439e-13 8.6952e-14 -1.0756e-17 -2.7727e-18 v Velocity[Y] -0.00013047 0.00012551 -9.4183e-10 -3.5458e-12 v Velocity[Z] -0.00012549 0.00013047 7.0775e-10 -1.4578e-12 v ǁVelocityǁ 7.5246e-10 0.00013963 1.0559e-05 6.8846e-06 v Pressure -0.0010428 0.020039 0.0011068 3.4318e-21 v k 1.3577e-09 0.0013356 0.000913 0.0011504 v omega 16.663 1.0313e+05 2667.6 501.28 v TempK 288 341.96 293.65 290.68 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.5932e-14 9.6595e-05 6.0241e-05 7.8132e-05 v CourantNb 2.3514e-09 0.00021563 1.3887e-05 7.9578e-06 v FourierNb 0.11138 0.6281 0.19394 0.16478 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9443 4.9443 0.00050533 -5.0035e-07 v volume_forces[Z] -4.9443 4.9443 -0.00050519 5.9895e-07 v ǁvolume_forcesǁ 2.7366e-08 4.9455 0.51197 0.24084 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.86 290.82 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015861 5.6099e-05 3.1455e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.11143 0.6281 0.19396 0.16479 INSTANT 0.595134000E+00 TIME STEP NUMBER 618 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10471E-04 0.23832E-02 Friction velocity uk : 0.10472E-04 0.23832E-02 Dimensionless distance yplus : 0.69731E-04 0.15855E-01 Friction thermal sca. tstar : -0.36883E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.48975E-04 0.11136E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10471E-04 0.23832E-02 Friction velocity uk : 0.10472E-04 0.23832E-02 Dimensionless distance yplus : 0.69731E-04 0.15855E-01 Friction thermal sca. tstar : -0.36883E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.48975E-04 0.11136E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34764E-08 3 0.17965E-06 0.29465E-12 0.11007E+01 c Velocity[X] 0.12302E-31 c Velocity[Y] 0.14732E-12 c Velocity[Z] 0.14733E-12 c Pressure 0.11552E-13 17 0.90063E-07 0.90063E-07 0.12976E+01 c k 0.40979E-06 2 0.47379E-07 0.38879E-08 0.16674E+01 c omega 0.13153E+02 1 0.17794E-08 0.43439E+00 0.34312E-02 c TempK 0.94612E+02 1 0.12123E-06 0.27918E-01 0.18516E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.0431e-13 8.6888e-14 -1.0748e-17 -2.7708e-18 v Velocity[Y] -0.00013041 0.00012544 -9.403e-10 -3.5391e-12 v Velocity[Z] -0.00012542 0.00013041 7.0588e-10 -1.4593e-12 v ǁVelocityǁ 7.4788e-10 0.00013956 1.0561e-05 6.8904e-06 v Pressure -0.0010445 0.020055 0.0011079 -4.2947e-20 v k 1.352e-09 0.0013336 0.00091145 0.0011485 v omega 16.641 1.0313e+05 2667.6 501.26 v TempK 288 341.96 293.65 290.68 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.5864e-14 9.6582e-05 6.0218e-05 7.8106e-05 v CourantNb 2.3548e-09 0.00021549 1.3885e-05 7.9607e-06 v FourierNb 0.11126 0.6281 0.19389 0.16473 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9443 4.9444 0.00050558 -5.0073e-07 v volume_forces[Z] -4.9443 4.9444 -0.00050544 5.9937e-07 v ǁvolume_forcesǁ 2.7201e-08 4.9456 0.51222 0.24103 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.86 290.82 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015855 5.6081e-05 3.1445e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.11131 0.6281 0.19391 0.16474 INSTANT 0.596097000E+00 TIME STEP NUMBER 619 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10437E-04 0.23824E-02 Friction velocity uk : 0.10437E-04 0.23823E-02 Dimensionless distance yplus : 0.69502E-04 0.15850E-01 Friction thermal sca. tstar : -0.34793E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.48814E-04 0.11132E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10437E-04 0.23824E-02 Friction velocity uk : 0.10437E-04 0.23823E-02 Dimensionless distance yplus : 0.69502E-04 0.15850E-01 Friction thermal sca. tstar : -0.34793E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.48814E-04 0.11132E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34773E-08 3 0.17918E-06 0.29406E-12 0.10996E+01 c Velocity[X] 0.12244E-31 c Velocity[Y] 0.14703E-12 c Velocity[Z] 0.14703E-12 c Pressure 0.11533E-13 17 0.89907E-07 0.89907E-07 0.12954E+01 c k 0.40914E-06 2 0.47278E-07 0.38655E-08 0.16652E+01 c omega 0.13153E+02 1 0.17737E-08 0.43206E+00 0.34220E-02 c TempK 0.94613E+02 1 0.12096E-06 0.27851E-01 0.18493E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.0423e-13 8.6824e-14 -1.074e-17 -2.7689e-18 v Velocity[Y] -0.00013035 0.00012538 -9.3877e-10 -3.5324e-12 v Velocity[Z] -0.00012536 0.00013035 7.0401e-10 -1.4608e-12 v ǁVelocityǁ 7.4329e-10 0.00013949 1.0564e-05 6.8963e-06 v Pressure -0.0010462 0.020071 0.001109 4.7703e-20 v k 1.3463e-09 0.0013317 0.00090991 0.0011466 v omega 16.619 1.0313e+05 2667.5 501.24 v TempK 288 341.96 293.65 290.68 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.5797e-14 9.6569e-05 6.0194e-05 7.808e-05 v CourantNb 2.3583e-09 0.00021534 1.3884e-05 7.9636e-06 v FourierNb 0.11114 0.6281 0.19384 0.16468 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9444 4.9444 0.00050583 -5.011e-07 v volume_forces[Z] -4.9444 4.9444 -0.00050569 5.9979e-07 v ǁvolume_forcesǁ 2.7036e-08 4.9457 0.51247 0.24123 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.87 290.82 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.01585 5.6063e-05 3.1434e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.11119 0.6281 0.19386 0.16469 INSTANT 0.597060000E+00 TIME STEP NUMBER 620 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10402E-04 0.23815E-02 Friction velocity uk : 0.10403E-04 0.23815E-02 Dimensionless distance yplus : 0.69271E-04 0.15844E-01 Friction thermal sca. tstar : -0.33022E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.48651E-04 0.11128E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10402E-04 0.23815E-02 Friction velocity uk : 0.10403E-04 0.23815E-02 Dimensionless distance yplus : 0.69271E-04 0.15844E-01 Friction thermal sca. tstar : -0.33022E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.48651E-04 0.11128E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34781E-08 3 0.17869E-06 0.29347E-12 0.10985E+01 c Velocity[X] 0.12185E-31 c Velocity[Y] 0.14673E-12 c Velocity[Z] 0.14673E-12 c Pressure 0.11496E-13 17 0.89618E-07 0.89618E-07 0.12932E+01 c k 0.40850E-06 2 0.47177E-07 0.38433E-08 0.16630E+01 c omega 0.13153E+02 1 0.17680E-08 0.42975E+00 0.34128E-02 c TempK 0.94614E+02 1 0.12068E-06 0.27784E-01 0.18471E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.0415e-13 8.676e-14 -1.0733e-17 -2.7671e-18 v Velocity[Y] -0.00013028 0.00012531 -9.3724e-10 -3.5257e-12 v Velocity[Z] -0.00012529 0.00013029 7.0214e-10 -1.4624e-12 v ǁVelocityǁ 7.3868e-10 0.00013943 1.0567e-05 6.9021e-06 v Pressure -0.0010478 0.020087 0.0011102 -1.6385e-19 v k 1.3406e-09 0.0013298 0.00090837 0.0011448 v omega 16.597 1.0313e+05 2667.5 501.22 v TempK 288 341.96 293.65 290.68 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.5731e-14 9.6556e-05 6.0171e-05 7.8053e-05 v CourantNb 2.3617e-09 0.0002152 1.3882e-05 7.9665e-06 v FourierNb 0.11102 0.6281 0.19379 0.16464 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9445 4.9445 0.00050608 -5.0148e-07 v volume_forces[Z] -4.9445 4.9445 -0.00050594 6.0022e-07 v ǁvolume_forcesǁ 2.687e-08 4.9457 0.51272 0.24142 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.87 290.83 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015844 5.6046e-05 3.1423e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.11107 0.6281 0.19381 0.16464 INSTANT 0.598023000E+00 TIME STEP NUMBER 621 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10367E-04 0.23807E-02 Friction velocity uk : 0.10368E-04 0.23806E-02 Dimensionless distance yplus : 0.69038E-04 0.15838E-01 Friction thermal sca. tstar : -0.31496E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.48488E-04 0.11124E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10367E-04 0.23807E-02 Friction velocity uk : 0.10368E-04 0.23806E-02 Dimensionless distance yplus : 0.69038E-04 0.15838E-01 Friction thermal sca. tstar : -0.31496E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.48488E-04 0.11124E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34790E-08 3 0.17821E-06 0.29288E-12 0.10975E+01 c Velocity[X] 0.12127E-31 c Velocity[Y] 0.14644E-12 c Velocity[Z] 0.14644E-12 c Pressure 0.11468E-13 17 0.89404E-07 0.89404E-07 0.12910E+01 c k 0.40786E-06 2 0.47076E-07 0.38212E-08 0.16609E+01 c omega 0.13153E+02 1 0.17623E-08 0.42745E+00 0.34037E-02 c TempK 0.94614E+02 1 0.12041E-06 0.27717E-01 0.18448E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.0407e-13 8.6696e-14 -1.0725e-17 -2.7652e-18 v Velocity[Y] -0.00013022 0.00012524 -9.3569e-10 -3.519e-12 v Velocity[Z] -0.00012523 0.00013023 7.0026e-10 -1.4639e-12 v ǁVelocityǁ 7.3406e-10 0.00013936 1.0569e-05 6.9079e-06 v Pressure -0.0010495 0.020103 0.0011113 -8.1188e-20 v k 1.335e-09 0.0013279 0.00090684 0.0011429 v omega 16.576 1.0313e+05 2667.5 501.2 v TempK 288 341.97 293.66 290.69 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.5664e-14 9.6543e-05 6.0148e-05 7.8027e-05 v CourantNb 2.3651e-09 0.00021506 1.3881e-05 7.9694e-06 v FourierNb 0.1109 0.6281 0.19374 0.16459 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9446 4.9446 0.00050633 -5.0186e-07 v volume_forces[Z] -4.9446 4.9446 -0.00050619 6.0064e-07 v ǁvolume_forcesǁ 2.6703e-08 4.9458 0.51297 0.24162 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.87 290.83 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015838 5.6028e-05 3.1412e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.11095 0.6281 0.19376 0.1646 INSTANT 0.598986000E+00 TIME STEP NUMBER 622 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10332E-04 0.23798E-02 Friction velocity uk : 0.10333E-04 0.23798E-02 Dimensionless distance yplus : 0.68804E-04 0.15833E-01 Friction thermal sca. tstar : -0.30164E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.48324E-04 0.11120E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10332E-04 0.23798E-02 Friction velocity uk : 0.10333E-04 0.23798E-02 Dimensionless distance yplus : 0.68804E-04 0.15833E-01 Friction thermal sca. tstar : -0.30164E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.48324E-04 0.11120E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34799E-08 3 0.17775E-06 0.29229E-12 0.10964E+01 c Velocity[X] 0.12070E-31 c Velocity[Y] 0.14614E-12 c Velocity[Z] 0.14615E-12 c Pressure 0.11485E-13 17 0.89528E-07 0.89528E-07 0.12889E+01 c k 0.40723E-06 2 0.46976E-07 0.37994E-08 0.16587E+01 c omega 0.13153E+02 1 0.17567E-08 0.42517E+00 0.33946E-02 c TempK 0.94615E+02 1 0.12014E-06 0.27651E-01 0.18426E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.04e-13 8.6633e-14 -1.0717e-17 -2.7634e-18 v Velocity[Y] -0.00013016 0.00012518 -9.3414e-10 -3.5123e-12 v Velocity[Z] -0.00012516 0.00013017 6.9837e-10 -1.4654e-12 v ǁVelocityǁ 7.2943e-10 0.00013929 1.0572e-05 6.9138e-06 v Pressure -0.0010512 0.020119 0.0011124 -5.0154e-20 v k 1.3294e-09 0.0013259 0.00090531 0.0011411 v omega 16.554 1.0313e+05 2667.5 501.18 v TempK 288 341.97 293.66 290.69 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.5599e-14 9.653e-05 6.0125e-05 7.8001e-05 v CourantNb 2.3686e-09 0.00021492 1.3879e-05 7.9724e-06 v FourierNb 0.11079 0.6281 0.19369 0.16454 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9446 4.9447 0.00050658 -5.0224e-07 v volume_forces[Z] -4.9446 4.9447 -0.00050644 6.0106e-07 v ǁvolume_forcesǁ 2.6536e-08 4.9459 0.51321 0.24181 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.87 290.83 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015833 5.601e-05 3.1402e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.11083 0.6281 0.19371 0.16455 INSTANT 0.599949000E+00 TIME STEP NUMBER 623 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10297E-04 0.23791E-02 Friction velocity uk : 0.10297E-04 0.23790E-02 Dimensionless distance yplus : 0.68569E-04 0.15828E-01 Friction thermal sca. tstar : -0.28987E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.48158E-04 0.11117E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10297E-04 0.23791E-02 Friction velocity uk : 0.10297E-04 0.23790E-02 Dimensionless distance yplus : 0.68569E-04 0.15828E-01 Friction thermal sca. tstar : -0.28987E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.48158E-04 0.11117E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34807E-08 3 0.17730E-06 0.29170E-12 0.10953E+01 c Velocity[X] 0.12012E-31 c Velocity[Y] 0.14585E-12 c Velocity[Z] 0.14585E-12 c Pressure 0.11474E-13 17 0.89447E-07 0.89447E-07 0.12867E+01 c k 0.40659E-06 2 0.46876E-07 0.37776E-08 0.16566E+01 c omega 0.13153E+02 1 0.17511E-08 0.42291E+00 0.33856E-02 c TempK 0.94615E+02 1 0.11986E-06 0.27584E-01 0.18404E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.0392e-13 8.6569e-14 -1.071e-17 -2.7615e-18 v Velocity[Y] -0.0001301 0.00012511 -9.3259e-10 -3.5057e-12 v Velocity[Z] -0.0001251 0.00013011 6.9648e-10 -1.4669e-12 v ǁVelocityǁ 7.2479e-10 0.00013922 1.0575e-05 6.9196e-06 v Pressure -0.0010529 0.020135 0.0011135 -3.4613e-20 v k 1.3238e-09 0.001324 0.00090378 0.0011392 v omega 16.532 1.0313e+05 2667.5 501.16 v TempK 288 341.97 293.66 290.69 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.5533e-14 9.6517e-05 6.0102e-05 7.7975e-05 v CourantNb 2.372e-09 0.00021477 1.3878e-05 7.9753e-06 v FourierNb 0.11067 0.6281 0.19364 0.16449 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9447 4.9447 0.00050683 -5.0261e-07 v volume_forces[Z] -4.9447 4.9447 -0.00050669 6.0148e-07 v ǁvolume_forcesǁ 2.6369e-08 4.9459 0.51346 0.24201 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.88 290.83 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015828 5.5993e-05 3.1391e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.11071 0.6281 0.19366 0.1645 INSTANT 0.600912000E+00 TIME STEP NUMBER 624 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10261E-04 0.23783E-02 Friction velocity uk : 0.10262E-04 0.23783E-02 Dimensionless distance yplus : 0.68331E-04 0.15823E-01 Friction thermal sca. tstar : -0.27939E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.47992E-04 0.11113E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10261E-04 0.23783E-02 Friction velocity uk : 0.10262E-04 0.23783E-02 Dimensionless distance yplus : 0.68331E-04 0.15823E-01 Friction thermal sca. tstar : -0.27939E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.47992E-04 0.11113E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34816E-08 3 0.32145E-06 0.29112E-12 0.10943E+01 c Velocity[X] 0.11955E-31 c Velocity[Y] 0.14556E-12 c Velocity[Z] 0.14556E-12 c Pressure 0.11439E-13 17 0.89172E-07 0.89172E-07 0.12846E+01 c k 0.40596E-06 2 0.46777E-07 0.37560E-08 0.16544E+01 c omega 0.13153E+02 1 0.17455E-08 0.42065E+00 0.33765E-02 c TempK 0.94616E+02 1 0.11959E-06 0.27519E-01 0.18382E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.0384e-13 8.6506e-14 -1.0702e-17 -2.7597e-18 v Velocity[Y] -0.00013004 0.00012505 -9.3103e-10 -3.4991e-12 v Velocity[Z] -0.00012503 0.00013004 6.9458e-10 -1.4685e-12 v ǁVelocityǁ 7.2014e-10 0.00013916 1.0578e-05 6.9255e-06 v Pressure -0.0010546 0.020151 0.0011146 -1.1276e-21 v k 1.3183e-09 0.0013221 0.00090226 0.0011374 v omega 16.511 1.0313e+05 2667.5 501.14 v TempK 288 341.97 293.67 290.69 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.5468e-14 9.6505e-05 6.0079e-05 7.7948e-05 v CourantNb 2.3754e-09 0.00021464 1.3876e-05 7.9782e-06 v FourierNb 0.11055 0.6281 0.19359 0.16444 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9448 4.9448 0.00050708 -5.0299e-07 v volume_forces[Z] -4.9448 4.9448 -0.00050694 6.019e-07 v ǁvolume_forcesǁ 2.6201e-08 4.946 0.51371 0.2422 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.88 290.84 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015823 5.5975e-05 3.138e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.11059 0.6281 0.19361 0.16445 INSTANT 0.601875000E+00 TIME STEP NUMBER 625 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10225E-04 0.23776E-02 Friction velocity uk : 0.10226E-04 0.23775E-02 Dimensionless distance yplus : 0.68093E-04 0.15818E-01 Friction thermal sca. tstar : -0.26996E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.47824E-04 0.11110E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10225E-04 0.23776E-02 Friction velocity uk : 0.10226E-04 0.23775E-02 Dimensionless distance yplus : 0.68093E-04 0.15818E-01 Friction thermal sca. tstar : -0.26996E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.47824E-04 0.11110E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34825E-08 3 0.19436E-06 0.29053E-12 0.10932E+01 c Velocity[X] 0.11899E-31 c Velocity[Y] 0.14527E-12 c Velocity[Z] 0.14527E-12 c Pressure 0.11423E-13 17 0.89044E-07 0.89044E-07 0.12824E+01 c k 0.40533E-06 2 0.46678E-07 0.37346E-08 0.16523E+01 c omega 0.13153E+02 1 0.17400E-08 0.41842E+00 0.33675E-02 c TempK 0.94617E+02 1 0.11932E-06 0.27453E-01 0.18360E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.0376e-13 8.6443e-14 -1.0694e-17 -2.7579e-18 v Velocity[Y] -0.00012998 0.00012498 -9.2946e-10 -3.4925e-12 v Velocity[Z] -0.00012497 0.00012998 6.9268e-10 -1.47e-12 v ǁVelocityǁ 7.1547e-10 0.00013909 1.058e-05 6.9313e-06 v Pressure -0.0010563 0.020167 0.0011157 2.9122e-20 v k 1.3128e-09 0.0013202 0.00090075 0.0011356 v omega 16.489 1.0313e+05 2667.4 501.12 v TempK 288 341.97 293.67 290.69 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.5403e-14 9.6492e-05 6.0056e-05 7.7922e-05 v CourantNb 2.3788e-09 0.00021451 1.3875e-05 7.9812e-06 v FourierNb 0.11043 0.6281 0.19354 0.1644 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9448 4.9449 0.00050733 -5.0336e-07 v volume_forces[Z] -4.9448 4.9449 -0.00050719 6.0232e-07 v ǁvolume_forcesǁ 2.6033e-08 4.9461 0.51396 0.2424 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.88 290.84 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015818 5.5958e-05 3.137e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.11048 0.6281 0.19356 0.16441 INSTANT 0.602838000E+00 TIME STEP NUMBER 626 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10189E-04 0.23768E-02 Friction velocity uk : 0.10190E-04 0.23768E-02 Dimensionless distance yplus : 0.67852E-04 0.15813E-01 Friction thermal sca. tstar : -0.26142E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.47655E-04 0.11106E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10189E-04 0.23768E-02 Friction velocity uk : 0.10190E-04 0.23768E-02 Dimensionless distance yplus : 0.67852E-04 0.15813E-01 Friction thermal sca. tstar : -0.26142E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.47655E-04 0.11106E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34834E-08 3 0.17585E-06 0.28995E-12 0.10922E+01 c Velocity[X] 0.11842E-31 c Velocity[Y] 0.14497E-12 c Velocity[Z] 0.14498E-12 c Pressure 0.11341E-13 17 0.88398E-07 0.88398E-07 0.12803E+01 c k 0.40470E-06 2 0.46579E-07 0.37133E-08 0.16501E+01 c omega 0.13153E+02 1 0.17345E-08 0.41620E+00 0.33586E-02 c TempK 0.94617E+02 1 0.11905E-06 0.27387E-01 0.18338E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.0368e-13 8.638e-14 -1.0687e-17 -2.756e-18 v Velocity[Y] -0.00012992 0.00012492 -9.2788e-10 -3.4859e-12 v Velocity[Z] -0.0001249 0.00012992 6.9078e-10 -1.4716e-12 v ǁVelocityǁ 7.108e-10 0.00013903 1.0583e-05 6.9372e-06 v Pressure -0.0010579 0.020183 0.0011168 3.7799e-20 v k 1.3073e-09 0.0013184 0.00089923 0.0011337 v omega 16.468 1.0313e+05 2667.4 501.1 v TempK 288 341.97 293.67 290.7 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.5339e-14 9.6479e-05 6.0033e-05 7.7896e-05 v CourantNb 2.3823e-09 0.00021438 1.3873e-05 7.9841e-06 v FourierNb 0.11031 0.6281 0.1935 0.16435 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9449 4.9449 0.00050758 -5.0374e-07 v volume_forces[Z] -4.9449 4.9449 -0.00050744 6.0274e-07 v ǁvolume_forcesǁ 2.5864e-08 4.9462 0.51421 0.24259 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.88 290.84 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015813 5.594e-05 3.1359e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.11036 0.6281 0.19351 0.16436 INSTANT 0.603801000E+00 TIME STEP NUMBER 627 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10153E-04 0.23761E-02 Friction velocity uk : 0.10153E-04 0.23760E-02 Dimensionless distance yplus : 0.67610E-04 0.15808E-01 Friction thermal sca. tstar : -0.25365E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.47485E-04 0.11103E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10153E-04 0.23761E-02 Friction velocity uk : 0.10153E-04 0.23760E-02 Dimensionless distance yplus : 0.67610E-04 0.15808E-01 Friction thermal sca. tstar : -0.25365E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.47485E-04 0.11103E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34842E-08 3 0.17544E-06 0.28937E-12 0.10911E+01 c Velocity[X] 0.11786E-31 c Velocity[Y] 0.14469E-12 c Velocity[Z] 0.14469E-12 c Pressure 0.11419E-13 17 0.89012E-07 0.89012E-07 0.12781E+01 c k 0.40407E-06 2 0.46481E-07 0.36922E-08 0.16480E+01 c omega 0.13153E+02 1 0.17290E-08 0.41399E+00 0.33497E-02 c TempK 0.94618E+02 1 0.11879E-06 0.27322E-01 0.18316E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.0361e-13 8.6317e-14 -1.0679e-17 -2.7542e-18 v Velocity[Y] -0.00012986 0.00012485 -9.263e-10 -3.4794e-12 v Velocity[Z] -0.00012484 0.00012987 6.8887e-10 -1.4731e-12 v ǁVelocityǁ 7.0611e-10 0.00013896 1.0586e-05 6.943e-06 v Pressure -0.0010596 0.020199 0.001118 3.8044e-20 v k 1.3019e-09 0.0013165 0.00089773 0.0011319 v omega 16.447 1.0313e+05 2667.4 501.08 v TempK 288 341.97 293.67 290.7 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.5275e-14 9.6466e-05 6.001e-05 7.787e-05 v CourantNb 2.3857e-09 0.00021425 1.3872e-05 7.9871e-06 v FourierNb 0.1102 0.6281 0.19345 0.1643 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.945 4.945 0.00050782 -5.0411e-07 v volume_forces[Z] -4.945 4.945 -0.00050769 6.0316e-07 v ǁvolume_forcesǁ 2.5695e-08 4.9462 0.51445 0.24278 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.89 290.84 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015808 5.5923e-05 3.1348e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.11024 0.6281 0.19346 0.16431 INSTANT 0.604764000E+00 TIME STEP NUMBER 628 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10116E-04 0.23753E-02 Friction velocity uk : 0.10117E-04 0.23753E-02 Dimensionless distance yplus : 0.67367E-04 0.15803E-01 Friction thermal sca. tstar : -0.24653E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.47314E-04 0.11099E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10116E-04 0.23753E-02 Friction velocity uk : 0.10117E-04 0.23753E-02 Dimensionless distance yplus : 0.67367E-04 0.15803E-01 Friction thermal sca. tstar : -0.24653E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.47314E-04 0.11099E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34851E-08 3 0.17490E-06 0.28879E-12 0.10900E+01 c Velocity[X] 0.11730E-31 c Velocity[Y] 0.14440E-12 c Velocity[Z] 0.14440E-12 c Pressure 0.11314E-13 17 0.88192E-07 0.88192E-07 0.12760E+01 c k 0.40344E-06 2 0.46383E-07 0.36712E-08 0.16459E+01 c omega 0.13153E+02 1 0.17235E-08 0.41180E+00 0.33408E-02 c TempK 0.94618E+02 1 0.11852E-06 0.27257E-01 0.18294E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.0353e-13 8.6254e-14 -1.0672e-17 -2.7524e-18 v Velocity[Y] -0.0001298 0.00012479 -9.2472e-10 -3.4729e-12 v Velocity[Z] -0.00012477 0.00012981 6.8695e-10 -1.4745e-12 v ǁVelocityǁ 7.0141e-10 0.0001389 1.0589e-05 6.9489e-06 v Pressure -0.0010613 0.020215 0.0011191 4.4418e-20 v k 1.2965e-09 0.0013146 0.00089623 0.0011301 v omega 16.425 1.0313e+05 2667.4 501.06 v TempK 288 341.97 293.68 290.7 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.5211e-14 9.6453e-05 5.9987e-05 7.7844e-05 v CourantNb 2.3891e-09 0.00021413 1.3871e-05 7.99e-06 v FourierNb 0.11008 0.6281 0.1934 0.16426 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9451 4.9451 0.00050807 -5.0448e-07 v volume_forces[Z] -4.9451 4.9451 -0.00050793 6.0357e-07 v ǁvolume_forcesǁ 2.5526e-08 4.9463 0.5147 0.24298 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.89 290.84 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015803 5.5905e-05 3.1338e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.11013 0.6281 0.19341 0.16426 INSTANT 0.605727000E+00 TIME STEP NUMBER 629 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10079E-04 0.23746E-02 Friction velocity uk : 0.10080E-04 0.23745E-02 Dimensionless distance yplus : 0.67121E-04 0.15798E-01 Friction thermal sca. tstar : -0.23997E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.47142E-04 0.11096E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10079E-04 0.23746E-02 Friction velocity uk : 0.10080E-04 0.23745E-02 Dimensionless distance yplus : 0.67121E-04 0.15798E-01 Friction thermal sca. tstar : -0.23997E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.47142E-04 0.11096E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34860E-08 3 0.17445E-06 0.28822E-12 0.10890E+01 c Velocity[X] 0.11674E-31 c Velocity[Y] 0.14411E-12 c Velocity[Z] 0.14411E-12 c Pressure 0.11256E-13 17 0.87735E-07 0.87735E-07 0.12739E+01 c k 0.40282E-06 2 0.46285E-07 0.36504E-08 0.16438E+01 c omega 0.13153E+02 1 0.17180E-08 0.40962E+00 0.33320E-02 c TempK 0.94619E+02 1 0.11825E-06 0.27193E-01 0.18272E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.0345e-13 8.6192e-14 -1.0664e-17 -2.7506e-18 v Velocity[Y] -0.00012974 0.00012473 -9.2342e-10 -3.7617e-12 v Velocity[Z] -0.00012471 0.00012975 6.8496e-10 -1.5433e-12 v ǁVelocityǁ 6.9677e-10 0.00013883 1.0592e-05 6.9548e-06 v Pressure -0.001063 0.020231 0.0011202 5.9812e-21 v k 1.2911e-09 0.0013127 0.00089473 0.0011283 v omega 16.404 1.0313e+05 2667.4 501.05 v TempK 288 341.97 293.68 290.7 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.5148e-14 9.644e-05 5.9964e-05 7.7818e-05 v CourantNb 2.3925e-09 0.000214 1.3869e-05 7.993e-06 v FourierNb 0.10997 0.6281 0.19335 0.16421 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9451 4.9451 0.00050832 -5.0485e-07 v volume_forces[Z] -4.9451 4.9451 -0.00050818 6.0399e-07 v ǁvolume_forcesǁ 2.5356e-08 4.9464 0.51495 0.24317 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.89 290.85 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015798 5.5888e-05 3.1327e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.11001 0.6281 0.19336 0.16422 INSTANT 0.606690000E+00 TIME STEP NUMBER 630 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10043E-04 0.23738E-02 Friction velocity uk : 0.10043E-04 0.23738E-02 Dimensionless distance yplus : 0.66878E-04 0.15793E-01 Friction thermal sca. tstar : -0.23392E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.46971E-04 0.11092E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10043E-04 0.23738E-02 Friction velocity uk : 0.10043E-04 0.23738E-02 Dimensionless distance yplus : 0.66878E-04 0.15793E-01 Friction thermal sca. tstar : -0.23392E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.46971E-04 0.11092E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34869E-08 3 0.17398E-06 0.28764E-12 0.10879E+01 c Velocity[X] 0.11619E-31 c Velocity[Y] 0.14382E-12 c Velocity[Z] 0.14382E-12 c Pressure 0.11230E-13 17 0.87533E-07 0.87533E-07 0.12718E+01 c k 0.40219E-06 2 0.46188E-07 0.36297E-08 0.16417E+01 c omega 0.13153E+02 1 0.17126E-08 0.40746E+00 0.33231E-02 c TempK 0.94619E+02 1 0.11799E-06 0.27129E-01 0.18250E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.0338e-13 8.6129e-14 -1.0657e-17 -2.7488e-18 v Velocity[Y] -0.00012968 0.00012466 -9.2182e-10 -3.7585e-12 v Velocity[Z] -0.00012464 0.00012969 6.8304e-10 -1.534e-12 v ǁVelocityǁ 6.9202e-10 0.00013877 1.0594e-05 6.9607e-06 v Pressure -0.0010647 0.020247 0.0011213 -7.756e-20 v k 1.2857e-09 0.0013108 0.00089323 0.0011265 v omega 16.383 1.0313e+05 2667.4 501.03 v TempK 288 341.97 293.68 290.71 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.5085e-14 9.6428e-05 5.9941e-05 7.7792e-05 v CourantNb 2.3959e-09 0.00021387 1.3868e-05 7.996e-06 v FourierNb 0.10985 0.6281 0.1933 0.16416 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9452 4.9452 0.00050857 -5.0523e-07 v volume_forces[Z] -4.9452 4.9452 -0.00050843 6.0441e-07 v ǁvolume_forcesǁ 2.5188e-08 4.9464 0.51519 0.24337 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.9 290.85 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015793 5.587e-05 3.1317e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.10989 0.6281 0.19331 0.16417 INSTANT 0.607653000E+00 TIME STEP NUMBER 631 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10005E-04 0.23731E-02 Friction velocity uk : 0.10006E-04 0.23730E-02 Dimensionless distance yplus : 0.66628E-04 0.15788E-01 Friction thermal sca. tstar : -0.22829E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.46795E-04 0.11089E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10005E-04 0.23731E-02 Friction velocity uk : 0.10006E-04 0.23730E-02 Dimensionless distance yplus : 0.66628E-04 0.15788E-01 Friction thermal sca. tstar : -0.22829E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.46795E-04 0.11089E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34879E-08 3 0.17351E-06 0.28707E-12 0.10869E+01 c Velocity[X] 0.11564E-31 c Velocity[Y] 0.14353E-12 c Velocity[Z] 0.14354E-12 c Pressure 0.11202E-13 17 0.87307E-07 0.87307E-07 0.12697E+01 c k 0.40157E-06 2 0.46091E-07 0.36091E-08 0.16396E+01 c omega 0.13153E+02 1 0.17072E-08 0.40531E+00 0.33144E-02 c TempK 0.94620E+02 1 0.11772E-06 0.27064E-01 0.18228E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.033e-13 8.6067e-14 -1.0649e-17 -2.747e-18 v Velocity[Y] -0.00012962 0.0001246 -9.2022e-10 -3.7494e-12 v Velocity[Z] -0.00012458 0.00012963 6.8111e-10 -1.5407e-12 v ǁVelocityǁ 6.8728e-10 0.0001387 1.0597e-05 6.9666e-06 v Pressure -0.0010663 0.020262 0.0011224 -8.8248e-22 v k 1.2804e-09 0.001309 0.00089175 0.0011247 v omega 16.362 1.0313e+05 2667.4 501.01 v TempK 288 341.97 293.69 290.71 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.5023e-14 9.6415e-05 5.9918e-05 7.7766e-05 v CourantNb 2.3993e-09 0.00021374 1.3866e-05 7.999e-06 v FourierNb 0.10974 0.6281 0.19325 0.16411 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9453 4.9453 0.00050881 -5.056e-07 v volume_forces[Z] -4.9453 4.9453 -0.00050868 6.0483e-07 v ǁvolume_forcesǁ 2.5017e-08 4.9465 0.51544 0.24356 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.9 290.85 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015788 5.5853e-05 3.1306e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.10978 0.6281 0.19326 0.16412 INSTANT 0.608616000E+00 TIME STEP NUMBER 632 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.99675E-05 0.23723E-02 Friction velocity uk : 0.99682E-05 0.23723E-02 Dimensionless distance yplus : 0.66377E-04 0.15783E-01 Friction thermal sca. tstar : -0.22305E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.46619E-04 0.11085E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.99675E-05 0.23723E-02 Friction velocity uk : 0.99682E-05 0.23723E-02 Dimensionless distance yplus : 0.66377E-04 0.15783E-01 Friction thermal sca. tstar : -0.22305E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.46619E-04 0.11085E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34888E-08 3 0.17305E-06 0.28650E-12 0.10858E+01 c Velocity[X] 0.11510E-31 c Velocity[Y] 0.14325E-12 c Velocity[Z] 0.14325E-12 c Pressure 0.11175E-13 17 0.87102E-07 0.87102E-07 0.12676E+01 c k 0.40095E-06 2 0.45995E-07 0.35887E-08 0.16375E+01 c omega 0.13153E+02 1 0.17018E-08 0.40317E+00 0.33056E-02 c TempK 0.94621E+02 1 0.11746E-06 0.27001E-01 0.18207E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.0322e-13 8.6005e-14 -1.0642e-17 -2.7452e-18 v Velocity[Y] -0.00012957 0.00012453 -9.1861e-10 -3.743e-12 v Velocity[Z] -0.00012451 0.00012957 6.7917e-10 -1.5424e-12 v ǁVelocityǁ 6.8253e-10 0.00013864 1.06e-05 6.9725e-06 v Pressure -0.001068 0.020278 0.0011235 -4.5497e-20 v k 1.2751e-09 0.0013071 0.00089026 0.0011229 v omega 16.341 1.0313e+05 2667.3 500.99 v TempK 288 341.97 293.69 290.71 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.496e-14 9.6402e-05 5.9896e-05 7.774e-05 v CourantNb 2.4027e-09 0.00021361 1.3865e-05 8.002e-06 v FourierNb 0.10962 0.6281 0.1932 0.16407 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9453 4.9454 0.00050906 -5.0597e-07 v volume_forces[Z] -4.9453 4.9454 -0.00050892 6.0524e-07 v ǁvolume_forcesǁ 2.4845e-08 4.9466 0.51569 0.24375 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.9 290.85 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015783 5.5835e-05 3.1296e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.10966 0.6281 0.19322 0.16407 INSTANT 0.609579000E+00 TIME STEP NUMBER 633 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.99296E-05 0.23716E-02 Friction velocity uk : 0.99303E-05 0.23716E-02 Dimensionless distance yplus : 0.66125E-04 0.15778E-01 Friction thermal sca. tstar : -0.21816E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.46442E-04 0.11082E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.99296E-05 0.23716E-02 Friction velocity uk : 0.99303E-05 0.23716E-02 Dimensionless distance yplus : 0.66125E-04 0.15778E-01 Friction thermal sca. tstar : -0.21816E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.46442E-04 0.11082E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34897E-08 3 0.18592E-06 0.28592E-12 0.10847E+01 c Velocity[X] 0.11456E-31 c Velocity[Y] 0.14296E-12 c Velocity[Z] 0.14296E-12 c Pressure 0.11161E-13 17 0.86984E-07 0.86984E-07 0.12655E+01 c k 0.40033E-06 2 0.45898E-07 0.35684E-08 0.16354E+01 c omega 0.13153E+02 1 0.16965E-08 0.40105E+00 0.32969E-02 c TempK 0.94621E+02 1 0.11720E-06 0.26937E-01 0.18185E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.0315e-13 8.5943e-14 -1.0634e-17 -2.7434e-18 v Velocity[Y] -0.00012951 0.00012447 -9.1699e-10 -3.7361e-12 v Velocity[Z] -0.00012445 0.00012951 6.7723e-10 -1.5437e-12 v ǁVelocityǁ 6.7776e-10 0.00013858 1.0603e-05 6.9784e-06 v Pressure -0.0010697 0.020294 0.0011246 -4.6869e-20 v k 1.2698e-09 0.0013053 0.00088878 0.0011211 v omega 16.32 1.0313e+05 2667.3 500.97 v TempK 288 341.97 293.69 290.71 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.4899e-14 9.6389e-05 5.9873e-05 7.7715e-05 v CourantNb 2.4061e-09 0.00021349 1.3864e-05 8.005e-06 v FourierNb 0.10951 0.6281 0.19315 0.16402 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9454 4.9454 0.00050931 -5.0633e-07 v volume_forces[Z] -4.9454 4.9454 -0.00050917 6.0565e-07 v ǁvolume_forcesǁ 2.4673e-08 4.9466 0.51593 0.24395 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.9 290.85 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015778 5.5818e-05 3.1285e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.10955 0.6281 0.19317 0.16403 INSTANT 0.610542000E+00 TIME STEP NUMBER 634 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.98914E-05 0.23709E-02 Friction velocity uk : 0.98921E-05 0.23708E-02 Dimensionless distance yplus : 0.65871E-04 0.15773E-01 Friction thermal sca. tstar : -0.21357E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.46263E-04 0.11078E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.98914E-05 0.23709E-02 Friction velocity uk : 0.98921E-05 0.23708E-02 Dimensionless distance yplus : 0.65871E-04 0.15773E-01 Friction thermal sca. tstar : -0.21357E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.46263E-04 0.11078E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34906E-08 3 0.17214E-06 0.28535E-12 0.10837E+01 c Velocity[X] 0.11402E-31 c Velocity[Y] 0.14268E-12 c Velocity[Z] 0.14268E-12 c Pressure 0.11128E-13 17 0.86729E-07 0.86729E-07 0.12634E+01 c k 0.39972E-06 2 0.45803E-07 0.35483E-08 0.16333E+01 c omega 0.13153E+02 1 0.16911E-08 0.39894E+00 0.32882E-02 c TempK 0.94622E+02 1 0.11694E-06 0.26874E-01 0.18164E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.0307e-13 8.5881e-14 -1.0627e-17 -2.7416e-18 v Velocity[Y] -0.00012945 0.00012441 -9.1536e-10 -3.7293e-12 v Velocity[Z] -0.00012439 0.00012945 6.7528e-10 -1.5452e-12 v ǁVelocityǁ 6.7299e-10 0.00013852 1.0606e-05 6.9843e-06 v Pressure -0.0010714 0.02031 0.0011257 -1.3502e-19 v k 1.2646e-09 0.0013034 0.00088731 0.0011193 v omega 16.299 1.0313e+05 2667.3 500.95 v TempK 288 341.98 293.69 290.71 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.4837e-14 9.6376e-05 5.985e-05 7.7689e-05 v CourantNb 2.4095e-09 0.00021336 1.3862e-05 8.008e-06 v FourierNb 0.10939 0.6281 0.1931 0.16397 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9455 4.9455 0.00050955 -5.067e-07 v volume_forces[Z] -4.9455 4.9455 -0.00050942 6.0606e-07 v ǁvolume_forcesǁ 2.4501e-08 4.9467 0.51618 0.24414 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.91 290.86 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015773 5.5801e-05 3.1275e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.10944 0.6281 0.19312 0.16398 INSTANT 0.611505000E+00 TIME STEP NUMBER 635 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.98530E-05 0.23701E-02 Friction velocity uk : 0.98537E-05 0.23701E-02 Dimensionless distance yplus : 0.65615E-04 0.15768E-01 Friction thermal sca. tstar : -0.20926E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.46084E-04 0.11075E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.98530E-05 0.23701E-02 Friction velocity uk : 0.98537E-05 0.23701E-02 Dimensionless distance yplus : 0.65615E-04 0.15768E-01 Friction thermal sca. tstar : -0.20926E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.46084E-04 0.11075E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34915E-08 3 0.17170E-06 0.28479E-12 0.10826E+01 c Velocity[X] 0.11348E-31 c Velocity[Y] 0.14239E-12 c Velocity[Z] 0.14239E-12 c Pressure 0.11133E-13 17 0.86764E-07 0.86764E-07 0.12613E+01 c k 0.39910E-06 2 0.45707E-07 0.35283E-08 0.16312E+01 c omega 0.13153E+02 1 0.16858E-08 0.39685E+00 0.32796E-02 c TempK 0.94622E+02 1 0.11668E-06 0.26810E-01 0.18142E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.0299e-13 8.5819e-14 -1.0619e-17 -2.7398e-18 v Velocity[Y] -0.00012939 0.00012434 -9.1373e-10 -3.7225e-12 v Velocity[Z] -0.00012432 0.00012939 6.7333e-10 -1.5467e-12 v ǁVelocityǁ 6.6821e-10 0.00013845 1.0609e-05 6.9902e-06 v Pressure -0.0010731 0.020326 0.0011268 -1.765e-21 v k 1.2594e-09 0.0013016 0.00088583 0.0011175 v omega 16.278 1.0313e+05 2667.3 500.93 v TempK 288 341.98 293.7 290.72 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.4776e-14 9.6364e-05 5.9827e-05 7.7663e-05 v CourantNb 2.4129e-09 0.00021323 1.3861e-05 8.011e-06 v FourierNb 0.10928 0.6281 0.19306 0.16393 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9455 4.9456 0.0005098 -5.0707e-07 v volume_forces[Z] -4.9455 4.9456 -0.00050966 6.0647e-07 v ǁvolume_forcesǁ 2.4329e-08 4.9468 0.51642 0.24433 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.91 290.86 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015768 5.5783e-05 3.1264e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.10932 0.6281 0.19307 0.16393 INSTANT 0.612468000E+00 TIME STEP NUMBER 636 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.98143E-05 0.23694E-02 Friction velocity uk : 0.98150E-05 0.23693E-02 Dimensionless distance yplus : 0.65357E-04 0.15764E-01 Friction thermal sca. tstar : -0.20520E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.45903E-04 0.11071E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.98143E-05 0.23694E-02 Friction velocity uk : 0.98150E-05 0.23693E-02 Dimensionless distance yplus : 0.65357E-04 0.15764E-01 Friction thermal sca. tstar : -0.20520E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.45903E-04 0.11071E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34925E-08 3 0.17120E-06 0.28422E-12 0.10816E+01 c Velocity[X] 0.11295E-31 c Velocity[Y] 0.14211E-12 c Velocity[Z] 0.14211E-12 c Pressure 0.11075E-13 17 0.86314E-07 0.86314E-07 0.12592E+01 c k 0.39849E-06 2 0.45612E-07 0.35085E-08 0.16291E+01 c omega 0.13153E+02 1 0.16805E-08 0.39477E+00 0.32710E-02 c TempK 0.94623E+02 1 0.11642E-06 0.26748E-01 0.18121E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.0292e-13 8.5757e-14 -1.0612e-17 -2.738e-18 v Velocity[Y] -0.00012933 0.00012428 -9.121e-10 -3.7158e-12 v Velocity[Z] -0.00012426 0.00012934 6.7137e-10 -1.5481e-12 v ǁVelocityǁ 6.6342e-10 0.00013839 1.0611e-05 6.9961e-06 v Pressure -0.0010748 0.020342 0.0011279 8.1384e-20 v k 1.2542e-09 0.0012997 0.00088437 0.0011157 v omega 16.257 1.0313e+05 2667.3 500.91 v TempK 288 341.98 293.7 290.72 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.4715e-14 9.6351e-05 5.9805e-05 7.7637e-05 v CourantNb 2.4163e-09 0.00021311 1.386e-05 8.014e-06 v FourierNb 0.10917 0.6281 0.19301 0.16388 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9456 4.9456 0.00051004 -5.0744e-07 v volume_forces[Z] -4.9456 4.9456 -0.00050991 6.0688e-07 v ǁvolume_forcesǁ 2.4156e-08 4.9468 0.51667 0.24452 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.91 290.86 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015764 5.5766e-05 3.1254e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.10921 0.6281 0.19302 0.16389 INSTANT 0.613431000E+00 TIME STEP NUMBER 637 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.97753E-05 0.23687E-02 Friction velocity uk : 0.97761E-05 0.23686E-02 Dimensionless distance yplus : 0.65098E-04 0.15759E-01 Friction thermal sca. tstar : -0.20137E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.45721E-04 0.11068E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.97753E-05 0.23687E-02 Friction velocity uk : 0.97761E-05 0.23686E-02 Dimensionless distance yplus : 0.65098E-04 0.15759E-01 Friction thermal sca. tstar : -0.20137E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.45721E-04 0.11068E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34934E-08 3 0.17078E-06 0.28366E-12 0.10805E+01 c Velocity[X] 0.11241E-31 c Velocity[Y] 0.14183E-12 c Velocity[Z] 0.14183E-12 c Pressure 0.11081E-13 17 0.86358E-07 0.86358E-07 0.12571E+01 c k 0.39788E-06 2 0.45517E-07 0.34888E-08 0.16271E+01 c omega 0.13153E+02 1 0.16753E-08 0.39270E+00 0.32624E-02 c TempK 0.94624E+02 1 0.11616E-06 0.26685E-01 0.18099E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.0284e-13 8.5696e-14 -1.0604e-17 -2.7362e-18 v Velocity[Y] -0.00012927 0.00012422 -9.1027e-10 -3.5305e-12 v Velocity[Z] -0.0001242 0.00012928 6.6968e-10 -1.2948e-12 v ǁVelocityǁ 6.5869e-10 0.00013833 1.0614e-05 7.002e-06 v Pressure -0.0010764 0.020357 0.001129 -2.9416e-20 v k 1.2491e-09 0.0012979 0.0008829 0.001114 v omega 16.236 1.0313e+05 2667.3 500.9 v TempK 288 341.98 293.7 290.72 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.4654e-14 9.6338e-05 5.9782e-05 7.7612e-05 v CourantNb 2.4196e-09 0.00021298 1.3859e-05 8.0171e-06 v FourierNb 0.10905 0.6281 0.19296 0.16383 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9457 4.9457 0.00051029 -5.078e-07 v volume_forces[Z] -4.9457 4.9457 -0.00051015 6.0729e-07 v ǁvolume_forcesǁ 2.3983e-08 4.9469 0.51691 0.24472 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.91 290.86 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015759 5.5749e-05 3.1243e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.1091 0.6281 0.19297 0.16384 INSTANT 0.614394000E+00 TIME STEP NUMBER 638 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.97367E-05 0.23679E-02 Friction velocity uk : 0.97374E-05 0.23679E-02 Dimensionless distance yplus : 0.64841E-04 0.15754E-01 Friction thermal sca. tstar : -0.19774E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.45540E-04 0.11064E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.97367E-05 0.23679E-02 Friction velocity uk : 0.97374E-05 0.23679E-02 Dimensionless distance yplus : 0.64841E-04 0.15754E-01 Friction thermal sca. tstar : -0.19774E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.45540E-04 0.11064E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34944E-08 3 0.17030E-06 0.28309E-12 0.10794E+01 c Velocity[X] 0.11188E-31 c Velocity[Y] 0.14154E-12 c Velocity[Z] 0.14155E-12 c Pressure 0.11022E-13 17 0.85896E-07 0.85896E-07 0.12551E+01 c k 0.39727E-06 2 0.45422E-07 0.34692E-08 0.16250E+01 c omega 0.13153E+02 1 0.16700E-08 0.39065E+00 0.32539E-02 c TempK 0.94624E+02 1 0.11590E-06 0.26623E-01 0.18078E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.0277e-13 8.5635e-14 -1.0597e-17 -2.7345e-18 v Velocity[Y] -0.00012922 0.00012416 -9.0862e-10 -3.5137e-12 v Velocity[Z] -0.00012414 0.00012922 6.6771e-10 -1.302e-12 v ǁVelocityǁ 6.5386e-10 0.00013827 1.0617e-05 7.0079e-06 v Pressure -0.0010781 0.020373 0.0011301 4.1574e-20 v k 1.2439e-09 0.0012961 0.00088145 0.0011122 v omega 16.215 1.0313e+05 2667.3 500.88 v TempK 288 341.98 293.7 290.72 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.4594e-14 9.6326e-05 5.976e-05 7.7586e-05 v CourantNb 2.423e-09 0.00021286 1.3857e-05 8.0201e-06 v FourierNb 0.10894 0.6281 0.19291 0.16379 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9457 4.9458 0.00051053 -5.0816e-07 v volume_forces[Z] -4.9457 4.9458 -0.0005104 6.077e-07 v ǁvolume_forcesǁ 2.3812e-08 4.947 0.51715 0.24491 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.92 290.87 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015754 5.5732e-05 3.1233e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.10898 0.6281 0.19293 0.16379 INSTANT 0.615357000E+00 TIME STEP NUMBER 639 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.96970E-05 0.23672E-02 Friction velocity uk : 0.96978E-05 0.23671E-02 Dimensionless distance yplus : 0.64576E-04 0.15749E-01 Friction thermal sca. tstar : -0.19430E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.45354E-04 0.11061E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.96970E-05 0.23672E-02 Friction velocity uk : 0.96978E-05 0.23671E-02 Dimensionless distance yplus : 0.64576E-04 0.15749E-01 Friction thermal sca. tstar : -0.19430E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.45354E-04 0.11061E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34953E-08 3 0.16986E-06 0.28253E-12 0.10784E+01 c Velocity[X] 0.11136E-31 c Velocity[Y] 0.14126E-12 c Velocity[Z] 0.14127E-12 c Pressure 0.10995E-13 17 0.85686E-07 0.85686E-07 0.12530E+01 c k 0.39666E-06 2 0.45328E-07 0.34498E-08 0.16230E+01 c omega 0.13153E+02 1 0.16648E-08 0.38861E+00 0.32454E-02 c TempK 0.94625E+02 1 0.11565E-06 0.26560E-01 0.18057E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.0269e-13 8.5573e-14 -1.059e-17 -2.7327e-18 v Velocity[Y] -0.00012916 0.00012409 -9.0697e-10 -3.5126e-12 v Velocity[Z] -0.00012407 0.00012916 6.6574e-10 -1.3014e-12 v ǁVelocityǁ 6.4902e-10 0.0001382 1.062e-05 7.0138e-06 v Pressure -0.0010798 0.020389 0.0011312 -9.0209e-20 v k 1.2388e-09 0.0012942 0.00087999 0.0011104 v omega 16.194 1.0313e+05 2667.2 500.86 v TempK 288 341.98 293.71 290.73 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.4534e-14 9.6313e-05 5.9737e-05 7.756e-05 v CourantNb 2.4264e-09 0.00021273 1.3856e-05 8.0232e-06 v FourierNb 0.10883 0.6281 0.19286 0.16374 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9458 4.9458 0.00051078 -5.0852e-07 v volume_forces[Z] -4.9458 4.9458 -0.00051064 6.081e-07 v ǁvolume_forcesǁ 2.3637e-08 4.947 0.5174 0.2451 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.92 290.87 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015749 5.5714e-05 3.1222e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.10887 0.6281 0.19288 0.16375 INSTANT 0.616320000E+00 TIME STEP NUMBER 640 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.96571E-05 0.23665E-02 Friction velocity uk : 0.96578E-05 0.23664E-02 Dimensionless distance yplus : 0.64310E-04 0.15744E-01 Friction thermal sca. tstar : -0.19103E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.45167E-04 0.11058E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.96571E-05 0.23665E-02 Friction velocity uk : 0.96578E-05 0.23664E-02 Dimensionless distance yplus : 0.64310E-04 0.15744E-01 Friction thermal sca. tstar : -0.19103E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.45167E-04 0.11058E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34963E-08 3 0.16941E-06 0.28197E-12 0.10773E+01 c Velocity[X] 0.11084E-31 c Velocity[Y] 0.14098E-12 c Velocity[Z] 0.14099E-12 c Pressure 0.10970E-13 17 0.85487E-07 0.85487E-07 0.12510E+01 c k 0.39606E-06 2 0.45234E-07 0.34305E-08 0.16209E+01 c omega 0.13153E+02 1 0.16596E-08 0.38658E+00 0.32369E-02 c TempK 0.94625E+02 1 0.11539E-06 0.26499E-01 0.18036E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.0262e-13 8.5512e-14 -1.0582e-17 -2.7309e-18 v Velocity[Y] -0.0001291 0.00012403 -9.0531e-10 -3.506e-12 v Velocity[Z] -0.00012401 0.0001291 6.6376e-10 -1.3027e-12 v ǁVelocityǁ 6.4418e-10 0.00013814 1.0623e-05 7.0198e-06 v Pressure -0.0010815 0.020405 0.0011323 -8.8248e-22 v k 1.2338e-09 0.0012924 0.00087854 0.0011087 v omega 16.174 1.0313e+05 2667.2 500.84 v TempK 288 341.98 293.71 290.73 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.4475e-14 9.63e-05 5.9715e-05 7.7535e-05 v CourantNb 2.4298e-09 0.00021261 1.3855e-05 8.0262e-06 v FourierNb 0.10872 0.6281 0.19282 0.16369 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9459 4.9459 0.00051102 -5.0889e-07 v volume_forces[Z] -4.9459 4.9459 -0.00051089 6.0851e-07 v ǁvolume_forcesǁ 2.3462e-08 4.9471 0.51764 0.24529 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.92 290.87 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015744 5.5697e-05 3.1212e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.10876 0.6281 0.19283 0.1637 INSTANT 0.617283000E+00 TIME STEP NUMBER 641 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.96169E-05 0.23657E-02 Friction velocity uk : 0.96177E-05 0.23657E-02 Dimensionless distance yplus : 0.64043E-04 0.15739E-01 Friction thermal sca. tstar : -0.18792E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.44980E-04 0.11054E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.96169E-05 0.23657E-02 Friction velocity uk : 0.96177E-05 0.23657E-02 Dimensionless distance yplus : 0.64043E-04 0.15739E-01 Friction thermal sca. tstar : -0.18792E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.44980E-04 0.11054E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34972E-08 3 0.24657E-06 0.28141E-12 0.10763E+01 c Velocity[X] 0.11032E-31 c Velocity[Y] 0.14070E-12 c Velocity[Z] 0.14071E-12 c Pressure 0.10958E-13 17 0.85392E-07 0.85392E-07 0.12489E+01 c k 0.39545E-06 2 0.45140E-07 0.34113E-08 0.16189E+01 c omega 0.13153E+02 1 0.16544E-08 0.38457E+00 0.32285E-02 c TempK 0.94626E+02 1 0.11514E-06 0.26437E-01 0.18014E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.0254e-13 8.5451e-14 -1.0575e-17 -2.7292e-18 v Velocity[Y] -0.00012904 0.00012397 -9.0365e-10 -3.4996e-12 v Velocity[Z] -0.00012395 0.00012905 6.6178e-10 -1.3046e-12 v ǁVelocityǁ 6.3933e-10 0.00013808 1.0626e-05 7.0257e-06 v Pressure -0.0010832 0.02042 0.0011334 -1.9611e-22 v k 1.2287e-09 0.0012906 0.0008771 0.0011069 v omega 16.153 1.0313e+05 2667.2 500.82 v TempK 288 341.98 293.71 290.73 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.4416e-14 9.6288e-05 5.9692e-05 7.7509e-05 v CourantNb 2.4331e-09 0.00021248 1.3854e-05 8.0293e-06 v FourierNb 0.10861 0.6281 0.19277 0.16365 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9459 4.946 0.00051127 -5.0925e-07 v volume_forces[Z] -4.9459 4.946 -0.00051113 6.0892e-07 v ǁvolume_forcesǁ 2.3287e-08 4.9472 0.51788 0.24548 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.93 290.87 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015739 5.568e-05 3.1201e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.10865 0.6281 0.19278 0.16365 INSTANT 0.618246000E+00 TIME STEP NUMBER 642 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.95765E-05 0.23650E-02 Friction velocity uk : 0.95773E-05 0.23650E-02 Dimensionless distance yplus : 0.63774E-04 0.15734E-01 Friction thermal sca. tstar : -0.18496E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.44791E-04 0.11051E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.95765E-05 0.23650E-02 Friction velocity uk : 0.95773E-05 0.23650E-02 Dimensionless distance yplus : 0.63774E-04 0.15734E-01 Friction thermal sca. tstar : -0.18496E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.44791E-04 0.11051E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34982E-08 3 0.16852E-06 0.28085E-12 0.10752E+01 c Velocity[X] 0.10980E-31 c Velocity[Y] 0.14042E-12 c Velocity[Z] 0.14043E-12 c Pressure 0.10951E-13 17 0.85338E-07 0.85338E-07 0.12469E+01 c k 0.39485E-06 2 0.45047E-07 0.33923E-08 0.16168E+01 c omega 0.13153E+02 1 0.16493E-08 0.38257E+00 0.32200E-02 c TempK 0.94627E+02 1 0.11489E-06 0.26375E-01 0.17993E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.0247e-13 8.5391e-14 -1.0568e-17 -2.7274e-18 v Velocity[Y] -0.00012899 0.00012391 -9.0197e-10 -3.4933e-12 v Velocity[Z] -0.00012389 0.00012899 6.5979e-10 -1.3063e-12 v ǁVelocityǁ 6.3447e-10 0.00013802 1.0629e-05 7.0317e-06 v Pressure -0.0010848 0.020436 0.0011345 4.0202e-20 v k 1.2237e-09 0.0012888 0.00087565 0.0011052 v omega 16.133 1.0313e+05 2667.2 500.8 v TempK 288 341.98 293.72 290.73 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.4357e-14 9.6275e-05 5.967e-05 7.7484e-05 v CourantNb 2.4365e-09 0.00021236 1.3852e-05 8.0323e-06 v FourierNb 0.1085 0.6281 0.19272 0.1636 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.946 4.946 0.00051151 -5.0961e-07 v volume_forces[Z] -4.946 4.946 -0.00051137 6.0932e-07 v ǁvolume_forcesǁ 2.3112e-08 4.9472 0.51813 0.24568 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.93 290.87 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015734 5.5663e-05 3.1191e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.10854 0.6281 0.19273 0.16361 INSTANT 0.619209000E+00 TIME STEP NUMBER 643 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.95358E-05 0.23643E-02 Friction velocity uk : 0.95366E-05 0.23642E-02 Dimensionless distance yplus : 0.63503E-04 0.15730E-01 Friction thermal sca. tstar : -0.18213E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.44600E-04 0.11047E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.95358E-05 0.23643E-02 Friction velocity uk : 0.95366E-05 0.23642E-02 Dimensionless distance yplus : 0.63503E-04 0.15730E-01 Friction thermal sca. tstar : -0.18213E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.44600E-04 0.11047E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.34991E-08 3 0.16806E-06 0.28029E-12 0.10741E+01 c Velocity[X] 0.10929E-31 c Velocity[Y] 0.14015E-12 c Velocity[Z] 0.14015E-12 c Pressure 0.10894E-13 17 0.84893E-07 0.84893E-07 0.12449E+01 c k 0.39425E-06 2 0.44954E-07 0.33734E-08 0.16148E+01 c omega 0.13153E+02 1 0.16441E-08 0.38058E+00 0.32117E-02 c TempK 0.94627E+02 1 0.11463E-06 0.26314E-01 0.17972E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.0239e-13 8.533e-14 -1.056e-17 -2.7257e-18 v Velocity[Y] -0.00012893 0.00012385 -9.003e-10 -3.4869e-12 v Velocity[Z] -0.00012383 0.00012893 6.578e-10 -1.308e-12 v ǁVelocityǁ 6.2961e-10 0.00013796 1.0632e-05 7.0376e-06 v Pressure -0.0010865 0.020452 0.0011356 8.6335e-20 v k 1.2187e-09 0.001287 0.00087422 0.0011034 v omega 16.112 1.0313e+05 2667.2 500.79 v TempK 288 341.98 293.72 290.73 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.4298e-14 9.6263e-05 5.9647e-05 7.7458e-05 v CourantNb 2.4399e-09 0.00021223 1.3851e-05 8.0354e-06 v FourierNb 0.10839 0.6281 0.19267 0.16355 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9461 4.9461 0.00051175 -5.0998e-07 v volume_forces[Z] -4.9461 4.9461 -0.00051162 6.0973e-07 v ǁvolume_forcesǁ 2.2936e-08 4.9473 0.51837 0.24587 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.93 290.88 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.01573 5.5646e-05 3.1181e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.10843 0.6281 0.19269 0.16356 INSTANT 0.620172000E+00 TIME STEP NUMBER 644 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.94949E-05 0.23636E-02 Friction velocity uk : 0.94956E-05 0.23635E-02 Dimensionless distance yplus : 0.63230E-04 0.15725E-01 Friction thermal sca. tstar : -0.17943E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.44409E-04 0.11044E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.94949E-05 0.23636E-02 Friction velocity uk : 0.94956E-05 0.23635E-02 Dimensionless distance yplus : 0.63230E-04 0.15725E-01 Friction thermal sca. tstar : -0.17943E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.44409E-04 0.11044E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.35001E-08 3 0.16763E-06 0.27974E-12 0.10731E+01 c Velocity[X] 0.10878E-31 c Velocity[Y] 0.13987E-12 c Velocity[Z] 0.13987E-12 c Pressure 0.10898E-13 17 0.84918E-07 0.84918E-07 0.12429E+01 c k 0.39365E-06 2 0.44861E-07 0.33546E-08 0.16127E+01 c omega 0.13153E+02 1 0.16390E-08 0.37860E+00 0.32033E-02 c TempK 0.94628E+02 1 0.11438E-06 0.26253E-01 0.17951E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.0232e-13 8.5269e-14 -1.0553e-17 -2.7239e-18 v Velocity[Y] -0.00012887 0.00012379 -8.9861e-10 -3.4805e-12 v Velocity[Z] -0.00012376 0.00012888 6.5581e-10 -1.3097e-12 v ǁVelocityǁ 6.2474e-10 0.0001379 1.0635e-05 7.0436e-06 v Pressure -0.0010882 0.020467 0.0011367 2.7945e-21 v k 1.2138e-09 0.0012852 0.00087278 0.0011017 v omega 16.092 1.0313e+05 2667.2 500.77 v TempK 288 341.98 293.72 290.74 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.424e-14 9.625e-05 5.9625e-05 7.7433e-05 v CourantNb 2.4432e-09 0.00021211 1.385e-05 8.0385e-06 v FourierNb 0.10828 0.6281 0.19263 0.16351 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9461 4.9462 0.000512 -5.1034e-07 v volume_forces[Z] -4.9461 4.9462 -0.00051186 6.1013e-07 v ǁvolume_forcesǁ 2.276e-08 4.9474 0.51861 0.24606 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.93 290.88 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015725 5.5629e-05 3.117e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.10832 0.6281 0.19264 0.16352 INSTANT 0.621135000E+00 TIME STEP NUMBER 645 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.94536E-05 0.23628E-02 Friction velocity uk : 0.94543E-05 0.23628E-02 Dimensionless distance yplus : 0.62955E-04 0.15720E-01 Friction thermal sca. tstar : -0.17684E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.44216E-04 0.11041E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.94536E-05 0.23628E-02 Friction velocity uk : 0.94543E-05 0.23628E-02 Dimensionless distance yplus : 0.62955E-04 0.15720E-01 Friction thermal sca. tstar : -0.17684E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.44216E-04 0.11041E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.35011E-08 3 0.25519E-06 0.27919E-12 0.10720E+01 c Velocity[X] 0.10827E-31 c Velocity[Y] 0.13959E-12 c Velocity[Z] 0.13959E-12 c Pressure 0.10871E-13 17 0.84705E-07 0.84705E-07 0.12408E+01 c k 0.39305E-06 2 0.44769E-07 0.33359E-08 0.16107E+01 c omega 0.13153E+02 1 0.16339E-08 0.37664E+00 0.31950E-02 c TempK 0.94628E+02 1 0.11413E-06 0.26193E-01 0.17931E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.0224e-13 8.5209e-14 -1.0546e-17 -2.7222e-18 v Velocity[Y] -0.00012882 0.00012372 -8.9693e-10 -3.4742e-12 v Velocity[Z] -0.0001237 0.00012882 6.5381e-10 -1.3114e-12 v ǁVelocityǁ 6.1985e-10 0.00013784 1.0638e-05 7.0495e-06 v Pressure -0.0010899 0.020483 0.0011378 1.0099e-20 v k 1.2089e-09 0.0012834 0.00087135 0.0011 v omega 16.071 1.0313e+05 2667.2 500.75 v TempK 288 341.98 293.72 290.74 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.4182e-14 9.6238e-05 5.9603e-05 7.7407e-05 v CourantNb 2.4466e-09 0.00021199 1.3849e-05 8.0416e-06 v FourierNb 0.10817 0.6281 0.19258 0.16346 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9462 4.9462 0.00051224 -5.107e-07 v volume_forces[Z] -4.9462 4.9462 -0.0005121 6.1053e-07 v ǁvolume_forcesǁ 2.2584e-08 4.9474 0.51885 0.24625 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.94 290.88 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.01572 5.5612e-05 3.116e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.10821 0.6281 0.19259 0.16347 INSTANT 0.622098000E+00 TIME STEP NUMBER 646 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.94120E-05 0.23621E-02 Friction velocity uk : 0.94127E-05 0.23621E-02 Dimensionless distance yplus : 0.62678E-04 0.15715E-01 Friction thermal sca. tstar : -0.17436E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.44021E-04 0.11037E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.94120E-05 0.23621E-02 Friction velocity uk : 0.94127E-05 0.23621E-02 Dimensionless distance yplus : 0.62678E-04 0.15715E-01 Friction thermal sca. tstar : -0.17436E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.44021E-04 0.11037E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.35021E-08 3 0.16674E-06 0.27863E-12 0.10710E+01 c Velocity[X] 0.10776E-31 c Velocity[Y] 0.13932E-12 c Velocity[Z] 0.13932E-12 c Pressure 0.10837E-13 17 0.84440E-07 0.84440E-07 0.12388E+01 c k 0.39246E-06 2 0.44677E-07 0.33174E-08 0.16087E+01 c omega 0.13153E+02 1 0.16289E-08 0.37469E+00 0.31867E-02 c TempK 0.94629E+02 1 0.11388E-06 0.26132E-01 0.17910E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.0217e-13 8.5149e-14 -1.0539e-17 -2.7204e-18 v Velocity[Y] -0.00012876 0.00012366 -8.9523e-10 -3.4678e-12 v Velocity[Z] -0.00012364 0.00012876 6.518e-10 -1.313e-12 v ǁVelocityǁ 6.1496e-10 0.00013778 1.0641e-05 7.0555e-06 v Pressure -0.0010915 0.020499 0.0011389 3.7554e-20 v k 1.204e-09 0.0012816 0.00086993 0.0010982 v omega 16.051 1.0313e+05 2667.1 500.73 v TempK 288 341.98 293.73 290.74 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.4125e-14 9.6225e-05 5.9581e-05 7.7382e-05 v CourantNb 2.45e-09 0.00021186 1.3848e-05 8.0447e-06 v FourierNb 0.10806 0.6281 0.19253 0.16342 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9463 4.9463 0.00051248 -5.1106e-07 v volume_forces[Z] -4.9463 4.9463 -0.00051235 6.1093e-07 v ǁvolume_forcesǁ 2.2408e-08 4.9475 0.51909 0.24644 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.94 290.88 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015715 5.5595e-05 3.115e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.1081 0.6281 0.19254 0.16342 INSTANT 0.623061000E+00 TIME STEP NUMBER 647 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.93701E-05 0.23614E-02 Friction velocity uk : 0.93708E-05 0.23613E-02 Dimensionless distance yplus : 0.62399E-04 0.15710E-01 Friction thermal sca. tstar : -0.17198E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.43825E-04 0.11034E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.93701E-05 0.23614E-02 Friction velocity uk : 0.93708E-05 0.23613E-02 Dimensionless distance yplus : 0.62399E-04 0.15710E-01 Friction thermal sca. tstar : -0.17198E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.43825E-04 0.11034E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.35031E-08 3 0.16629E-06 0.27808E-12 0.10699E+01 c Velocity[X] 0.10726E-31 c Velocity[Y] 0.13904E-12 c Velocity[Z] 0.13904E-12 c Pressure 0.10802E-13 17 0.84167E-07 0.84167E-07 0.12368E+01 c k 0.39186E-06 2 0.44585E-07 0.32990E-08 0.16067E+01 c omega 0.13153E+02 1 0.16238E-08 0.37275E+00 0.31785E-02 c TempK 0.94629E+02 1 0.11363E-06 0.26072E-01 0.17889E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.021e-13 8.5089e-14 -1.0531e-17 -2.7187e-18 v Velocity[Y] -0.0001287 0.0001236 -8.9353e-10 -3.4615e-12 v Velocity[Z] -0.00012358 0.00012871 6.4979e-10 -1.3147e-12 v ǁVelocityǁ 6.1006e-10 0.00013773 1.0644e-05 7.0614e-06 v Pressure -0.0010932 0.020514 0.00114 1.2894e-20 v k 1.1991e-09 0.0012798 0.00086851 0.0010965 v omega 16.031 1.0313e+05 2667.1 500.71 v TempK 288 341.99 293.73 290.74 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.4067e-14 9.6212e-05 5.9558e-05 7.7356e-05 v CourantNb 2.4533e-09 0.00021174 1.3847e-05 8.0478e-06 v FourierNb 0.10795 0.6281 0.19248 0.16337 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9463 4.9464 0.00051272 -5.1142e-07 v volume_forces[Z] -4.9463 4.9464 -0.00051259 6.1134e-07 v ǁvolume_forcesǁ 2.2231e-08 4.9476 0.51934 0.24663 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.94 290.88 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.01571 5.5578e-05 3.1139e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.10799 0.6281 0.1925 0.16338 INSTANT 0.624024000E+00 TIME STEP NUMBER 648 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.93279E-05 0.23607E-02 Friction velocity uk : 0.93286E-05 0.23606E-02 Dimensionless distance yplus : 0.62118E-04 0.15706E-01 Friction thermal sca. tstar : -0.16969E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.43628E-04 0.11031E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.93279E-05 0.23607E-02 Friction velocity uk : 0.93286E-05 0.23606E-02 Dimensionless distance yplus : 0.62118E-04 0.15706E-01 Friction thermal sca. tstar : -0.16969E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.43628E-04 0.11031E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.35041E-08 3 0.16586E-06 0.27753E-12 0.10689E+01 c Velocity[X] 0.10676E-31 c Velocity[Y] 0.13876E-12 c Velocity[Z] 0.13877E-12 c Pressure 0.10788E-13 17 0.84054E-07 0.84054E-07 0.12348E+01 c k 0.39127E-06 2 0.44494E-07 0.32808E-08 0.16047E+01 c omega 0.13153E+02 1 0.16188E-08 0.37082E+00 0.31702E-02 c TempK 0.94630E+02 1 0.11339E-06 0.26012E-01 0.17868E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.0202e-13 8.5029e-14 -1.0524e-17 -2.717e-18 v Velocity[Y] -0.00012865 0.00012354 -8.9183e-10 -3.4553e-12 v Velocity[Z] -0.00012352 0.00012865 6.4778e-10 -1.3164e-12 v ǁVelocityǁ 6.0515e-10 0.00013768 1.0647e-05 7.0674e-06 v Pressure -0.0010949 0.02053 0.001141 8.6483e-20 v k 1.1942e-09 0.001278 0.00086709 0.0010948 v omega 16.01 1.0313e+05 2667.1 500.69 v TempK 288 341.99 293.73 290.74 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.4011e-14 9.62e-05 5.9536e-05 7.7331e-05 v CourantNb 2.4566e-09 0.00021162 1.3846e-05 8.0509e-06 v FourierNb 0.10784 0.6281 0.19244 0.16332 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9464 4.9464 0.00051297 -5.1178e-07 v volume_forces[Z] -4.9464 4.9464 -0.00051283 6.1174e-07 v ǁvolume_forcesǁ 2.2054e-08 4.9476 0.51958 0.24682 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.94 290.89 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015706 5.5561e-05 3.1129e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.10788 0.6281 0.19245 0.16333 INSTANT 0.624987000E+00 TIME STEP NUMBER 649 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.92854E-05 0.23600E-02 Friction velocity uk : 0.92861E-05 0.23599E-02 Dimensionless distance yplus : 0.61835E-04 0.15701E-01 Friction thermal sca. tstar : -0.16749E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.43429E-04 0.11027E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.92854E-05 0.23600E-02 Friction velocity uk : 0.92861E-05 0.23599E-02 Dimensionless distance yplus : 0.61835E-04 0.15701E-01 Friction thermal sca. tstar : -0.16749E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.43429E-04 0.11027E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.35051E-08 3 0.16542E-06 0.27698E-12 0.10678E+01 c Velocity[X] 0.10626E-31 c Velocity[Y] 0.13849E-12 c Velocity[Z] 0.13849E-12 c Pressure 0.10763E-13 17 0.83859E-07 0.83859E-07 0.12328E+01 c k 0.39068E-06 2 0.44403E-07 0.32626E-08 0.16027E+01 c omega 0.13153E+02 1 0.16138E-08 0.36891E+00 0.31620E-02 c TempK 0.94631E+02 1 0.11314E-06 0.25952E-01 0.17847E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.0195e-13 8.4969e-14 -1.0517e-17 -2.7153e-18 v Velocity[Y] -0.00012859 0.00012348 -8.9012e-10 -3.449e-12 v Velocity[Z] -0.00012346 0.0001286 6.4576e-10 -1.318e-12 v ǁVelocityǁ 6.0024e-10 0.00013764 1.065e-05 7.0734e-06 v Pressure -0.0010966 0.020546 0.0011421 -1.4311e-19 v k 1.1894e-09 0.0012762 0.00086568 0.0010931 v omega 15.99 1.0313e+05 2667.1 500.68 v TempK 288 341.99 293.73 290.75 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.3954e-14 9.6187e-05 5.9514e-05 7.7306e-05 v CourantNb 2.46e-09 0.00021149 1.3844e-05 8.054e-06 v FourierNb 0.10773 0.6281 0.19239 0.16328 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9465 4.9465 0.00051321 -5.1213e-07 v volume_forces[Z] -4.9465 4.9465 -0.00051307 6.1214e-07 v ǁvolume_forcesǁ 2.1876e-08 4.9477 0.51982 0.24701 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.95 290.89 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015701 5.5544e-05 3.1119e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.10778 0.6281 0.1924 0.16329 INSTANT 0.625950000E+00 TIME STEP NUMBER 650 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.92426E-05 0.23592E-02 Friction velocity uk : 0.92433E-05 0.23592E-02 Dimensionless distance yplus : 0.61550E-04 0.15696E-01 Friction thermal sca. tstar : -0.16538E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.43229E-04 0.11024E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.92426E-05 0.23592E-02 Friction velocity uk : 0.92433E-05 0.23592E-02 Dimensionless distance yplus : 0.61550E-04 0.15696E-01 Friction thermal sca. tstar : -0.16538E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.43229E-04 0.11024E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.35061E-08 3 0.16498E-06 0.27644E-12 0.10667E+01 c Velocity[X] 0.10577E-31 c Velocity[Y] 0.13822E-12 c Velocity[Z] 0.13822E-12 c Pressure 0.10721E-13 17 0.83532E-07 0.83532E-07 0.12309E+01 c k 0.39009E-06 2 0.44312E-07 0.32446E-08 0.16007E+01 c omega 0.13153E+02 1 0.16088E-08 0.36701E+00 0.31539E-02 c TempK 0.94631E+02 1 0.11289E-06 0.25892E-01 0.17827E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.0188e-13 8.4909e-14 -1.051e-17 -2.7135e-18 v Velocity[Y] -0.00012854 0.00012342 -8.884e-10 -3.4428e-12 v Velocity[Z] -0.0001234 0.00012854 6.4374e-10 -1.3197e-12 v ǁVelocityǁ 5.9531e-10 0.00013759 1.0653e-05 7.0793e-06 v Pressure -0.0010983 0.020561 0.0011432 3.373e-20 v k 1.1846e-09 0.0012745 0.00086427 0.0010914 v omega 15.97 1.0313e+05 2667.1 500.66 v TempK 288 341.99 293.74 290.75 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.3898e-14 9.6175e-05 5.9492e-05 7.728e-05 v CourantNb 2.4633e-09 0.00021137 1.3843e-05 8.0571e-06 v FourierNb 0.10763 0.6281 0.19234 0.16323 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9465 4.9466 0.00051345 -5.1249e-07 v volume_forces[Z] -4.9465 4.9466 -0.00051331 6.1253e-07 v ǁvolume_forcesǁ 2.1699e-08 4.9478 0.52006 0.2472 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.95 290.89 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015696 5.5527e-05 3.1109e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.10767 0.6281 0.19236 0.16324 INSTANT 0.626913000E+00 TIME STEP NUMBER 651 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.91994E-05 0.23585E-02 Friction velocity uk : 0.92001E-05 0.23585E-02 Dimensionless distance yplus : 0.61263E-04 0.15691E-01 Friction thermal sca. tstar : -0.16334E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.43027E-04 0.11021E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.91994E-05 0.23585E-02 Friction velocity uk : 0.92001E-05 0.23585E-02 Dimensionless distance yplus : 0.61263E-04 0.15691E-01 Friction thermal sca. tstar : -0.16334E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.43027E-04 0.11021E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.35071E-08 3 0.16455E-06 0.27589E-12 0.10657E+01 c Velocity[X] 0.10528E-31 c Velocity[Y] 0.13794E-12 c Velocity[Z] 0.13795E-12 c Pressure 0.10728E-13 17 0.83583E-07 0.83583E-07 0.12289E+01 c k 0.38950E-06 2 0.44222E-07 0.32267E-08 0.15987E+01 c omega 0.13153E+02 1 0.16038E-08 0.36512E+00 0.31458E-02 c TempK 0.94632E+02 1 0.11265E-06 0.25833E-01 0.17806E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.018e-13 8.4849e-14 -1.0503e-17 -2.7118e-18 v Velocity[Y] -0.00012848 0.00012336 -8.8668e-10 -3.4366e-12 v Velocity[Z] -0.00012334 0.00012848 6.4171e-10 -1.3213e-12 v ǁVelocityǁ 5.9038e-10 0.00013754 1.0656e-05 7.0853e-06 v Pressure -0.0010999 0.020577 0.0011443 -6.6872e-20 v k 1.1799e-09 0.0012727 0.00086287 0.0010897 v omega 15.95 1.0313e+05 2667.1 500.64 v TempK 288 341.99 293.74 290.75 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.3842e-14 9.6163e-05 5.947e-05 7.7255e-05 v CourantNb 2.4667e-09 0.00021125 1.3842e-05 8.0602e-06 v FourierNb 0.10752 0.6281 0.1923 0.16319 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9466 4.9466 0.00051369 -5.1285e-07 v volume_forces[Z] -4.9466 4.9466 -0.00051356 6.1293e-07 v ǁvolume_forcesǁ 2.1521e-08 4.9478 0.5203 0.24739 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.95 290.89 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015691 5.551e-05 3.1098e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.10756 0.6281 0.19231 0.1632 INSTANT 0.627876000E+00 TIME STEP NUMBER 652 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.91559E-05 0.23578E-02 Friction velocity uk : 0.91566E-05 0.23578E-02 Dimensionless distance yplus : 0.60973E-04 0.15687E-01 Friction thermal sca. tstar : -0.16137E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.42824E-04 0.11017E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.91559E-05 0.23578E-02 Friction velocity uk : 0.91566E-05 0.23578E-02 Dimensionless distance yplus : 0.60973E-04 0.15687E-01 Friction thermal sca. tstar : -0.16137E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.42824E-04 0.11017E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.35081E-08 3 0.16418E-06 0.27534E-12 0.10646E+01 c Velocity[X] 0.10478E-31 c Velocity[Y] 0.13767E-12 c Velocity[Z] 0.13767E-12 c Pressure 0.10750E-13 17 0.83755E-07 0.83755E-07 0.12269E+01 c k 0.38892E-06 2 0.44132E-07 0.32089E-08 0.15967E+01 c omega 0.13153E+02 1 0.15989E-08 0.36324E+00 0.31377E-02 c TempK 0.94632E+02 1 0.11240E-06 0.25774E-01 0.17786E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.0173e-13 8.479e-14 -1.0496e-17 -2.7101e-18 v Velocity[Y] -0.00012843 0.0001233 -8.8495e-10 -3.4304e-12 v Velocity[Z] -0.00012328 0.00012843 6.3968e-10 -1.323e-12 v ǁVelocityǁ 5.8544e-10 0.0001375 1.0659e-05 7.0913e-06 v Pressure -0.0011016 0.020593 0.0011454 2.9269e-20 v k 1.1751e-09 0.0012709 0.00086147 0.001088 v omega 15.93 1.0313e+05 2667.1 500.62 v TempK 288 341.99 293.74 290.75 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.3786e-14 9.615e-05 5.9448e-05 7.723e-05 v CourantNb 2.47e-09 0.00021113 1.3841e-05 8.0634e-06 v FourierNb 0.10741 0.6281 0.19225 0.16314 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9467 4.9467 0.00051393 -5.132e-07 v volume_forces[Z] -4.9467 4.9467 -0.0005138 6.1333e-07 v ǁvolume_forcesǁ 2.1342e-08 4.9479 0.52054 0.24758 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.95 290.9 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015687 5.5493e-05 3.1088e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.10745 0.6281 0.19226 0.16315 INSTANT 0.628839000E+00 TIME STEP NUMBER 653 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.91121E-05 0.23571E-02 Friction velocity uk : 0.91128E-05 0.23571E-02 Dimensionless distance yplus : 0.60681E-04 0.15682E-01 Friction thermal sca. tstar : -0.15948E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.42619E-04 0.11014E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.91121E-05 0.23571E-02 Friction velocity uk : 0.91128E-05 0.23571E-02 Dimensionless distance yplus : 0.60681E-04 0.15682E-01 Friction thermal sca. tstar : -0.15948E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.42619E-04 0.11014E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.35091E-08 3 0.16367E-06 0.27480E-12 0.10636E+01 c Velocity[X] 0.10430E-31 c Velocity[Y] 0.13740E-12 c Velocity[Z] 0.13740E-12 c Pressure 0.10649E-13 17 0.82970E-07 0.82970E-07 0.12249E+01 c k 0.38833E-06 2 0.44042E-07 0.31913E-08 0.15947E+01 c omega 0.13153E+02 1 0.15940E-08 0.36138E+00 0.31296E-02 c TempK 0.94633E+02 1 0.11216E-06 0.25715E-01 0.17765E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.0166e-13 8.4731e-14 -1.0488e-17 -2.7084e-18 v Velocity[Y] -0.00012837 0.00012324 -8.8321e-10 -3.4243e-12 v Velocity[Z] -0.00012322 0.00012837 6.3764e-10 -1.3246e-12 v ǁVelocityǁ 5.8049e-10 0.00013745 1.0662e-05 7.0973e-06 v Pressure -0.0011033 0.020608 0.0011465 2.0493e-20 v k 1.1704e-09 0.0012692 0.00086007 0.0010863 v omega 15.91 1.0313e+05 2667 500.6 v TempK 288 341.99 293.74 290.76 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.373e-14 9.6138e-05 5.9426e-05 7.7205e-05 v CourantNb 2.4733e-09 0.00021101 1.384e-05 8.0665e-06 v FourierNb 0.10731 0.6281 0.1922 0.1631 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9467 4.9468 0.00051417 -5.1356e-07 v volume_forces[Z] -4.9467 4.9468 -0.00051404 6.1373e-07 v ǁvolume_forcesǁ 2.1164e-08 4.948 0.52078 0.24777 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.96 290.9 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015682 5.5476e-05 3.1078e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.10735 0.6281 0.19222 0.1631 INSTANT 0.629802000E+00 TIME STEP NUMBER 654 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.90679E-05 0.23564E-02 Friction velocity uk : 0.90686E-05 0.23563E-02 Dimensionless distance yplus : 0.60387E-04 0.15677E-01 Friction thermal sca. tstar : -0.15764E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.42412E-04 0.11011E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.90679E-05 0.23564E-02 Friction velocity uk : 0.90686E-05 0.23563E-02 Dimensionless distance yplus : 0.60387E-04 0.15677E-01 Friction thermal sca. tstar : -0.15764E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.42412E-04 0.11011E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.35101E-08 3 0.16324E-06 0.27426E-12 0.10625E+01 c Velocity[X] 0.10381E-31 c Velocity[Y] 0.13713E-12 c Velocity[Z] 0.13713E-12 c Pressure 0.10631E-13 17 0.82823E-07 0.82823E-07 0.12230E+01 c k 0.38775E-06 2 0.43953E-07 0.31737E-08 0.15927E+01 c omega 0.13153E+02 1 0.15891E-08 0.35952E+00 0.31216E-02 c TempK 0.94634E+02 1 0.11192E-06 0.25656E-01 0.17745E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.0158e-13 8.4672e-14 -1.0481e-17 -2.7067e-18 v Velocity[Y] -0.00012832 0.00012318 -8.8147e-10 -3.4162e-12 v Velocity[Z] -0.00012316 0.00012832 6.356e-10 -1.3258e-12 v ǁVelocityǁ 5.7553e-10 0.00013741 1.0665e-05 7.1033e-06 v Pressure -0.001105 0.020624 0.0011476 2.6082e-20 v k 1.1657e-09 0.0012674 0.00085868 0.0010846 v omega 15.89 1.0313e+05 2667 500.59 v TempK 288 341.99 293.75 290.76 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.3675e-14 9.6125e-05 5.9404e-05 7.718e-05 v CourantNb 2.4767e-09 0.00021089 1.3839e-05 8.0696e-06 v FourierNb 0.1072 0.6281 0.19216 0.16305 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9468 4.9468 0.00051441 -5.1391e-07 v volume_forces[Z] -4.9468 4.9468 -0.00051428 6.1412e-07 v ǁvolume_forcesǁ 2.0985e-08 4.948 0.52102 0.24796 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.96 290.9 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015677 5.5459e-05 3.1068e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.10724 0.6281 0.19217 0.16306 INSTANT 0.630765000E+00 TIME STEP NUMBER 655 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.90234E-05 0.23557E-02 Friction velocity uk : 0.90241E-05 0.23556E-02 Dimensionless distance yplus : 0.60091E-04 0.15672E-01 Friction thermal sca. tstar : -0.15587E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.42204E-04 0.11007E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.90234E-05 0.23557E-02 Friction velocity uk : 0.90241E-05 0.23556E-02 Dimensionless distance yplus : 0.60091E-04 0.15672E-01 Friction thermal sca. tstar : -0.15587E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.42204E-04 0.11007E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.35111E-08 3 0.16282E-06 0.27372E-12 0.10615E+01 c Velocity[X] 0.10333E-31 c Velocity[Y] 0.13686E-12 c Velocity[Z] 0.13686E-12 c Pressure 0.10608E-13 17 0.82644E-07 0.82644E-07 0.12210E+01 c k 0.38717E-06 2 0.43864E-07 0.31563E-08 0.15907E+01 c omega 0.13153E+02 1 0.15842E-08 0.35768E+00 0.31136E-02 c TempK 0.94634E+02 1 0.11168E-06 0.25598E-01 0.17724E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.0151e-13 8.4613e-14 -1.0474e-17 -2.705e-18 v Velocity[Y] -0.00012826 0.00012312 -8.7973e-10 -3.41e-12 v Velocity[Z] -0.0001231 0.00012826 6.3355e-10 -1.3275e-12 v ǁVelocityǁ 5.7057e-10 0.00013736 1.0668e-05 7.1093e-06 v Pressure -0.0011067 0.020639 0.0011486 1.1766e-21 v k 1.161e-09 0.0012657 0.00085729 0.0010829 v omega 15.87 1.0313e+05 2667 500.57 v TempK 288 341.99 293.75 290.76 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.3621e-14 9.6113e-05 5.9382e-05 7.7155e-05 v CourantNb 2.48e-09 0.00021077 1.3838e-05 8.0728e-06 v FourierNb 0.10709 0.6281 0.19211 0.16301 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9469 4.9469 0.00051465 -5.1427e-07 v volume_forces[Z] -4.9469 4.9469 -0.00051452 6.1452e-07 v ǁvolume_forcesǁ 2.0805e-08 4.9481 0.52126 0.24815 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.96 290.9 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015672 5.5443e-05 3.1058e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.10714 0.6281 0.19212 0.16301 INSTANT 0.631728000E+00 TIME STEP NUMBER 656 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.89785E-05 0.23550E-02 Friction velocity uk : 0.89793E-05 0.23549E-02 Dimensionless distance yplus : 0.59792E-04 0.15668E-01 Friction thermal sca. tstar : -0.15415E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.41994E-04 0.11004E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.89785E-05 0.23550E-02 Friction velocity uk : 0.89793E-05 0.23549E-02 Dimensionless distance yplus : 0.59792E-04 0.15668E-01 Friction thermal sca. tstar : -0.15415E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.41994E-04 0.11004E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.35122E-08 3 0.16239E-06 0.27318E-12 0.10604E+01 c Velocity[X] 0.10285E-31 c Velocity[Y] 0.13659E-12 c Velocity[Z] 0.13659E-12 c Pressure 0.10576E-13 17 0.82393E-07 0.82393E-07 0.12191E+01 c k 0.38659E-06 2 0.43775E-07 0.31390E-08 0.15888E+01 c omega 0.13153E+02 1 0.15793E-08 0.35585E+00 0.31056E-02 c TempK 0.94635E+02 1 0.11144E-06 0.25540E-01 0.17704E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.0144e-13 8.4554e-14 -1.0467e-17 -2.7033e-18 v Velocity[Y] -0.00012821 0.00012306 -8.7798e-10 -3.4039e-12 v Velocity[Z] -0.00012304 0.00012821 6.315e-10 -1.329e-12 v ǁVelocityǁ 5.656e-10 0.00013732 1.0671e-05 7.1153e-06 v Pressure -0.0011083 0.020655 0.0011497 5.7998e-20 v k 1.1564e-09 0.0012639 0.00085591 0.0010812 v omega 15.85 1.0313e+05 2667 500.55 v TempK 288 341.99 293.75 290.76 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.3566e-14 9.61e-05 5.936e-05 7.7129e-05 v CourantNb 2.4833e-09 0.00021065 1.3837e-05 8.0759e-06 v FourierNb 0.10699 0.6281 0.19206 0.16296 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9469 4.947 0.00051489 -5.1462e-07 v volume_forces[Z] -4.9469 4.947 -0.00051476 6.1491e-07 v ǁvolume_forcesǁ 2.0626e-08 4.9481 0.52149 0.24834 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.97 290.9 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015668 5.5426e-05 3.1047e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.10703 0.6281 0.19208 0.16297 INSTANT 0.632691000E+00 TIME STEP NUMBER 657 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.89333E-05 0.23543E-02 Friction velocity uk : 0.89340E-05 0.23542E-02 Dimensionless distance yplus : 0.59491E-04 0.15663E-01 Friction thermal sca. tstar : -0.15249E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.41783E-04 0.11001E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.89333E-05 0.23543E-02 Friction velocity uk : 0.89340E-05 0.23542E-02 Dimensionless distance yplus : 0.59491E-04 0.15663E-01 Friction thermal sca. tstar : -0.15249E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.41783E-04 0.11001E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.35132E-08 3 0.16196E-06 0.27264E-12 0.10593E+01 c Velocity[X] 0.10238E-31 c Velocity[Y] 0.13632E-12 c Velocity[Z] 0.13632E-12 c Pressure 0.10553E-13 17 0.82215E-07 0.82215E-07 0.12171E+01 c k 0.38601E-06 2 0.43687E-07 0.31218E-08 0.15868E+01 c omega 0.13153E+02 1 0.15745E-08 0.35403E+00 0.30976E-02 c TempK 0.94635E+02 1 0.11120E-06 0.25482E-01 0.17684E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.0137e-13 8.4495e-14 -1.046e-17 -2.7016e-18 v Velocity[Y] -0.00012815 0.000123 -8.7622e-10 -3.3978e-12 v Velocity[Z] -0.00012298 0.00012815 6.2945e-10 -1.3306e-12 v ǁVelocityǁ 5.6063e-10 0.00013727 1.0674e-05 7.1213e-06 v Pressure -0.00111 0.02067 0.0011508 1.2198e-19 v k 1.1518e-09 0.0012622 0.00085453 0.0010795 v omega 15.83 1.0313e+05 2667 500.53 v TempK 288 341.99 293.76 290.76 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.3512e-14 9.6088e-05 5.9338e-05 7.7104e-05 v CourantNb 2.4866e-09 0.00021053 1.3836e-05 8.0791e-06 v FourierNb 0.10688 0.6281 0.19202 0.16292 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.947 4.947 0.00051513 -5.1497e-07 v volume_forces[Z] -4.947 4.947 -0.000515 6.1531e-07 v ǁvolume_forcesǁ 2.0447e-08 4.9482 0.52173 0.24853 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.97 290.91 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015663 5.5409e-05 3.1037e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.10693 0.6281 0.19203 0.16292 INSTANT 0.633654000E+00 TIME STEP NUMBER 658 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.88878E-05 0.23536E-02 Friction velocity uk : 0.88885E-05 0.23535E-02 Dimensionless distance yplus : 0.59187E-04 0.15658E-01 Friction thermal sca. tstar : -0.15088E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.41570E-04 0.10997E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.88878E-05 0.23536E-02 Friction velocity uk : 0.88885E-05 0.23535E-02 Dimensionless distance yplus : 0.59187E-04 0.15658E-01 Friction thermal sca. tstar : -0.15088E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.41570E-04 0.10997E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.35142E-08 3 0.16154E-06 0.27210E-12 0.10583E+01 c Velocity[X] 0.10190E-31 c Velocity[Y] 0.13605E-12 c Velocity[Z] 0.13605E-12 c Pressure 0.10528E-13 17 0.82020E-07 0.82020E-07 0.12152E+01 c k 0.38543E-06 2 0.43599E-07 0.31047E-08 0.15848E+01 c omega 0.13153E+02 1 0.15697E-08 0.35223E+00 0.30897E-02 c TempK 0.94636E+02 1 0.11096E-06 0.25424E-01 0.17664E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.0129e-13 8.4436e-14 -1.0453e-17 -2.6999e-18 v Velocity[Y] -0.0001281 0.00012294 -8.7446e-10 -3.3916e-12 v Velocity[Z] -0.00012292 0.0001281 6.2739e-10 -1.3321e-12 v ǁVelocityǁ 5.5565e-10 0.00013722 1.0677e-05 7.1273e-06 v Pressure -0.0011117 0.020686 0.0011519 -9.9033e-20 v k 1.1472e-09 0.0012604 0.00085315 0.0010779 v omega 15.811 1.0313e+05 2667 500.52 v TempK 288 341.99 293.76 290.77 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.3458e-14 9.6076e-05 5.9316e-05 7.7079e-05 v CourantNb 2.4899e-09 0.00021041 1.3835e-05 8.0822e-06 v FourierNb 0.10678 0.6281 0.19197 0.16287 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9471 4.9471 0.00051537 -5.1533e-07 v volume_forces[Z] -4.9471 4.9471 -0.00051524 6.157e-07 v ǁvolume_forcesǁ 2.0267e-08 4.9483 0.52197 0.24872 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.97 290.91 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015658 5.5393e-05 3.1027e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.10682 0.6281 0.19198 0.16288 INSTANT 0.634617000E+00 TIME STEP NUMBER 659 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.88418E-05 0.23529E-02 Friction velocity uk : 0.88425E-05 0.23528E-02 Dimensionless distance yplus : 0.58882E-04 0.15654E-01 Friction thermal sca. tstar : -0.14932E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.41355E-04 0.10994E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.88418E-05 0.23529E-02 Friction velocity uk : 0.88425E-05 0.23528E-02 Dimensionless distance yplus : 0.58882E-04 0.15654E-01 Friction thermal sca. tstar : -0.14932E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.41355E-04 0.10994E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.35153E-08 3 0.16111E-06 0.27156E-12 0.10572E+01 c Velocity[X] 0.10143E-31 c Velocity[Y] 0.13578E-12 c Velocity[Z] 0.13578E-12 c Pressure 0.10511E-13 17 0.81882E-07 0.81882E-07 0.12133E+01 c k 0.38486E-06 2 0.43511E-07 0.30878E-08 0.15829E+01 c omega 0.13153E+02 1 0.15649E-08 0.35043E+00 0.30818E-02 c TempK 0.94637E+02 1 0.11072E-06 0.25366E-01 0.17643E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.0122e-13 8.4378e-14 -1.0446e-17 -2.6982e-18 v Velocity[Y] -0.00012804 0.00012289 -8.7269e-10 -3.3855e-12 v Velocity[Z] -0.00012286 0.00012805 6.2532e-10 -1.3337e-12 v ǁVelocityǁ 5.5066e-10 0.00013718 1.068e-05 7.1333e-06 v Pressure -0.0011134 0.020701 0.001153 -2.8533e-20 v k 1.1426e-09 0.0012587 0.00085178 0.0010762 v omega 15.791 1.0313e+05 2667 500.5 v TempK 288 341.99 293.76 290.77 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.3404e-14 9.6063e-05 5.9294e-05 7.7054e-05 v CourantNb 2.4933e-09 0.00021029 1.3834e-05 8.0854e-06 v FourierNb 0.10668 0.6281 0.19192 0.16283 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9471 4.9472 0.00051561 -5.1568e-07 v volume_forces[Z] -4.9471 4.9472 -0.00051547 6.1609e-07 v ǁvolume_forcesǁ 2.0087e-08 4.9483 0.52221 0.24891 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.97 290.91 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015654 5.5376e-05 3.1017e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.10672 0.6281 0.19194 0.16283 INSTANT 0.635580000E+00 TIME STEP NUMBER 660 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.87955E-05 0.23522E-02 Friction velocity uk : 0.87962E-05 0.23521E-02 Dimensionless distance yplus : 0.58573E-04 0.15649E-01 Friction thermal sca. tstar : -0.14781E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.41138E-04 0.10991E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.87955E-05 0.23522E-02 Friction velocity uk : 0.87962E-05 0.23521E-02 Dimensionless distance yplus : 0.58573E-04 0.15649E-01 Friction thermal sca. tstar : -0.14781E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.41138E-04 0.10991E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.35163E-08 3 0.16069E-06 0.27103E-12 0.10562E+01 c Velocity[X] 0.10097E-31 c Velocity[Y] 0.13551E-12 c Velocity[Z] 0.13552E-12 c Pressure 0.10480E-13 17 0.81643E-07 0.81643E-07 0.12113E+01 c k 0.38428E-06 2 0.43423E-07 0.30710E-08 0.15809E+01 c omega 0.13153E+02 1 0.15601E-08 0.34865E+00 0.30740E-02 c TempK 0.94637E+02 1 0.11048E-06 0.25309E-01 0.17623E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.0115e-13 8.4319e-14 -1.0439e-17 -2.6965e-18 v Velocity[Y] -0.00012799 0.00012283 -8.7092e-10 -3.3799e-12 v Velocity[Z] -0.00012281 0.00012799 6.2325e-10 -1.335e-12 v ǁVelocityǁ 5.4567e-10 0.00013713 1.0683e-05 7.1393e-06 v Pressure -0.0011151 0.020717 0.0011541 7.3932e-20 v k 1.1381e-09 0.001257 0.00085041 0.0010745 v omega 15.771 1.0313e+05 2666.9 500.48 v TempK 288 341.99 293.76 290.77 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.3351e-14 9.6051e-05 5.9272e-05 7.7029e-05 v CourantNb 2.4966e-09 0.00021017 1.3833e-05 8.0886e-06 v FourierNb 0.10657 0.6281 0.19188 0.16278 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9472 4.9472 0.00051585 -5.1603e-07 v volume_forces[Z] -4.9472 4.9472 -0.00051571 6.1648e-07 v ǁvolume_forcesǁ 1.9906e-08 4.9484 0.52245 0.2491 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.98 290.91 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015649 5.5359e-05 3.1007e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.10661 0.6281 0.19189 0.16279 INSTANT 0.636543000E+00 TIME STEP NUMBER 661 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.87488E-05 0.23515E-02 Friction velocity uk : 0.87496E-05 0.23514E-02 Dimensionless distance yplus : 0.58262E-04 0.15644E-01 Friction thermal sca. tstar : -0.14634E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.40920E-04 0.10988E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.87488E-05 0.23515E-02 Friction velocity uk : 0.87496E-05 0.23514E-02 Dimensionless distance yplus : 0.58262E-04 0.15644E-01 Friction thermal sca. tstar : -0.14634E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.40920E-04 0.10988E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.35174E-08 3 0.16028E-06 0.27050E-12 0.10551E+01 c Velocity[X] 0.10050E-31 c Velocity[Y] 0.13525E-12 c Velocity[Z] 0.13525E-12 c Pressure 0.10489E-13 17 0.81707E-07 0.81707E-07 0.12094E+01 c k 0.38371E-06 2 0.43336E-07 0.30542E-08 0.15790E+01 c omega 0.13153E+02 1 0.15554E-08 0.34688E+00 0.30662E-02 c TempK 0.94638E+02 1 0.11025E-06 0.25252E-01 0.17603E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.0108e-13 8.4261e-14 -1.0432e-17 -2.6949e-18 v Velocity[Y] -0.00012793 0.00012277 -8.6914e-10 -3.3738e-12 v Velocity[Z] -0.00012275 0.00012794 6.2118e-10 -1.3366e-12 v ǁVelocityǁ 5.4067e-10 0.00013709 1.0686e-05 7.1453e-06 v Pressure -0.0011167 0.020732 0.0011551 1.3816e-19 v k 1.1336e-09 0.0012553 0.00084905 0.0010729 v omega 15.752 1.0313e+05 2666.9 500.46 v TempK 288 341.99 293.77 290.77 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.3298e-14 9.6039e-05 5.925e-05 7.7005e-05 v CourantNb 2.4999e-09 0.00021005 1.3832e-05 8.0917e-06 v FourierNb 0.10647 0.6281 0.19183 0.16274 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9473 4.9473 0.00051608 -5.1638e-07 v volume_forces[Z] -4.9473 4.9473 -0.00051595 6.1687e-07 v ǁvolume_forcesǁ 1.9726e-08 4.9485 0.52268 0.24929 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.98 290.91 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015644 5.5343e-05 3.0997e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.10651 0.6281 0.19185 0.16274 INSTANT 0.637506000E+00 TIME STEP NUMBER 662 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.87018E-05 0.23508E-02 Friction velocity uk : 0.87025E-05 0.23507E-02 Dimensionless distance yplus : 0.57949E-04 0.15640E-01 Friction thermal sca. tstar : -0.14491E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.40700E-04 0.10984E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.87018E-05 0.23508E-02 Friction velocity uk : 0.87025E-05 0.23507E-02 Dimensionless distance yplus : 0.57949E-04 0.15640E-01 Friction thermal sca. tstar : -0.14491E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.40700E-04 0.10984E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.35184E-08 3 0.15986E-06 0.26996E-12 0.10540E+01 c Velocity[X] 0.10004E-31 c Velocity[Y] 0.13498E-12 c Velocity[Z] 0.13498E-12 c Pressure 0.10444E-13 17 0.81356E-07 0.81356E-07 0.12075E+01 c k 0.38314E-06 2 0.43249E-07 0.30376E-08 0.15770E+01 c omega 0.13153E+02 1 0.15506E-08 0.34511E+00 0.30584E-02 c TempK 0.94638E+02 1 0.11001E-06 0.25195E-01 0.17583E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.0101e-13 8.4203e-14 -1.0425e-17 -2.6932e-18 v Velocity[Y] -0.00012788 0.00012271 -8.6735e-10 -3.3678e-12 v Velocity[Z] -0.00012269 0.00012788 6.191e-10 -1.3382e-12 v ǁVelocityǁ 5.3566e-10 0.00013704 1.069e-05 7.1514e-06 v Pressure -0.0011184 0.020748 0.0011562 -3.5103e-20 v k 1.1291e-09 0.0012535 0.00084769 0.0010712 v omega 15.732 1.0313e+05 2666.9 500.45 v TempK 288 342 293.77 290.77 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.3245e-14 9.6026e-05 5.9229e-05 7.698e-05 v CourantNb 2.5032e-09 0.00020993 1.3831e-05 8.0949e-06 v FourierNb 0.10636 0.6281 0.19179 0.16269 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9473 4.9474 0.00051632 -5.1673e-07 v volume_forces[Z] -4.9473 4.9474 -0.00051619 6.1726e-07 v ǁvolume_forcesǁ 1.9545e-08 4.9485 0.52292 0.24948 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.98 290.92 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.01564 5.5326e-05 3.0987e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.10641 0.6281 0.1918 0.1627 INSTANT 0.638469000E+00 TIME STEP NUMBER 663 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.86543E-05 0.23501E-02 Friction velocity uk : 0.86550E-05 0.23500E-02 Dimensionless distance yplus : 0.57633E-04 0.15635E-01 Friction thermal sca. tstar : -0.14352E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.40478E-04 0.10981E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.86543E-05 0.23501E-02 Friction velocity uk : 0.86550E-05 0.23500E-02 Dimensionless distance yplus : 0.57633E-04 0.15635E-01 Friction thermal sca. tstar : -0.14352E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.40478E-04 0.10981E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.35195E-08 3 0.15942E-06 0.26943E-12 0.10530E+01 c Velocity[X] 0.99575E-32 c Velocity[Y] 0.13471E-12 c Velocity[Z] 0.13472E-12 c Pressure 0.10410E-13 17 0.81090E-07 0.81090E-07 0.12056E+01 c k 0.38257E-06 2 0.43163E-07 0.30211E-08 0.15751E+01 c omega 0.13153E+02 1 0.15459E-08 0.34336E+00 0.30506E-02 c TempK 0.94639E+02 1 0.10978E-06 0.25138E-01 0.17563E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.0094e-13 8.4145e-14 -1.0418e-17 -2.6915e-18 v Velocity[Y] -0.00012783 0.00012265 -8.6556e-10 -3.3618e-12 v Velocity[Z] -0.00012263 0.00012783 6.1702e-10 -1.3397e-12 v ǁVelocityǁ 5.3065e-10 0.000137 1.0693e-05 7.1574e-06 v Pressure -0.0011201 0.020763 0.0011573 -6.1283e-21 v k 1.1246e-09 0.0012518 0.00084633 0.0010696 v omega 15.713 1.0313e+05 2666.9 500.43 v TempK 288 342 293.77 290.78 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.3193e-14 9.6014e-05 5.9207e-05 7.6955e-05 v CourantNb 2.5065e-09 0.00020981 1.3831e-05 8.0981e-06 v FourierNb 0.10626 0.6281 0.19174 0.16265 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9474 4.9474 0.00051656 -5.1708e-07 v volume_forces[Z] -4.9474 4.9474 -0.00051643 6.1765e-07 v ǁvolume_forcesǁ 1.9364e-08 4.9486 0.52316 0.24967 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.98 290.92 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015635 5.5309e-05 3.0977e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.1063 0.6281 0.19175 0.16265 INSTANT 0.639432000E+00 TIME STEP NUMBER 664 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.86064E-05 0.23494E-02 Friction velocity uk : 0.86072E-05 0.23493E-02 Dimensionless distance yplus : 0.57314E-04 0.15630E-01 Friction thermal sca. tstar : -0.14217E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.40254E-04 0.10978E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.86064E-05 0.23494E-02 Friction velocity uk : 0.86072E-05 0.23493E-02 Dimensionless distance yplus : 0.57314E-04 0.15630E-01 Friction thermal sca. tstar : -0.14217E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.40254E-04 0.10978E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.35205E-08 3 0.15900E-06 0.26890E-12 0.10519E+01 c Velocity[X] 0.99115E-32 c Velocity[Y] 0.13445E-12 c Velocity[Z] 0.13445E-12 c Pressure 0.10386E-13 17 0.80904E-07 0.80904E-07 0.12037E+01 c k 0.38201E-06 2 0.43076E-07 0.30047E-08 0.15732E+01 c omega 0.13153E+02 1 0.15412E-08 0.34162E+00 0.30429E-02 c TempK 0.94639E+02 1 0.10954E-06 0.25081E-01 0.17544E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.0086e-13 8.4087e-14 -1.0411e-17 -2.6899e-18 v Velocity[Y] -0.00012777 0.00012259 -8.6377e-10 -3.3558e-12 v Velocity[Z] -0.00012257 0.00012778 6.1494e-10 -1.3413e-12 v ǁVelocityǁ 5.2564e-10 0.00013696 1.0696e-05 7.1634e-06 v Pressure -0.0011218 0.020778 0.0011584 -5.692e-20 v k 1.1202e-09 0.0012501 0.00084498 0.0010679 v omega 15.693 1.0313e+05 2666.9 500.41 v TempK 288 342 293.77 290.78 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.314e-14 9.6002e-05 5.9185e-05 7.693e-05 v CourantNb 2.5098e-09 0.00020969 1.383e-05 8.1013e-06 v FourierNb 0.10616 0.6281 0.19169 0.1626 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9475 4.9475 0.0005168 -5.1743e-07 v volume_forces[Z] -4.9475 4.9475 -0.00051667 6.1804e-07 v ǁvolume_forcesǁ 1.9183e-08 4.9487 0.52339 0.24985 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.99 290.92 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.01563 5.5293e-05 3.0967e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.1062 0.6281 0.19171 0.16261 INSTANT 0.640395000E+00 TIME STEP NUMBER 665 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.85582E-05 0.23487E-02 Friction velocity uk : 0.85589E-05 0.23486E-02 Dimensionless distance yplus : 0.56993E-04 0.15626E-01 Friction thermal sca. tstar : -0.14086E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.40028E-04 0.10975E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.85582E-05 0.23487E-02 Friction velocity uk : 0.85589E-05 0.23486E-02 Dimensionless distance yplus : 0.56993E-04 0.15626E-01 Friction thermal sca. tstar : -0.14086E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.40028E-04 0.10975E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.35216E-08 3 0.15859E-06 0.26837E-12 0.10509E+01 c Velocity[X] 0.98659E-32 c Velocity[Y] 0.13418E-12 c Velocity[Z] 0.13419E-12 c Pressure 0.10369E-13 17 0.80768E-07 0.80768E-07 0.12018E+01 c k 0.38144E-06 2 0.42990E-07 0.29884E-08 0.15713E+01 c omega 0.13153E+02 1 0.15365E-08 0.33990E+00 0.30352E-02 c TempK 0.94640E+02 1 0.10931E-06 0.25025E-01 0.17524E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.0079e-13 8.4029e-14 -1.0404e-17 -2.6882e-18 v Velocity[Y] -0.00012772 0.00012254 -8.6197e-10 -3.3498e-12 v Velocity[Z] -0.00012251 0.00012772 6.1285e-10 -1.3428e-12 v ǁVelocityǁ 5.2062e-10 0.00013691 1.0699e-05 7.1695e-06 v Pressure -0.0011234 0.020794 0.0011594 -1.51e-20 v k 1.1158e-09 0.0012484 0.00084363 0.0010663 v omega 15.674 1.0313e+05 2666.9 500.39 v TempK 288 342 293.78 290.78 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.3088e-14 9.599e-05 5.9164e-05 7.6905e-05 v CourantNb 2.5131e-09 0.00020957 1.3829e-05 8.1045e-06 v FourierNb 0.10606 0.6281 0.19165 0.16256 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9475 4.9475 0.00051703 -5.1777e-07 v volume_forces[Z] -4.9475 4.9475 -0.0005169 6.1843e-07 v ǁvolume_forcesǁ 1.9002e-08 4.9487 0.52363 0.25004 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.99 290.92 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015626 5.5276e-05 3.0957e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.1061 0.6281 0.19166 0.16256 INSTANT 0.641358000E+00 TIME STEP NUMBER 666 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.85095E-05 0.23480E-02 Friction velocity uk : 0.85102E-05 0.23479E-02 Dimensionless distance yplus : 0.56669E-04 0.15621E-01 Friction thermal sca. tstar : -0.13958E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.39801E-04 0.10971E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.85095E-05 0.23480E-02 Friction velocity uk : 0.85102E-05 0.23479E-02 Dimensionless distance yplus : 0.56669E-04 0.15621E-01 Friction thermal sca. tstar : -0.13958E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.39801E-04 0.10971E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.35227E-08 3 0.15818E-06 0.26784E-12 0.10498E+01 c Velocity[X] 0.98206E-32 c Velocity[Y] 0.13392E-12 c Velocity[Z] 0.13392E-12 c Pressure 0.10341E-13 17 0.80548E-07 0.80548E-07 0.11999E+01 c k 0.38088E-06 2 0.42905E-07 0.29723E-08 0.15693E+01 c omega 0.13153E+02 1 0.15319E-08 0.33818E+00 0.30275E-02 c TempK 0.94641E+02 1 0.10908E-06 0.24969E-01 0.17504E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.0072e-13 8.3972e-14 -1.0397e-17 -2.6865e-18 v Velocity[Y] -0.00012767 0.00012248 -8.6016e-10 -3.3439e-12 v Velocity[Z] -0.00012246 0.00012767 6.1075e-10 -1.3443e-12 v ǁVelocityǁ 5.156e-10 0.00013687 1.0702e-05 7.1755e-06 v Pressure -0.0011251 0.020809 0.0011605 -3.9613e-20 v k 1.1114e-09 0.0012467 0.00084228 0.0010647 v omega 15.654 1.0313e+05 2666.9 500.38 v TempK 288 342 293.78 290.78 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.3037e-14 9.5977e-05 5.9142e-05 7.688e-05 v CourantNb 2.5163e-09 0.00020946 1.3828e-05 8.1077e-06 v FourierNb 0.10596 0.6281 0.1916 0.16251 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9476 4.9476 0.00051727 -5.1812e-07 v volume_forces[Z] -4.9476 4.9476 -0.00051714 6.1882e-07 v ǁvolume_forcesǁ 1.8821e-08 4.9488 0.52386 0.25023 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.99 290.93 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015621 5.526e-05 3.0947e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.106 0.6281 0.19162 0.16252 INSTANT 0.642321000E+00 TIME STEP NUMBER 667 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.84604E-05 0.23473E-02 Friction velocity uk : 0.84612E-05 0.23473E-02 Dimensionless distance yplus : 0.56342E-04 0.15617E-01 Friction thermal sca. tstar : -0.13833E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.39571E-04 0.10968E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.84604E-05 0.23473E-02 Friction velocity uk : 0.84612E-05 0.23473E-02 Dimensionless distance yplus : 0.56342E-04 0.15617E-01 Friction thermal sca. tstar : -0.13833E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.39571E-04 0.10968E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.35238E-08 3 0.15777E-06 0.26732E-12 0.10488E+01 c Velocity[X] 0.97755E-32 c Velocity[Y] 0.13366E-12 c Velocity[Z] 0.13366E-12 c Pressure 0.10318E-13 17 0.80369E-07 0.80369E-07 0.11980E+01 c k 0.38031E-06 2 0.42819E-07 0.29562E-08 0.15674E+01 c omega 0.13153E+02 1 0.15273E-08 0.33647E+00 0.30198E-02 c TempK 0.94641E+02 1 0.10885E-06 0.24913E-01 0.17484E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.0065e-13 8.3914e-14 -1.0391e-17 -2.6849e-18 v Velocity[Y] -0.00012761 0.00012242 -8.5835e-10 -3.3379e-12 v Velocity[Z] -0.0001224 0.00012762 6.0866e-10 -1.3459e-12 v ǁVelocityǁ 5.1058e-10 0.00013682 1.0705e-05 7.1815e-06 v Pressure -0.0011268 0.020825 0.0011616 3.7897e-20 v k 1.107e-09 0.001245 0.00084094 0.001063 v omega 15.635 1.0313e+05 2666.8 500.36 v TempK 288 342 293.78 290.79 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.2985e-14 9.5965e-05 5.912e-05 7.6856e-05 v CourantNb 2.5196e-09 0.00020934 1.3827e-05 8.111e-06 v FourierNb 0.10586 0.6281 0.19156 0.16247 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9476 4.9477 0.00051751 -5.1847e-07 v volume_forces[Z] -4.9476 4.9477 -0.00051738 6.192e-07 v ǁvolume_forcesǁ 1.8639e-08 4.9488 0.5241 0.25042 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 293.99 290.93 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015617 5.5243e-05 3.0937e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.1059 0.6281 0.19157 0.16248 INSTANT 0.643284000E+00 TIME STEP NUMBER 668 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.84109E-05 0.23466E-02 Friction velocity uk : 0.84117E-05 0.23466E-02 Dimensionless distance yplus : 0.56012E-04 0.15612E-01 Friction thermal sca. tstar : -0.13712E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.39340E-04 0.10965E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.84109E-05 0.23466E-02 Friction velocity uk : 0.84117E-05 0.23466E-02 Dimensionless distance yplus : 0.56012E-04 0.15612E-01 Friction thermal sca. tstar : -0.13712E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.39340E-04 0.10965E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.35248E-08 3 0.15735E-06 0.26679E-12 0.10477E+01 c Velocity[X] 0.97307E-32 c Velocity[Y] 0.13339E-12 c Velocity[Z] 0.13340E-12 c Pressure 0.10297E-13 17 0.80206E-07 0.80206E-07 0.11962E+01 c k 0.37975E-06 2 0.42734E-07 0.29402E-08 0.15655E+01 c omega 0.13153E+02 1 0.15226E-08 0.33478E+00 0.30122E-02 c TempK 0.94642E+02 1 0.10862E-06 0.24857E-01 0.17464E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.0058e-13 8.3857e-14 -1.0384e-17 -2.6832e-18 v Velocity[Y] -0.00012756 0.00012236 -8.5654e-10 -3.332e-12 v Velocity[Z] -0.00012234 0.00012757 6.0655e-10 -1.3474e-12 v ǁVelocityǁ 5.0555e-10 0.00013678 1.0708e-05 7.1876e-06 v Pressure -0.0011285 0.02084 0.0011626 2.5298e-20 v k 1.1026e-09 0.0012433 0.0008396 0.0010614 v omega 15.616 1.0313e+05 2666.8 500.34 v TempK 288 342 293.78 290.79 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.2934e-14 9.5953e-05 5.9099e-05 7.6831e-05 v CourantNb 2.5229e-09 0.00020922 1.3826e-05 8.1142e-06 v FourierNb 0.10575 0.6281 0.19151 0.16242 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9477 4.9477 0.00051774 -5.1881e-07 v volume_forces[Z] -4.9477 4.9477 -0.00051761 6.1959e-07 v ǁvolume_forcesǁ 1.8457e-08 4.9489 0.52433 0.25061 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294 290.93 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015612 5.5227e-05 3.0927e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.1058 0.6281 0.19153 0.16243 INSTANT 0.644247000E+00 TIME STEP NUMBER 669 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.83610E-05 0.23459E-02 Friction velocity uk : 0.83617E-05 0.23459E-02 Dimensionless distance yplus : 0.55680E-04 0.15607E-01 Friction thermal sca. tstar : -0.13609E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.39106E-04 0.10962E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.83610E-05 0.23459E-02 Friction velocity uk : 0.83617E-05 0.23459E-02 Dimensionless distance yplus : 0.55680E-04 0.15607E-01 Friction thermal sca. tstar : -0.13609E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.39106E-04 0.10962E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.35259E-08 3 0.15694E-06 0.26627E-12 0.10466E+01 c Velocity[X] 0.96861E-32 c Velocity[Y] 0.13313E-12 c Velocity[Z] 0.13313E-12 c Pressure 0.10280E-13 17 0.80065E-07 0.80065E-07 0.11943E+01 c k 0.37919E-06 2 0.42649E-07 0.29244E-08 0.15636E+01 c omega 0.13153E+02 1 0.15180E-08 0.33309E+00 0.30046E-02 c TempK 0.94642E+02 1 0.10839E-06 0.24802E-01 0.17445E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.0051e-13 8.3799e-14 -1.0377e-17 -2.6816e-18 v Velocity[Y] -0.00012751 0.00012231 -8.5471e-10 -3.3261e-12 v Velocity[Z] -0.00012229 0.00012751 6.0445e-10 -1.3489e-12 v ǁVelocityǁ 5.0053e-10 0.00013674 1.0712e-05 7.1936e-06 v Pressure -0.0011302 0.020855 0.0011637 1.5198e-20 v k 1.0983e-09 0.0012416 0.00083827 0.0010598 v omega 15.597 1.0313e+05 2666.8 500.33 v TempK 288 342 293.79 290.79 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.2884e-14 9.5941e-05 5.9077e-05 7.6806e-05 v CourantNb 2.5262e-09 0.0002091 1.3825e-05 8.1174e-06 v FourierNb 0.10565 0.6281 0.19147 0.16238 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9478 4.9478 0.00051798 -5.1916e-07 v volume_forces[Z] -4.9478 4.9478 -0.00051785 6.1997e-07 v ǁvolume_forcesǁ 1.8276e-08 4.949 0.52457 0.25079 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294 290.93 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015607 5.5211e-05 3.0917e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.1057 0.6281 0.19148 0.16239 INSTANT 0.645210000E+00 TIME STEP NUMBER 670 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.83106E-05 0.23452E-02 Friction velocity uk : 0.83113E-05 0.23452E-02 Dimensionless distance yplus : 0.55344E-04 0.15603E-01 Friction thermal sca. tstar : -0.13787E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.38870E-04 0.10958E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.83106E-05 0.23452E-02 Friction velocity uk : 0.83113E-05 0.23452E-02 Dimensionless distance yplus : 0.55344E-04 0.15603E-01 Friction thermal sca. tstar : -0.13787E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.38870E-04 0.10958E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.35270E-08 3 0.15656E-06 0.26574E-12 0.10456E+01 c Velocity[X] 0.96417E-32 c Velocity[Y] 0.13287E-12 c Velocity[Z] 0.13287E-12 c Pressure 0.10264E-13 15 0.79942E-07 0.79942E-07 0.11924E+01 c k 0.37863E-06 2 0.42565E-07 0.29086E-08 0.15617E+01 c omega 0.13153E+02 1 0.15135E-08 0.33142E+00 0.29971E-02 c TempK 0.94643E+02 1 0.10816E-06 0.24747E-01 0.17425E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.0044e-13 8.3742e-14 -1.037e-17 -2.68e-18 v Velocity[Y] -0.00012746 0.00012225 -8.5349e-10 -3.9565e-12 v Velocity[Z] -0.00012223 0.00012746 6.0142e-10 -2.1506e-12 v ǁVelocityǁ 4.9634e-10 0.00013669 1.0715e-05 7.1997e-06 v Pressure -0.0011318 0.020871 0.0011648 8.7953e-20 v k 1.094e-09 0.00124 0.00083694 0.0010582 v omega 15.578 1.0313e+05 2666.8 500.31 v TempK 288 342 293.79 290.79 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.2833e-14 9.5929e-05 5.9056e-05 7.6782e-05 v CourantNb 2.5284e-09 0.00020899 1.3825e-05 8.1206e-06 v FourierNb 0.10555 0.6281 0.19142 0.16233 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9478 4.9479 0.00051822 -5.195e-07 v volume_forces[Z] -4.9478 4.9479 -0.00051808 6.2036e-07 v ǁvolume_forcesǁ 1.8094e-08 4.949 0.5248 0.25098 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294 290.93 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015603 5.5194e-05 3.0907e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.1056 0.6281 0.19144 0.16234 INSTANT 0.646173000E+00 TIME STEP NUMBER 671 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.82687E-05 0.23445E-02 Friction velocity uk : 0.82694E-05 0.23445E-02 Dimensionless distance yplus : 0.55065E-04 0.15598E-01 Friction thermal sca. tstar : -0.13971E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.38674E-04 0.10955E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.82687E-05 0.23445E-02 Friction velocity uk : 0.82694E-05 0.23445E-02 Dimensionless distance yplus : 0.55065E-04 0.15598E-01 Friction thermal sca. tstar : -0.13971E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.38674E-04 0.10955E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.35281E-08 3 0.15617E-06 0.26522E-12 0.10445E+01 c Velocity[X] 0.96000E-32 c Velocity[Y] 0.13261E-12 c Velocity[Z] 0.13261E-12 c Pressure 0.10281E-13 15 0.80072E-07 0.80072E-07 0.11906E+01 c k 0.37808E-06 2 0.42481E-07 0.28930E-08 0.15598E+01 c omega 0.13153E+02 1 0.15089E-08 0.32975E+00 0.29895E-02 c TempK 0.94644E+02 1 0.10793E-06 0.24692E-01 0.17406E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.0037e-13 8.3685e-14 -1.0363e-17 -2.6783e-18 v Velocity[Y] -0.0001274 0.00012219 -8.5168e-10 -3.9831e-12 v Velocity[Z] -0.00012217 0.00012741 5.9933e-10 -2.1316e-12 v ǁVelocityǁ 4.91e-10 0.00013665 1.0718e-05 7.2057e-06 v Pressure -0.0011335 0.020886 0.0011658 6.344e-20 v k 1.0897e-09 0.0012383 0.00083561 0.0010566 v omega 15.558 1.0313e+05 2666.8 500.29 v TempK 288 342 293.79 290.79 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.2783e-14 9.5917e-05 5.9034e-05 7.6757e-05 v CourantNb 2.5313e-09 0.00020887 1.3824e-05 8.1239e-06 v FourierNb 0.10545 0.6281 0.19138 0.16229 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9479 4.9479 0.00051845 -5.1988e-07 v volume_forces[Z] -4.9479 4.9479 -0.00051832 6.2076e-07 v ǁvolume_forcesǁ 1.7943e-08 4.9491 0.52504 0.25117 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294 290.94 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015598 5.5178e-05 3.0897e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.1055 0.6281 0.19139 0.1623 INSTANT 0.647136000E+00 TIME STEP NUMBER 672 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.82147E-05 0.23439E-02 Friction velocity uk : 0.82154E-05 0.23438E-02 Dimensionless distance yplus : 0.54706E-04 0.15594E-01 Friction thermal sca. tstar : -0.14163E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.38422E-04 0.10952E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.82147E-05 0.23439E-02 Friction velocity uk : 0.82154E-05 0.23438E-02 Dimensionless distance yplus : 0.54706E-04 0.15594E-01 Friction thermal sca. tstar : -0.14163E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.38422E-04 0.10952E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.35292E-08 3 0.15572E-06 0.26470E-12 0.10435E+01 c Velocity[X] 0.95557E-32 c Velocity[Y] 0.13235E-12 c Velocity[Z] 0.13235E-12 c Pressure 0.10217E-13 15 0.79573E-07 0.79573E-07 0.11887E+01 c k 0.37752E-06 2 0.42397E-07 0.28774E-08 0.15579E+01 c omega 0.13153E+02 1 0.15044E-08 0.32810E+00 0.29820E-02 c TempK 0.94644E+02 1 0.10770E-06 0.24637E-01 0.17386E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.003e-13 8.3628e-14 -1.0356e-17 -2.6767e-18 v Velocity[Y] -0.00012735 0.00012214 -8.4983e-10 -3.9591e-12 v Velocity[Z] -0.00012211 0.00012736 5.9721e-10 -2.1403e-12 v ǁVelocityǁ 4.8586e-10 0.00013661 1.0721e-05 7.2118e-06 v Pressure -0.0011352 0.020901 0.0011669 -3.8927e-20 v k 1.0855e-09 0.0012366 0.00083429 0.001055 v omega 15.539 1.0313e+05 2666.8 500.27 v TempK 288 342 293.8 290.8 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.2733e-14 9.5904e-05 5.9013e-05 7.6732e-05 v CourantNb 2.5347e-09 0.00020875 1.3823e-05 8.1271e-06 v FourierNb 0.10535 0.6281 0.19133 0.16225 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.948 4.948 0.00051869 -5.2022e-07 v volume_forces[Z] -4.948 4.948 -0.00051855 6.2115e-07 v ǁvolume_forcesǁ 1.775e-08 4.9492 0.52527 0.25135 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.01 290.94 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015594 5.5161e-05 3.0887e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.1054 0.6281 0.19135 0.16225 INSTANT 0.648099000E+00 TIME STEP NUMBER 673 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.81619E-05 0.23432E-02 Friction velocity uk : 0.81627E-05 0.23431E-02 Dimensionless distance yplus : 0.54354E-04 0.15589E-01 Friction thermal sca. tstar : -0.14362E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.38175E-04 0.10949E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.81619E-05 0.23432E-02 Friction velocity uk : 0.81627E-05 0.23431E-02 Dimensionless distance yplus : 0.54354E-04 0.15589E-01 Friction thermal sca. tstar : -0.14362E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.38175E-04 0.10949E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.35303E-08 3 0.15531E-06 0.26418E-12 0.10424E+01 c Velocity[X] 0.95113E-32 c Velocity[Y] 0.13209E-12 c Velocity[Z] 0.13209E-12 c Pressure 0.10210E-13 15 0.79518E-07 0.79518E-07 0.11869E+01 c k 0.37697E-06 2 0.42313E-07 0.28620E-08 0.15560E+01 c omega 0.13153E+02 1 0.14998E-08 0.32645E+00 0.29745E-02 c TempK 0.94645E+02 1 0.10748E-06 0.24582E-01 0.17367E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.0023e-13 8.3572e-14 -1.035e-17 -2.6751e-18 v Velocity[Y] -0.0001273 0.00012208 -8.4799e-10 -3.953e-12 v Velocity[Z] -0.00012206 0.0001273 5.9509e-10 -2.1422e-12 v ǁVelocityǁ 4.8075e-10 0.00013656 1.0724e-05 7.2178e-06 v Pressure -0.0011369 0.020917 0.001168 -2.1719e-20 v k 1.0812e-09 0.0012349 0.00083297 0.0010533 v omega 15.52 1.0313e+05 2666.8 500.26 v TempK 288 342 293.8 290.8 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.2683e-14 9.5892e-05 5.8992e-05 7.6708e-05 v CourantNb 2.538e-09 0.00020864 1.3822e-05 8.1304e-06 v FourierNb 0.10526 0.6281 0.19129 0.1622 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.948 4.948 0.00051892 -5.2056e-07 v volume_forces[Z] -4.948 4.948 -0.00051879 6.2153e-07 v ǁvolume_forcesǁ 1.7564e-08 4.9492 0.52551 0.25154 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.01 290.94 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015589 5.5145e-05 3.0877e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.1053 0.6281 0.1913 0.16221 INSTANT 0.649062000E+00 TIME STEP NUMBER 674 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.81090E-05 0.23425E-02 Friction velocity uk : 0.81097E-05 0.23425E-02 Dimensionless distance yplus : 0.54002E-04 0.15585E-01 Friction thermal sca. tstar : -0.14570E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.37927E-04 0.10946E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.81090E-05 0.23425E-02 Friction velocity uk : 0.81097E-05 0.23425E-02 Dimensionless distance yplus : 0.54002E-04 0.15585E-01 Friction thermal sca. tstar : -0.14570E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.37927E-04 0.10946E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.35314E-08 3 0.15523E-06 0.26366E-12 0.10414E+01 c Velocity[X] 0.94674E-32 c Velocity[Y] 0.13183E-12 c Velocity[Z] 0.13183E-12 c Pressure 0.10184E-13 15 0.79314E-07 0.79314E-07 0.11850E+01 c k 0.37641E-06 2 0.42230E-07 0.28467E-08 0.15541E+01 c omega 0.13153E+02 1 0.14953E-08 0.32482E+00 0.29671E-02 c TempK 0.94645E+02 1 0.10725E-06 0.24528E-01 0.17347E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.0016e-13 8.3515e-14 -1.0343e-17 -2.6734e-18 v Velocity[Y] -0.00012725 0.00012203 -8.4614e-10 -3.946e-12 v Velocity[Z] -0.000122 0.00012725 5.9297e-10 -2.1423e-12 v ǁVelocityǁ 4.7566e-10 0.00013652 1.0728e-05 7.2239e-06 v Pressure -0.0011385 0.020932 0.001169 -8.1874e-20 v k 1.077e-09 0.0012333 0.00083166 0.0010517 v omega 15.501 1.0313e+05 2666.7 500.24 v TempK 288 342 293.8 290.8 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.2633e-14 9.588e-05 5.897e-05 7.6683e-05 v CourantNb 2.5413e-09 0.00020852 1.3822e-05 8.1336e-06 v FourierNb 0.10516 0.6281 0.19124 0.16216 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9481 4.9481 0.00051916 -5.209e-07 v volume_forces[Z] -4.9481 4.9481 -0.00051902 6.2191e-07 v ǁvolume_forcesǁ 1.7379e-08 4.9493 0.52574 0.25173 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.01 290.94 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015585 5.5129e-05 3.0868e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.1052 0.6281 0.19126 0.16217 INSTANT 0.650025000E+00 TIME STEP NUMBER 675 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.80558E-05 0.23418E-02 Friction velocity uk : 0.80566E-05 0.23418E-02 Dimensionless distance yplus : 0.53648E-04 0.15580E-01 Friction thermal sca. tstar : -0.14788E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.37679E-04 0.10943E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.80558E-05 0.23418E-02 Friction velocity uk : 0.80566E-05 0.23418E-02 Dimensionless distance yplus : 0.53648E-04 0.15580E-01 Friction thermal sca. tstar : -0.14788E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.37679E-04 0.10943E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.35325E-08 3 0.15450E-06 0.26314E-12 0.10403E+01 c Velocity[X] 0.94241E-32 c Velocity[Y] 0.13157E-12 c Velocity[Z] 0.13157E-12 c Pressure 0.10149E-13 15 0.79037E-07 0.79037E-07 0.11832E+01 c k 0.37586E-06 2 0.42147E-07 0.28314E-08 0.15523E+01 c omega 0.13153E+02 1 0.14909E-08 0.32319E+00 0.29596E-02 c TempK 0.94646E+02 1 0.10703E-06 0.24473E-01 0.17328E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.0009e-13 8.3459e-14 -1.0336e-17 -2.6718e-18 v Velocity[Y] -0.0001272 0.00012197 -8.4429e-10 -3.9393e-12 v Velocity[Z] -0.00012195 0.0001272 5.9084e-10 -2.1428e-12 v ǁVelocityǁ 4.706e-10 0.00013648 1.0731e-05 7.23e-06 v Pressure -0.0011402 0.020947 0.0011701 -5.7851e-20 v k 1.0728e-09 0.0012316 0.00083034 0.0010502 v omega 15.482 1.0313e+05 2666.7 500.22 v TempK 288 342 293.8 290.8 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.2584e-14 9.5868e-05 5.8949e-05 7.6659e-05 v CourantNb 2.5445e-09 0.00020841 1.3821e-05 8.1369e-06 v FourierNb 0.10506 0.6281 0.1912 0.16211 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9482 4.9482 0.00051939 -5.2125e-07 v volume_forces[Z] -4.9482 4.9482 -0.00051926 6.2229e-07 v ǁvolume_forcesǁ 1.7195e-08 4.9493 0.52597 0.25191 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.01 290.94 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.01558 5.5113e-05 3.0858e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.1051 0.6281 0.19121 0.16212 INSTANT 0.650988000E+00 TIME STEP NUMBER 676 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.80023E-05 0.23411E-02 Friction velocity uk : 0.80031E-05 0.23411E-02 Dimensionless distance yplus : 0.53292E-04 0.15576E-01 Friction thermal sca. tstar : -0.15015E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.37429E-04 0.10939E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.80023E-05 0.23411E-02 Friction velocity uk : 0.80031E-05 0.23411E-02 Dimensionless distance yplus : 0.53292E-04 0.15576E-01 Friction thermal sca. tstar : -0.15015E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.37429E-04 0.10939E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.35336E-08 3 0.15457E-06 0.26262E-12 0.10393E+01 c Velocity[X] 0.93810E-32 c Velocity[Y] 0.13131E-12 c Velocity[Z] 0.13131E-12 c Pressure 0.10148E-13 15 0.79032E-07 0.79032E-07 0.11814E+01 c k 0.37531E-06 2 0.42064E-07 0.28163E-08 0.15504E+01 c omega 0.13153E+02 1 0.14864E-08 0.32158E+00 0.29523E-02 c TempK 0.94646E+02 1 0.10680E-06 0.24419E-01 0.17309E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.0002e-13 8.3402e-14 -1.0329e-17 -2.6702e-18 v Velocity[Y] -0.00012716 0.00012191 -8.4243e-10 -3.9326e-12 v Velocity[Z] -0.00012189 0.00012716 5.887e-10 -2.1433e-12 v ǁVelocityǁ 4.6554e-10 0.00013644 1.0734e-05 7.236e-06 v Pressure -0.0011419 0.020963 0.0011712 5.8685e-20 v k 1.0686e-09 0.00123 0.00082904 0.0010486 v omega 15.464 1.0313e+05 2666.7 500.21 v TempK 288 342.01 293.81 290.8 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.2535e-14 9.5856e-05 5.8928e-05 7.6635e-05 v CourantNb 2.5478e-09 0.00020829 1.382e-05 8.1402e-06 v FourierNb 0.10496 0.6281 0.19115 0.16207 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9482 4.9482 0.00051962 -5.2159e-07 v volume_forces[Z] -4.9482 4.9482 -0.00051949 6.2267e-07 v ǁvolume_forcesǁ 1.7012e-08 4.9494 0.52621 0.2521 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.02 290.95 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015576 5.5096e-05 3.0848e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.105 0.6281 0.19117 0.16208 INSTANT 0.651951000E+00 TIME STEP NUMBER 677 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.79484E-05 0.23405E-02 Friction velocity uk : 0.79492E-05 0.23404E-02 Dimensionless distance yplus : 0.52933E-04 0.15571E-01 Friction thermal sca. tstar : -0.15253E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.37177E-04 0.10936E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.79484E-05 0.23405E-02 Friction velocity uk : 0.79492E-05 0.23404E-02 Dimensionless distance yplus : 0.52933E-04 0.15571E-01 Friction thermal sca. tstar : -0.15253E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.37177E-04 0.10936E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.35347E-08 3 0.15372E-06 0.26211E-12 0.10382E+01 c Velocity[X] 0.93381E-32 c Velocity[Y] 0.13105E-12 c Velocity[Z] 0.13105E-12 c Pressure 0.10132E-13 15 0.78902E-07 0.78902E-07 0.11795E+01 c k 0.37477E-06 2 0.41982E-07 0.28012E-08 0.15485E+01 c omega 0.13153E+02 1 0.14819E-08 0.31998E+00 0.29449E-02 c TempK 0.94647E+02 1 0.10658E-06 0.24365E-01 0.17290E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.9954e-14 8.3346e-14 -1.0322e-17 -2.6686e-18 v Velocity[Y] -0.00012712 0.00012186 -8.4057e-10 -3.926e-12 v Velocity[Z] -0.00012183 0.00012713 5.8657e-10 -2.1437e-12 v ǁVelocityǁ 4.605e-10 0.00013639 1.0737e-05 7.2421e-06 v Pressure -0.0011436 0.020978 0.0011722 1.3767e-19 v k 1.0645e-09 0.0012283 0.00082773 0.001047 v omega 15.445 1.0313e+05 2666.7 500.19 v TempK 288 342.01 293.81 290.81 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.2486e-14 9.5844e-05 5.8906e-05 7.661e-05 v CourantNb 2.551e-09 0.00020818 1.3819e-05 8.1434e-06 v FourierNb 0.10486 0.6281 0.19111 0.16203 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9483 4.9483 0.00051986 -5.2193e-07 v volume_forces[Z] -4.9483 4.9483 -0.00051973 6.2305e-07 v ǁvolume_forcesǁ 1.6829e-08 4.9495 0.52644 0.25229 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.02 290.95 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015571 5.508e-05 3.0838e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.1049 0.6281 0.19112 0.16203 INSTANT 0.652914000E+00 TIME STEP NUMBER 678 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.78941E-05 0.23398E-02 Friction velocity uk : 0.78948E-05 0.23397E-02 Dimensionless distance yplus : 0.52571E-04 0.15567E-01 Friction thermal sca. tstar : -0.15502E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.36922E-04 0.10933E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.78941E-05 0.23398E-02 Friction velocity uk : 0.78948E-05 0.23397E-02 Dimensionless distance yplus : 0.52571E-04 0.15567E-01 Friction thermal sca. tstar : -0.15502E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.36922E-04 0.10933E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.35359E-08 3 0.15332E-06 0.26159E-12 0.10371E+01 c Velocity[X] 0.92956E-32 c Velocity[Y] 0.13080E-12 c Velocity[Z] 0.13080E-12 c Pressure 0.10114E-13 15 0.78767E-07 0.78767E-07 0.11777E+01 c k 0.37422E-06 2 0.41899E-07 0.27863E-08 0.15467E+01 c omega 0.13153E+02 1 0.14775E-08 0.31838E+00 0.29375E-02 c TempK 0.94648E+02 1 0.10636E-06 0.24312E-01 0.17270E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.9885e-14 8.329e-14 -1.0316e-17 -2.667e-18 v Velocity[Y] -0.00012708 0.0001218 -8.387e-10 -3.9193e-12 v Velocity[Z] -0.00012178 0.00012709 5.8442e-10 -2.1442e-12 v ǁVelocityǁ 4.5545e-10 0.00013635 1.0741e-05 7.2482e-06 v Pressure -0.0011452 0.020993 0.0011733 -6.3636e-20 v k 1.0604e-09 0.0012267 0.00082643 0.0010454 v omega 15.426 1.0313e+05 2666.7 500.17 v TempK 288 342.01 293.81 290.81 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.2438e-14 9.5832e-05 5.8885e-05 7.6586e-05 v CourantNb 2.5542e-09 0.00020806 1.3819e-05 8.1467e-06 v FourierNb 0.10476 0.6281 0.19106 0.16198 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9483 4.9484 0.00052009 -5.2227e-07 v volume_forces[Z] -4.9483 4.9484 -0.00051996 6.2343e-07 v ǁvolume_forcesǁ 1.6647e-08 4.9495 0.52667 0.25247 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.02 290.95 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015567 5.5064e-05 3.0828e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.10481 0.6281 0.19108 0.16199 INSTANT 0.653877000E+00 TIME STEP NUMBER 679 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.78392E-05 0.23391E-02 Friction velocity uk : 0.78400E-05 0.23391E-02 Dimensionless distance yplus : 0.52206E-04 0.15562E-01 Friction thermal sca. tstar : -0.15763E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.36666E-04 0.10930E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.78392E-05 0.23391E-02 Friction velocity uk : 0.78400E-05 0.23391E-02 Dimensionless distance yplus : 0.52206E-04 0.15562E-01 Friction thermal sca. tstar : -0.15763E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.36666E-04 0.10930E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.35370E-08 3 0.15292E-06 0.26108E-12 0.10361E+01 c Velocity[X] 0.92535E-32 c Velocity[Y] 0.13054E-12 c Velocity[Z] 0.13054E-12 c Pressure 0.10086E-13 15 0.78544E-07 0.78544E-07 0.11759E+01 c k 0.37367E-06 2 0.41817E-07 0.27715E-08 0.15448E+01 c omega 0.13153E+02 1 0.14731E-08 0.31680E+00 0.29302E-02 c TempK 0.94648E+02 1 0.10614E-06 0.24258E-01 0.17251E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.9816e-14 8.3234e-14 -1.0309e-17 -2.6654e-18 v Velocity[Y] -0.00012704 0.00012175 -8.3683e-10 -3.9127e-12 v Velocity[Z] -0.00012172 0.00012705 5.8228e-10 -2.1447e-12 v ǁVelocityǁ 4.5042e-10 0.00013631 1.0744e-05 7.2543e-06 v Pressure -0.0011469 0.021008 0.0011744 1.5169e-19 v k 1.0563e-09 0.001225 0.00082513 0.0010438 v omega 15.407 1.0313e+05 2666.7 500.16 v TempK 288 342.01 293.81 290.81 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.239e-14 9.582e-05 5.8864e-05 7.6561e-05 v CourantNb 2.5575e-09 0.00020795 1.3818e-05 8.15e-06 v FourierNb 0.10467 0.6281 0.19102 0.16194 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9484 4.9484 0.00052032 -5.2261e-07 v volume_forces[Z] -4.9484 4.9484 -0.00052019 6.238e-07 v ǁvolume_forcesǁ 1.6465e-08 4.9496 0.5269 0.25266 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.03 290.95 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015562 5.5048e-05 3.0819e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.10471 0.6281 0.19103 0.16195 INSTANT 0.654840000E+00 TIME STEP NUMBER 680 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.77839E-05 0.23384E-02 Friction velocity uk : 0.77847E-05 0.23384E-02 Dimensionless distance yplus : 0.51837E-04 0.15558E-01 Friction thermal sca. tstar : -0.16038E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.36407E-04 0.10927E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.77839E-05 0.23384E-02 Friction velocity uk : 0.77847E-05 0.23384E-02 Dimensionless distance yplus : 0.51837E-04 0.15558E-01 Friction thermal sca. tstar : -0.16038E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.36407E-04 0.10927E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.35381E-08 3 0.15255E-06 0.26057E-12 0.10350E+01 c Velocity[X] 0.92116E-32 c Velocity[Y] 0.13028E-12 c Velocity[Z] 0.13028E-12 c Pressure 0.10110E-13 15 0.78730E-07 0.78730E-07 0.11741E+01 c k 0.37313E-06 2 0.41736E-07 0.27567E-08 0.15429E+01 c omega 0.13153E+02 1 0.14687E-08 0.31523E+00 0.29229E-02 c TempK 0.94649E+02 1 0.10591E-06 0.24205E-01 0.17232E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.9747e-14 8.3178e-14 -1.0302e-17 -2.6638e-18 v Velocity[Y] -0.00012701 0.00012169 -8.3495e-10 -3.9061e-12 v Velocity[Z] -0.00012167 0.00012701 5.8013e-10 -2.1452e-12 v ǁVelocityǁ 4.4539e-10 0.00013627 1.0747e-05 7.2603e-06 v Pressure -0.0011486 0.021023 0.0011754 -4.4271e-20 v k 1.0522e-09 0.0012234 0.00082384 0.0010422 v omega 15.388 1.0313e+05 2666.7 500.14 v TempK 288 342.01 293.82 290.81 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.2342e-14 9.5808e-05 5.8843e-05 7.6537e-05 v CourantNb 2.5607e-09 0.00020783 1.3817e-05 8.1533e-06 v FourierNb 0.10457 0.6281 0.19098 0.1619 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9485 4.9485 0.00052056 -5.2294e-07 v volume_forces[Z] -4.9485 4.9485 -0.00052043 6.2418e-07 v ǁvolume_forcesǁ 1.6283e-08 4.9497 0.52713 0.25285 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.03 290.96 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015558 5.5032e-05 3.0809e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.10461 0.6281 0.19099 0.1619 INSTANT 0.655803000E+00 TIME STEP NUMBER 681 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.77280E-05 0.23378E-02 Friction velocity uk : 0.77288E-05 0.23377E-02 Dimensionless distance yplus : 0.51465E-04 0.15553E-01 Friction thermal sca. tstar : -0.16328E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.36146E-04 0.10924E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.77280E-05 0.23378E-02 Friction velocity uk : 0.77288E-05 0.23377E-02 Dimensionless distance yplus : 0.51465E-04 0.15553E-01 Friction thermal sca. tstar : -0.16328E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.36146E-04 0.10924E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.35392E-08 3 0.15209E-06 0.26006E-12 0.10340E+01 c Velocity[X] 0.91699E-32 c Velocity[Y] 0.13003E-12 c Velocity[Z] 0.13003E-12 c Pressure 0.10023E-13 15 0.78051E-07 0.78051E-07 0.11723E+01 c k 0.37259E-06 2 0.41654E-07 0.27421E-08 0.15411E+01 c omega 0.13153E+02 1 0.14643E-08 0.31366E+00 0.29157E-02 c TempK 0.94649E+02 1 0.10569E-06 0.24152E-01 0.17213E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.9679e-14 8.3122e-14 -1.0296e-17 -2.6622e-18 v Velocity[Y] -0.00012697 0.00012164 -8.3307e-10 -3.8995e-12 v Velocity[Z] -0.00012161 0.00012697 5.7797e-10 -2.1457e-12 v ǁVelocityǁ 4.4037e-10 0.00013623 1.075e-05 7.2664e-06 v Pressure -0.0011503 0.021039 0.0011765 5.9175e-20 v k 1.0481e-09 0.0012217 0.00082255 0.0010407 v omega 15.37 1.0313e+05 2666.7 500.12 v TempK 288 342.01 293.82 290.82 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.2294e-14 9.5796e-05 5.8822e-05 7.6513e-05 v CourantNb 2.564e-09 0.00020772 1.3817e-05 8.1566e-06 v FourierNb 0.10447 0.6281 0.19093 0.16185 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9485 4.9485 0.00052079 -5.2328e-07 v volume_forces[Z] -4.9485 4.9485 -0.00052066 6.2456e-07 v ǁvolume_forcesǁ 1.6101e-08 4.9497 0.52737 0.25303 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.03 290.96 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015553 5.5016e-05 3.0799e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.10452 0.6281 0.19095 0.16186 INSTANT 0.656766000E+00 TIME STEP NUMBER 682 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.76716E-05 0.23371E-02 Friction velocity uk : 0.76724E-05 0.23370E-02 Dimensionless distance yplus : 0.51090E-04 0.15549E-01 Friction thermal sca. tstar : -0.16633E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.35882E-04 0.10920E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.76716E-05 0.23371E-02 Friction velocity uk : 0.76724E-05 0.23370E-02 Dimensionless distance yplus : 0.51090E-04 0.15549E-01 Friction thermal sca. tstar : -0.16633E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.35882E-04 0.10920E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.35404E-08 3 0.15171E-06 0.25955E-12 0.10329E+01 c Velocity[X] 0.91279E-32 c Velocity[Y] 0.12977E-12 c Velocity[Z] 0.12977E-12 c Pressure 0.99942E-14 15 0.77825E-07 0.77825E-07 0.11705E+01 c k 0.37205E-06 2 0.41573E-07 0.27275E-08 0.15393E+01 c omega 0.13153E+02 1 0.14600E-08 0.31211E+00 0.29084E-02 c TempK 0.94650E+02 1 0.10548E-06 0.24099E-01 0.17194E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.961e-14 8.3066e-14 -1.0289e-17 -2.6606e-18 v Velocity[Y] -0.00012693 0.00012158 -8.3118e-10 -3.893e-12 v Velocity[Z] -0.00012156 0.00012693 5.7582e-10 -2.1462e-12 v ǁVelocityǁ 4.3535e-10 0.00013618 1.0754e-05 7.2725e-06 v Pressure -0.0011519 0.021054 0.0011775 5.0987e-20 v k 1.0441e-09 0.0012201 0.00082127 0.0010391 v omega 15.351 1.0313e+05 2666.6 500.11 v TempK 288 342.01 293.82 290.82 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.2247e-14 9.5784e-05 5.88e-05 7.6488e-05 v CourantNb 2.5672e-09 0.00020761 1.3816e-05 8.1599e-06 v FourierNb 0.10438 0.6281 0.19089 0.16181 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9486 4.9486 0.00052102 -5.2362e-07 v volume_forces[Z] -4.9486 4.9486 -0.00052089 6.2493e-07 v ǁvolume_forcesǁ 1.5919e-08 4.9498 0.5276 0.25322 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.03 290.96 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015549 5.5e-05 3.0789e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.10442 0.6281 0.1909 0.16182 INSTANT 0.657729000E+00 TIME STEP NUMBER 683 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.76147E-05 0.23364E-02 Friction velocity uk : 0.76154E-05 0.23364E-02 Dimensionless distance yplus : 0.50710E-04 0.15544E-01 Friction thermal sca. tstar : -0.16956E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.35616E-04 0.10917E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.76147E-05 0.23364E-02 Friction velocity uk : 0.76154E-05 0.23364E-02 Dimensionless distance yplus : 0.50710E-04 0.15544E-01 Friction thermal sca. tstar : -0.16956E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.35616E-04 0.10917E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.35415E-08 3 0.15133E-06 0.25904E-12 0.10319E+01 c Velocity[X] 0.90869E-32 c Velocity[Y] 0.12952E-12 c Velocity[Z] 0.12952E-12 c Pressure 0.99722E-14 15 0.77652E-07 0.77652E-07 0.11687E+01 c k 0.37151E-06 2 0.41492E-07 0.27131E-08 0.15374E+01 c omega 0.13153E+02 1 0.14556E-08 0.31056E+00 0.29012E-02 c TempK 0.94650E+02 1 0.10526E-06 0.24046E-01 0.17175E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.9542e-14 8.3011e-14 -1.0282e-17 -2.659e-18 v Velocity[Y] -0.00012689 0.00012153 -8.2929e-10 -3.8865e-12 v Velocity[Z] -0.0001215 0.0001269 5.7365e-10 -2.1467e-12 v ǁVelocityǁ 4.3034e-10 0.00013614 1.0757e-05 7.2786e-06 v Pressure -0.0011536 0.021069 0.0011786 -4.1182e-21 v k 1.0401e-09 0.0012185 0.00081998 0.0010375 v omega 15.333 1.0313e+05 2666.6 500.09 v TempK 288 342.01 293.82 290.82 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.2199e-14 9.5772e-05 5.8779e-05 7.6464e-05 v CourantNb 2.5704e-09 0.00020749 1.3815e-05 8.1632e-06 v FourierNb 0.10428 0.6281 0.19084 0.16177 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9486 4.9487 0.00052126 -5.2396e-07 v volume_forces[Z] -4.9486 4.9487 -0.00052112 6.2531e-07 v ǁvolume_forcesǁ 1.5738e-08 4.9498 0.52783 0.2534 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.04 290.96 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015544 5.4983e-05 3.078e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.10432 0.6281 0.19086 0.16177 INSTANT 0.658692000E+00 TIME STEP NUMBER 684 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.75571E-05 0.23357E-02 Friction velocity uk : 0.75579E-05 0.23357E-02 Dimensionless distance yplus : 0.50327E-04 0.15540E-01 Friction thermal sca. tstar : -0.17299E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.35347E-04 0.10914E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.75571E-05 0.23357E-02 Friction velocity uk : 0.75579E-05 0.23357E-02 Dimensionless distance yplus : 0.50327E-04 0.15540E-01 Friction thermal sca. tstar : -0.17299E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.35347E-04 0.10914E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.35427E-08 3 0.15093E-06 0.25853E-12 0.10308E+01 c Velocity[X] 0.90459E-32 c Velocity[Y] 0.12926E-12 c Velocity[Z] 0.12926E-12 c Pressure 0.99501E-14 15 0.77479E-07 0.77479E-07 0.11669E+01 c k 0.37097E-06 2 0.41412E-07 0.26987E-08 0.15356E+01 c omega 0.13153E+02 1 0.14513E-08 0.30903E+00 0.28940E-02 c TempK 0.94651E+02 1 0.10504E-06 0.23994E-01 0.17156E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.9474e-14 8.2955e-14 -1.0276e-17 -2.6574e-18 v Velocity[Y] -0.00012685 0.00012147 -8.2739e-10 -3.8799e-12 v Velocity[Z] -0.00012145 0.00012686 5.7149e-10 -2.1472e-12 v ǁVelocityǁ 4.2534e-10 0.0001361 1.076e-05 7.2847e-06 v Pressure -0.0011553 0.021084 0.0011796 2.3533e-20 v k 1.0361e-09 0.0012168 0.0008187 0.001036 v omega 15.314 1.0313e+05 2666.6 500.07 v TempK 288 342.01 293.83 290.82 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.2152e-14 9.576e-05 5.8758e-05 7.644e-05 v CourantNb 2.5736e-09 0.00020738 1.3815e-05 8.1665e-06 v FourierNb 0.10419 0.6281 0.1908 0.16172 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9487 4.9487 0.00052149 -5.2429e-07 v volume_forces[Z] -4.9487 4.9487 -0.00052136 6.2568e-07 v ǁvolume_forcesǁ 1.5557e-08 4.9499 0.52806 0.25359 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.04 290.96 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.01554 5.4967e-05 3.077e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.10423 0.6281 0.19081 0.16173 INSTANT 0.659655000E+00 TIME STEP NUMBER 685 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.74990E-05 0.23351E-02 Friction velocity uk : 0.74998E-05 0.23350E-02 Dimensionless distance yplus : 0.49940E-04 0.15535E-01 Friction thermal sca. tstar : -0.17662E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.35075E-04 0.10911E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.74990E-05 0.23351E-02 Friction velocity uk : 0.74998E-05 0.23350E-02 Dimensionless distance yplus : 0.49940E-04 0.15535E-01 Friction thermal sca. tstar : -0.17662E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.35075E-04 0.10911E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.35438E-08 3 0.15054E-06 0.25802E-12 0.10297E+01 c Velocity[X] 0.90049E-32 c Velocity[Y] 0.12901E-12 c Velocity[Z] 0.12901E-12 c Pressure 0.99282E-14 15 0.77308E-07 0.77308E-07 0.11651E+01 c k 0.37043E-06 2 0.41332E-07 0.26845E-08 0.15337E+01 c omega 0.13153E+02 1 0.14470E-08 0.30750E+00 0.28869E-02 c TempK 0.94652E+02 1 0.10482E-06 0.23941E-01 0.17137E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.9406e-14 8.29e-14 -1.0269e-17 -2.6558e-18 v Velocity[Y] -0.00012682 0.00012142 -8.2549e-10 -3.8734e-12 v Velocity[Z] -0.00012139 0.00012682 5.6932e-10 -2.1476e-12 v ǁVelocityǁ 4.2034e-10 0.00013606 1.0764e-05 7.2908e-06 v Pressure -0.001157 0.021099 0.0011807 -6.0793e-21 v k 1.0321e-09 0.0012152 0.00081743 0.0010344 v omega 15.296 1.0313e+05 2666.6 500.06 v TempK 288 342.01 293.83 290.82 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.2106e-14 9.5748e-05 5.8737e-05 7.6416e-05 v CourantNb 2.5769e-09 0.00020727 1.3814e-05 8.1698e-06 v FourierNb 0.10409 0.6281 0.19076 0.16168 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9488 4.9488 0.00052172 -5.2463e-07 v volume_forces[Z] -4.9488 4.9488 -0.00052159 6.2605e-07 v ǁvolume_forcesǁ 1.5376e-08 4.95 0.52829 0.25377 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.04 290.97 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015535 5.4951e-05 3.076e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.10413 0.6281 0.19077 0.16169 INSTANT 0.660618000E+00 TIME STEP NUMBER 686 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.74403E-05 0.23344E-02 Friction velocity uk : 0.74411E-05 0.23344E-02 Dimensionless distance yplus : 0.49549E-04 0.15531E-01 Friction thermal sca. tstar : -0.18050E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.34800E-04 0.10908E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.74403E-05 0.23344E-02 Friction velocity uk : 0.74411E-05 0.23344E-02 Dimensionless distance yplus : 0.49549E-04 0.15531E-01 Friction thermal sca. tstar : -0.18050E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.34800E-04 0.10908E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.35450E-08 3 0.15020E-06 0.25751E-12 0.10287E+01 c Velocity[X] 0.89643E-32 c Velocity[Y] 0.12876E-12 c Velocity[Z] 0.12876E-12 c Pressure 0.99097E-14 15 0.77162E-07 0.77162E-07 0.11633E+01 c k 0.36990E-06 2 0.41252E-07 0.26703E-08 0.15319E+01 c omega 0.13153E+02 1 0.14427E-08 0.30598E+00 0.28798E-02 c TempK 0.94652E+02 1 0.10461E-06 0.23889E-01 0.17119E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.9338e-14 8.2845e-14 -1.0263e-17 -2.6542e-18 v Velocity[Y] -0.00012678 0.00012136 -8.2358e-10 -3.8669e-12 v Velocity[Z] -0.00012134 0.00012678 5.6714e-10 -2.1481e-12 v ǁVelocityǁ 4.1536e-10 0.00013602 1.0767e-05 7.2969e-06 v Pressure -0.0011587 0.021115 0.0011818 -3.0494e-20 v k 1.0281e-09 0.0012136 0.00081616 0.0010329 v omega 15.277 1.0313e+05 2666.6 500.04 v TempK 288 342.01 293.83 290.83 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.2059e-14 9.5736e-05 5.8716e-05 7.6392e-05 v CourantNb 2.5801e-09 0.00020715 1.3814e-05 8.1731e-06 v FourierNb 0.104 0.6281 0.19071 0.16164 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9488 4.9489 0.00052195 -5.2496e-07 v volume_forces[Z] -4.9488 4.9489 -0.00052182 6.2643e-07 v ǁvolume_forcesǁ 1.5195e-08 4.95 0.52852 0.25396 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.04 290.97 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015531 5.4935e-05 3.0751e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.10404 0.6281 0.19073 0.16164 INSTANT 0.661581000E+00 TIME STEP NUMBER 687 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.73809E-05 0.23337E-02 Friction velocity uk : 0.73817E-05 0.23337E-02 Dimensionless distance yplus : 0.49154E-04 0.15526E-01 Friction thermal sca. tstar : -0.18463E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.34523E-04 0.10905E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.73809E-05 0.23337E-02 Friction velocity uk : 0.73817E-05 0.23337E-02 Dimensionless distance yplus : 0.49154E-04 0.15526E-01 Friction thermal sca. tstar : -0.18463E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.34523E-04 0.10905E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.35461E-08 3 0.14976E-06 0.25701E-12 0.10276E+01 c Velocity[X] 0.89242E-32 c Velocity[Y] 0.12850E-12 c Velocity[Z] 0.12850E-12 c Pressure 0.98901E-14 15 0.77008E-07 0.77008E-07 0.11616E+01 c k 0.36936E-06 2 0.41172E-07 0.26562E-08 0.15301E+01 c omega 0.13153E+02 1 0.14385E-08 0.30448E+00 0.28727E-02 c TempK 0.94653E+02 1 0.10439E-06 0.23837E-01 0.17100E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.927e-14 8.279e-14 -1.0256e-17 -2.6527e-18 v Velocity[Y] -0.00012674 0.00012131 -8.2167e-10 -3.8605e-12 v Velocity[Z] -0.00012129 0.00012675 5.6497e-10 -2.1486e-12 v ǁVelocityǁ 4.1038e-10 0.00013598 1.077e-05 7.303e-06 v Pressure -0.0011603 0.02113 0.0011828 -7.2608e-20 v k 1.0242e-09 0.001212 0.00081489 0.0010313 v omega 15.259 1.0313e+05 2666.6 500.03 v TempK 288 342.01 293.83 290.83 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.2013e-14 9.5724e-05 5.8695e-05 7.6368e-05 v CourantNb 2.5833e-09 0.00020704 1.3813e-05 8.1764e-06 v FourierNb 0.1039 0.6281 0.19067 0.16159 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9489 4.9489 0.00052218 -5.253e-07 v volume_forces[Z] -4.9489 4.9489 -0.00052205 6.268e-07 v ǁvolume_forcesǁ 1.5015e-08 4.9501 0.52875 0.25414 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.05 290.97 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015526 5.4919e-05 3.0741e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.10394 0.6281 0.19068 0.1616 INSTANT 0.662544000E+00 TIME STEP NUMBER 688 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.73210E-05 0.23331E-02 Friction velocity uk : 0.73217E-05 0.23330E-02 Dimensionless distance yplus : 0.48755E-04 0.15522E-01 Friction thermal sca. tstar : -0.18906E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.34242E-04 0.10902E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.73210E-05 0.23331E-02 Friction velocity uk : 0.73217E-05 0.23330E-02 Dimensionless distance yplus : 0.48755E-04 0.15522E-01 Friction thermal sca. tstar : -0.18906E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.34242E-04 0.10902E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.35473E-08 3 0.14938E-06 0.25650E-12 0.10266E+01 c Velocity[X] 0.88835E-32 c Velocity[Y] 0.12825E-12 c Velocity[Z] 0.12825E-12 c Pressure 0.98644E-14 15 0.76807E-07 0.76807E-07 0.11598E+01 c k 0.36883E-06 2 0.41092E-07 0.26422E-08 0.15283E+01 c omega 0.13153E+02 1 0.14342E-08 0.30298E+00 0.28656E-02 c TempK 0.94653E+02 1 0.10418E-06 0.23786E-01 0.17081E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.9203e-14 8.2735e-14 -1.0249e-17 -2.6511e-18 v Velocity[Y] -0.0001267 0.00012126 -8.1975e-10 -3.854e-12 v Velocity[Z] -0.00012123 0.00012671 5.6278e-10 -2.149e-12 v ǁVelocityǁ 4.0542e-10 0.00013594 1.0774e-05 7.3091e-06 v Pressure -0.001162 0.021145 0.0011839 3.9319e-20 v k 1.0203e-09 0.0012104 0.00081362 0.0010298 v omega 15.24 1.0313e+05 2666.6 500.01 v TempK 288 342.01 293.84 290.83 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.1967e-14 9.5712e-05 5.8674e-05 7.6343e-05 v CourantNb 2.5865e-09 0.00020693 1.3812e-05 8.1797e-06 v FourierNb 0.10381 0.6281 0.19062 0.16155 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.949 4.949 0.00052241 -5.2563e-07 v volume_forces[Z] -4.949 4.949 -0.00052228 6.2717e-07 v ǁvolume_forcesǁ 1.4835e-08 4.9501 0.52898 0.25433 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.05 290.97 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015522 5.4903e-05 3.0731e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.10385 0.6281 0.19064 0.16156 INSTANT 0.663507000E+00 TIME STEP NUMBER 689 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.72603E-05 0.23324E-02 Friction velocity uk : 0.72611E-05 0.23324E-02 Dimensionless distance yplus : 0.48351E-04 0.15518E-01 Friction thermal sca. tstar : -0.19382E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.33959E-04 0.10899E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.72603E-05 0.23324E-02 Friction velocity uk : 0.72611E-05 0.23324E-02 Dimensionless distance yplus : 0.48351E-04 0.15518E-01 Friction thermal sca. tstar : -0.19382E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.33959E-04 0.10899E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.35484E-08 3 0.14899E-06 0.25600E-12 0.10255E+01 c Velocity[X] 0.88435E-32 c Velocity[Y] 0.12800E-12 c Velocity[Z] 0.12800E-12 c Pressure 0.98423E-14 15 0.76633E-07 0.76633E-07 0.11580E+01 c k 0.36830E-06 2 0.41013E-07 0.26283E-08 0.15265E+01 c omega 0.13153E+02 1 0.14300E-08 0.30149E+00 0.28585E-02 c TempK 0.94654E+02 1 0.10396E-06 0.23734E-01 0.17063E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.9135e-14 8.268e-14 -1.0243e-17 -2.6495e-18 v Velocity[Y] -0.00012667 0.0001212 -8.1783e-10 -3.8476e-12 v Velocity[Z] -0.00012118 0.00012667 5.606e-10 -2.1495e-12 v ǁVelocityǁ 4.0047e-10 0.0001359 1.0777e-05 7.3152e-06 v Pressure -0.0011637 0.02116 0.0011849 1.336e-19 v k 1.0164e-09 0.0012088 0.00081236 0.0010283 v omega 15.222 1.0313e+05 2666.6 499.99 v TempK 288 342.01 293.84 290.83 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.1921e-14 9.57e-05 5.8654e-05 7.6319e-05 v CourantNb 2.5897e-09 0.00020682 1.3812e-05 8.183e-06 v FourierNb 0.10371 0.6281 0.19058 0.16151 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.949 4.949 0.00052264 -5.2596e-07 v volume_forces[Z] -4.949 4.949 -0.00052251 6.2754e-07 v ǁvolume_forcesǁ 1.4656e-08 4.9502 0.52921 0.25451 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.05 290.97 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015518 5.4888e-05 3.0722e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.10376 0.6281 0.19059 0.16152 INSTANT 0.664470000E+00 TIME STEP NUMBER 690 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.71990E-05 0.23318E-02 Friction velocity uk : 0.71998E-05 0.23317E-02 Dimensionless distance yplus : 0.47943E-04 0.15513E-01 Friction thermal sca. tstar : -0.19896E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.33672E-04 0.10896E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.71990E-05 0.23318E-02 Friction velocity uk : 0.71998E-05 0.23317E-02 Dimensionless distance yplus : 0.47943E-04 0.15513E-01 Friction thermal sca. tstar : -0.19896E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.33672E-04 0.10896E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.35496E-08 3 0.14859E-06 0.25550E-12 0.10245E+01 c Velocity[X] 0.88037E-32 c Velocity[Y] 0.12775E-12 c Velocity[Z] 0.12775E-12 c Pressure 0.98228E-14 15 0.76480E-07 0.76480E-07 0.11563E+01 c k 0.36777E-06 2 0.40934E-07 0.26145E-08 0.15247E+01 c omega 0.13153E+02 1 0.14258E-08 0.30001E+00 0.28515E-02 c TempK 0.94655E+02 1 0.10375E-06 0.23683E-01 0.17044E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.9068e-14 8.2626e-14 -1.0236e-17 -2.648e-18 v Velocity[Y] -0.00012663 0.00012115 -8.1591e-10 -3.8412e-12 v Velocity[Z] -0.00012112 0.00012663 5.5841e-10 -2.1499e-12 v ǁVelocityǁ 3.9553e-10 0.00013586 1.078e-05 7.3213e-06 v Pressure -0.0011653 0.021175 0.001186 -5.9322e-21 v k 1.0125e-09 0.0012072 0.0008111 0.0010267 v omega 15.204 1.0313e+05 2666.5 499.98 v TempK 288 342.01 293.84 290.83 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.1876e-14 9.5688e-05 5.8633e-05 7.6295e-05 v CourantNb 2.5929e-09 0.00020671 1.3811e-05 8.1864e-06 v FourierNb 0.10362 0.6281 0.19054 0.16146 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9491 4.9491 0.00052287 -5.263e-07 v volume_forces[Z] -4.9491 4.9491 -0.00052274 6.2791e-07 v ǁvolume_forcesǁ 1.4477e-08 4.9503 0.52944 0.2547 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.05 290.98 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015513 5.4872e-05 3.0712e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.10366 0.6281 0.19055 0.16147 INSTANT 0.665433000E+00 TIME STEP NUMBER 691 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.71371E-05 0.23311E-02 Friction velocity uk : 0.71379E-05 0.23311E-02 Dimensionless distance yplus : 0.47530E-04 0.15509E-01 Friction thermal sca. tstar : -0.20452E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.33382E-04 0.10892E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.71371E-05 0.23311E-02 Friction velocity uk : 0.71379E-05 0.23311E-02 Dimensionless distance yplus : 0.47530E-04 0.15509E-01 Friction thermal sca. tstar : -0.20452E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.33382E-04 0.10892E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.35508E-08 3 0.14822E-06 0.25500E-12 0.10234E+01 c Velocity[X] 0.87638E-32 c Velocity[Y] 0.12750E-12 c Velocity[Z] 0.12750E-12 c Pressure 0.97997E-14 15 0.76299E-07 0.76299E-07 0.11545E+01 c k 0.36724E-06 2 0.40855E-07 0.26008E-08 0.15229E+01 c omega 0.13153E+02 1 0.14216E-08 0.29854E+00 0.28445E-02 c TempK 0.94655E+02 1 0.10354E-06 0.23631E-01 0.17025E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.9001e-14 8.2571e-14 -1.023e-17 -2.6464e-18 v Velocity[Y] -0.00012659 0.0001211 -8.1397e-10 -3.8348e-12 v Velocity[Z] -0.00012107 0.0001266 5.5622e-10 -2.1503e-12 v ǁVelocityǁ 3.9061e-10 0.00013582 1.0784e-05 7.3274e-06 v Pressure -0.001167 0.02119 0.001187 -2.1621e-20 v k 1.0086e-09 0.0012056 0.00080985 0.0010252 v omega 15.186 1.0313e+05 2666.5 499.96 v TempK 288 342.02 293.84 290.84 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.183e-14 9.5676e-05 5.8612e-05 7.6271e-05 v CourantNb 2.5961e-09 0.00020659 1.3811e-05 8.1897e-06 v FourierNb 0.10353 0.6281 0.19049 0.16142 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9491 4.9492 0.0005231 -5.2663e-07 v volume_forces[Z] -4.9491 4.9492 -0.00052297 6.2828e-07 v ǁvolume_forcesǁ 1.4298e-08 4.9503 0.52967 0.25488 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.06 290.98 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015509 5.4856e-05 3.0702e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.10357 0.6281 0.19051 0.16143 INSTANT 0.666396000E+00 TIME STEP NUMBER 692 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.70744E-05 0.23304E-02 Friction velocity uk : 0.70752E-05 0.23304E-02 Dimensionless distance yplus : 0.47113E-04 0.15504E-01 Friction thermal sca. tstar : -0.21057E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.33089E-04 0.10889E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.70744E-05 0.23304E-02 Friction velocity uk : 0.70752E-05 0.23304E-02 Dimensionless distance yplus : 0.47113E-04 0.15504E-01 Friction thermal sca. tstar : -0.21057E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.33089E-04 0.10889E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.35519E-08 3 0.14783E-06 0.25449E-12 0.10223E+01 c Velocity[X] 0.87246E-32 c Velocity[Y] 0.12725E-12 c Velocity[Z] 0.12725E-12 c Pressure 0.97798E-14 15 0.76142E-07 0.76142E-07 0.11528E+01 c k 0.36671E-06 2 0.40777E-07 0.25871E-08 0.15211E+01 c omega 0.13153E+02 1 0.14174E-08 0.29707E+00 0.28375E-02 c TempK 0.94656E+02 1 0.10332E-06 0.23580E-01 0.17007E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.8934e-14 8.2517e-14 -1.0223e-17 -2.6448e-18 v Velocity[Y] -0.00012656 0.00012104 -8.1204e-10 -3.8284e-12 v Velocity[Z] -0.00012102 0.00012656 5.5402e-10 -2.1508e-12 v ǁVelocityǁ 3.857e-10 0.00013578 1.0787e-05 7.3335e-06 v Pressure -0.0011687 0.021205 0.0011881 1.2433e-19 v k 1.0048e-09 0.001204 0.0008086 0.0010237 v omega 15.168 1.0313e+05 2666.5 499.94 v TempK 288 342.02 293.85 290.84 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.1785e-14 9.5665e-05 5.8591e-05 7.6247e-05 v CourantNb 2.5993e-09 0.00020648 1.381e-05 8.193e-06 v FourierNb 0.10344 0.6281 0.19045 0.16138 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9492 4.9492 0.00052333 -5.2696e-07 v volume_forces[Z] -4.9492 4.9492 -0.0005232 6.2865e-07 v ǁvolume_forcesǁ 1.4121e-08 4.9504 0.5299 0.25507 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.06 290.98 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015504 5.484e-05 3.0693e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.10348 0.6281 0.19046 0.16139 INSTANT 0.667359000E+00 TIME STEP NUMBER 693 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.70110E-05 0.23298E-02 Friction velocity uk : 0.70118E-05 0.23297E-02 Dimensionless distance yplus : 0.46691E-04 0.15500E-01 Friction thermal sca. tstar : -0.21719E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.32793E-04 0.10886E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.70110E-05 0.23298E-02 Friction velocity uk : 0.70118E-05 0.23297E-02 Dimensionless distance yplus : 0.46691E-04 0.15500E-01 Friction thermal sca. tstar : -0.21719E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.32793E-04 0.10886E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.35531E-08 3 0.14747E-06 0.25400E-12 0.10213E+01 c Velocity[X] 0.86853E-32 c Velocity[Y] 0.12700E-12 c Velocity[Z] 0.12700E-12 c Pressure 0.97634E-14 15 0.76014E-07 0.76014E-07 0.11510E+01 c k 0.36619E-06 2 0.40699E-07 0.25736E-08 0.15193E+01 c omega 0.13153E+02 1 0.14132E-08 0.29562E+00 0.28306E-02 c TempK 0.94656E+02 1 0.10311E-06 0.23529E-01 0.16988E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.8867e-14 8.2462e-14 -1.0217e-17 -2.6433e-18 v Velocity[Y] -0.00012652 0.00012099 -8.1009e-10 -3.8221e-12 v Velocity[Z] -0.00012096 0.00012652 5.5182e-10 -2.1512e-12 v ǁVelocityǁ 3.8081e-10 0.00013574 1.079e-05 7.3396e-06 v Pressure -0.0011704 0.02122 0.0011891 -7.3343e-20 v k 1.001e-09 0.0012024 0.00080735 0.0010222 v omega 15.149 1.0313e+05 2666.5 499.93 v TempK 288 342.02 293.85 290.84 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.174e-14 9.5653e-05 5.857e-05 7.6223e-05 v CourantNb 2.6025e-09 0.00020637 1.381e-05 8.1964e-06 v FourierNb 0.10334 0.6281 0.19041 0.16134 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9493 4.9493 0.00052356 -5.2729e-07 v volume_forces[Z] -4.9493 4.9493 -0.00052343 6.2902e-07 v ǁvolume_forcesǁ 1.3943e-08 4.9504 0.53012 0.25525 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.06 290.98 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.0155 5.4824e-05 3.0683e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.10338 0.6281 0.19042 0.16134 INSTANT 0.668322000E+00 TIME STEP NUMBER 694 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.69468E-05 0.23291E-02 Friction velocity uk : 0.69477E-05 0.23291E-02 Dimensionless distance yplus : 0.46264E-04 0.15496E-01 Friction thermal sca. tstar : -0.22450E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.32493E-04 0.10883E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.69468E-05 0.23291E-02 Friction velocity uk : 0.69477E-05 0.23291E-02 Dimensionless distance yplus : 0.46264E-04 0.15496E-01 Friction thermal sca. tstar : -0.22450E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.32493E-04 0.10883E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.35543E-08 3 0.14709E-06 0.25350E-12 0.10202E+01 c Velocity[X] 0.86466E-32 c Velocity[Y] 0.12675E-12 c Velocity[Z] 0.12675E-12 c Pressure 0.97379E-14 15 0.75814E-07 0.75814E-07 0.11493E+01 c k 0.36566E-06 2 0.40621E-07 0.25601E-08 0.15175E+01 c omega 0.13153E+02 1 0.14091E-08 0.29418E+00 0.28237E-02 c TempK 0.94657E+02 1 0.10290E-06 0.23479E-01 0.16970E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.8801e-14 8.2408e-14 -1.021e-17 -2.6417e-18 v Velocity[Y] -0.00012648 0.00012094 -8.0815e-10 -3.8158e-12 v Velocity[Z] -0.00012091 0.00012649 5.4961e-10 -2.1516e-12 v ǁVelocityǁ 3.7594e-10 0.0001357 1.0794e-05 7.3457e-06 v Pressure -0.001172 0.021235 0.0011902 2.2846e-20 v k 9.972e-10 0.0012008 0.00080611 0.0010206 v omega 15.131 1.0313e+05 2666.5 499.91 v TempK 288 342.02 293.85 290.84 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.1696e-14 9.5641e-05 5.8549e-05 7.62e-05 v CourantNb 2.6057e-09 0.00020626 1.3809e-05 8.1997e-06 v FourierNb 0.10325 0.6281 0.19036 0.16129 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9493 4.9493 0.00052379 -5.2762e-07 v volume_forces[Z] -4.9493 4.9493 -0.00052366 6.2938e-07 v ǁvolume_forcesǁ 1.3766e-08 4.9505 0.53035 0.25543 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.06 290.98 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015496 5.4808e-05 3.0674e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.10329 0.6281 0.19038 0.1613 INSTANT 0.669285000E+00 TIME STEP NUMBER 695 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.68819E-05 0.23285E-02 Friction velocity uk : 0.68828E-05 0.23284E-02 Dimensionless distance yplus : 0.45832E-04 0.15491E-01 Friction thermal sca. tstar : -0.23258E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.32189E-04 0.10880E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.68819E-05 0.23285E-02 Friction velocity uk : 0.68828E-05 0.23284E-02 Dimensionless distance yplus : 0.45832E-04 0.15491E-01 Friction thermal sca. tstar : -0.23258E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.32189E-04 0.10880E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.35555E-08 3 0.14672E-06 0.25300E-12 0.10192E+01 c Velocity[X] 0.86080E-32 c Velocity[Y] 0.12650E-12 c Velocity[Z] 0.12650E-12 c Pressure 0.97541E-14 15 0.75939E-07 0.75939E-07 0.11476E+01 c k 0.36514E-06 2 0.40543E-07 0.25468E-08 0.15157E+01 c omega 0.13153E+02 1 0.14050E-08 0.29274E+00 0.28168E-02 c TempK 0.94657E+02 1 0.10269E-06 0.23428E-01 0.16952E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.8734e-14 8.2354e-14 -1.0204e-17 -2.6402e-18 v Velocity[Y] -0.00012645 0.00012088 -8.062e-10 -3.8095e-12 v Velocity[Z] -0.00012086 0.00012645 5.4741e-10 -2.1518e-12 v ǁVelocityǁ 3.7109e-10 0.00013566 1.0797e-05 7.3518e-06 v Pressure -0.0011737 0.02125 0.0011912 6.3636e-20 v k 9.9342e-10 0.0011993 0.00080486 0.0010191 v omega 15.113 1.0313e+05 2666.5 499.9 v TempK 288 342.02 293.85 290.84 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.1652e-14 9.5629e-05 5.8529e-05 7.6176e-05 v CourantNb 2.6089e-09 0.00020615 1.3809e-05 8.2031e-06 v FourierNb 0.10316 0.6281 0.19032 0.16125 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9494 4.9494 0.00052402 -5.2795e-07 v volume_forces[Z] -4.9494 4.9494 -0.00052389 6.2975e-07 v ǁvolume_forcesǁ 1.359e-08 4.9506 0.53058 0.25562 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.07 290.99 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015491 5.4792e-05 3.0664e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.1032 0.6281 0.19033 0.16126 INSTANT 0.670248000E+00 TIME STEP NUMBER 696 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.68163E-05 0.23278E-02 Friction velocity uk : 0.68171E-05 0.23278E-02 Dimensionless distance yplus : 0.45394E-04 0.15487E-01 Friction thermal sca. tstar : -0.24158E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.31882E-04 0.10877E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.68163E-05 0.23278E-02 Friction velocity uk : 0.68171E-05 0.23278E-02 Dimensionless distance yplus : 0.45394E-04 0.15487E-01 Friction thermal sca. tstar : -0.24158E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.31882E-04 0.10877E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.35567E-08 3 0.14635E-06 0.25250E-12 0.10181E+01 c Velocity[X] 0.85695E-32 c Velocity[Y] 0.12625E-12 c Velocity[Z] 0.12625E-12 c Pressure 0.97466E-14 15 0.75879E-07 0.75879E-07 0.11458E+01 c k 0.36462E-06 2 0.40466E-07 0.25335E-08 0.15139E+01 c omega 0.13153E+02 1 0.14009E-08 0.29131E+00 0.28099E-02 c TempK 0.94658E+02 1 0.10248E-06 0.23378E-01 0.16933E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.8668e-14 8.23e-14 -1.0198e-17 -2.6386e-18 v Velocity[Y] -0.00012641 0.00012083 -8.0424e-10 -3.803e-12 v Velocity[Z] -0.00012081 0.00012641 5.4519e-10 -2.1523e-12 v ǁVelocityǁ 3.6626e-10 0.00013562 1.08e-05 7.358e-06 v Pressure -0.0011754 0.021265 0.0011922 -1.0786e-21 v k 9.8966e-10 0.0011977 0.00080363 0.0010176 v omega 15.095 1.0313e+05 2666.5 499.88 v TempK 288 342.02 293.86 290.85 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.1607e-14 9.5617e-05 5.8508e-05 7.6152e-05 v CourantNb 2.6121e-09 0.00020604 1.3808e-05 8.2064e-06 v FourierNb 0.10307 0.6281 0.19028 0.16121 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9494 4.9495 0.00052425 -5.2828e-07 v volume_forces[Z] -4.9494 4.9495 -0.00052412 6.3012e-07 v ǁvolume_forcesǁ 1.3415e-08 4.9506 0.53081 0.2558 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.07 290.99 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015487 5.4777e-05 3.0654e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.10311 0.6281 0.19029 0.16122 INSTANT 0.671211000E+00 TIME STEP NUMBER 697 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.67498E-05 0.23272E-02 Friction velocity uk : 0.67506E-05 0.23271E-02 Dimensionless distance yplus : 0.44951E-04 0.15483E-01 Friction thermal sca. tstar : -0.25171E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.31571E-04 0.10874E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.67498E-05 0.23272E-02 Friction velocity uk : 0.67506E-05 0.23271E-02 Dimensionless distance yplus : 0.44951E-04 0.15483E-01 Friction thermal sca. tstar : -0.25171E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.31571E-04 0.10874E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.35579E-08 3 0.14595E-06 0.25201E-12 0.10171E+01 c Velocity[X] 0.85312E-32 c Velocity[Y] 0.12600E-12 c Velocity[Z] 0.12600E-12 c Pressure 0.96741E-14 15 0.75314E-07 0.75314E-07 0.11441E+01 c k 0.36410E-06 2 0.40389E-07 0.25203E-08 0.15121E+01 c omega 0.13153E+02 1 0.13968E-08 0.28989E+00 0.28030E-02 c TempK 0.94659E+02 1 0.10228E-06 0.23328E-01 0.16915E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.8602e-14 8.2246e-14 -1.0191e-17 -2.6371e-18 v Velocity[Y] -0.00012637 0.00012078 -8.0228e-10 -3.7967e-12 v Velocity[Z] -0.00012075 0.00012638 5.4298e-10 -2.1527e-12 v ǁVelocityǁ 3.6145e-10 0.00013558 1.0804e-05 7.3641e-06 v Pressure -0.0011771 0.02128 0.0011933 -5.1968e-21 v k 9.8592e-10 0.0011961 0.00080239 0.0010161 v omega 15.077 1.0313e+05 2666.5 499.86 v TempK 288 342.02 293.86 290.85 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.1563e-14 9.5605e-05 5.8487e-05 7.6128e-05 v CourantNb 2.6152e-09 0.00020593 1.3808e-05 8.2098e-06 v FourierNb 0.10298 0.6281 0.19024 0.16117 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9495 4.9495 0.00052448 -5.2861e-07 v volume_forces[Z] -4.9495 4.9495 -0.00052435 6.3048e-07 v ǁvolume_forcesǁ 1.324e-08 4.9507 0.53103 0.25598 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.07 290.99 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015483 5.4761e-05 3.0645e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.10302 0.6281 0.19025 0.16117 INSTANT 0.672174000E+00 TIME STEP NUMBER 698 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.66824E-05 0.23265E-02 Friction velocity uk : 0.66833E-05 0.23265E-02 Dimensionless distance yplus : 0.44503E-04 0.15478E-01 Friction thermal sca. tstar : -0.26321E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.31256E-04 0.10871E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.66824E-05 0.23265E-02 Friction velocity uk : 0.66833E-05 0.23265E-02 Dimensionless distance yplus : 0.44503E-04 0.15478E-01 Friction thermal sca. tstar : -0.26321E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.31256E-04 0.10871E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.35591E-08 3 0.14558E-06 0.25151E-12 0.10160E+01 c Velocity[X] 0.84931E-32 c Velocity[Y] 0.12576E-12 c Velocity[Z] 0.12576E-12 c Pressure 0.96561E-14 15 0.75173E-07 0.75173E-07 0.11424E+01 c k 0.36358E-06 2 0.40312E-07 0.25072E-08 0.15103E+01 c omega 0.13153E+02 1 0.13927E-08 0.28848E+00 0.27962E-02 c TempK 0.94659E+02 1 0.10207E-06 0.23278E-01 0.16897E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.8536e-14 8.2192e-14 -1.0185e-17 -2.6356e-18 v Velocity[Y] -0.00012634 0.00012073 -8.0031e-10 -3.7904e-12 v Velocity[Z] -0.0001207 0.00012634 5.4076e-10 -2.1531e-12 v ǁVelocityǁ 3.5667e-10 0.00013554 1.0807e-05 7.3702e-06 v Pressure -0.0011787 0.021295 0.0011943 -6.8098e-20 v k 9.822e-10 0.0011945 0.00080116 0.0010146 v omega 15.06 1.0313e+05 2666.4 499.85 v TempK 288 342.02 293.86 290.85 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.152e-14 9.5594e-05 5.8467e-05 7.6104e-05 v CourantNb 2.6184e-09 0.00020582 1.3807e-05 8.2132e-06 v FourierNb 0.10289 0.6281 0.19019 0.16112 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9496 4.9496 0.00052471 -5.2893e-07 v volume_forces[Z] -4.9496 4.9496 -0.00052458 6.3085e-07 v ǁvolume_forcesǁ 1.3066e-08 4.9507 0.53126 0.25617 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.07 290.99 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015478 5.4745e-05 3.0635e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.10293 0.6281 0.19021 0.16113 INSTANT 0.673137000E+00 TIME STEP NUMBER 699 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.66142E-05 0.23259E-02 Friction velocity uk : 0.66151E-05 0.23258E-02 Dimensionless distance yplus : 0.44049E-04 0.15474E-01 Friction thermal sca. tstar : -0.27643E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.30937E-04 0.10868E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.66142E-05 0.23259E-02 Friction velocity uk : 0.66151E-05 0.23258E-02 Dimensionless distance yplus : 0.44049E-04 0.15474E-01 Friction thermal sca. tstar : -0.27643E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.30937E-04 0.10868E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.35603E-08 3 0.14521E-06 0.25102E-12 0.10149E+01 c Velocity[X] 0.84553E-32 c Velocity[Y] 0.12551E-12 c Velocity[Z] 0.12551E-12 c Pressure 0.96371E-14 15 0.75023E-07 0.75023E-07 0.11407E+01 c k 0.36306E-06 2 0.40235E-07 0.24941E-08 0.15086E+01 c omega 0.13153E+02 1 0.13886E-08 0.28708E+00 0.27894E-02 c TempK 0.94660E+02 1 0.10186E-06 0.23228E-01 0.16878E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.847e-14 8.2139e-14 -1.0178e-17 -2.634e-18 v Velocity[Y] -0.0001263 0.00012067 -7.9834e-10 -3.7841e-12 v Velocity[Z] -0.00012065 0.00012631 5.3854e-10 -2.1535e-12 v ǁVelocityǁ 3.5191e-10 0.0001355 1.0811e-05 7.3763e-06 v Pressure -0.0011804 0.02131 0.0011954 -6.8735e-20 v k 9.785e-10 0.001193 0.00079993 0.0010131 v omega 15.042 1.0313e+05 2666.4 499.83 v TempK 288 342.02 293.86 290.85 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.1476e-14 9.5582e-05 5.8446e-05 7.608e-05 v CourantNb 2.6216e-09 0.00020571 1.3807e-05 8.2165e-06 v FourierNb 0.10279 0.6281 0.19015 0.16108 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9496 4.9496 0.00052493 -5.2926e-07 v volume_forces[Z] -4.9496 4.9496 -0.00052481 6.3121e-07 v ǁvolume_forcesǁ 1.2894e-08 4.9508 0.53149 0.25635 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.08 290.99 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015474 5.4729e-05 3.0626e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.10284 0.6281 0.19016 0.16109 INSTANT 0.674100000E+00 TIME STEP NUMBER 700 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.65452E-05 0.23252E-02 Friction velocity uk : 0.65460E-05 0.23252E-02 Dimensionless distance yplus : 0.43589E-04 0.15470E-01 Friction thermal sca. tstar : -0.29187E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.30614E-04 0.10865E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.65452E-05 0.23252E-02 Friction velocity uk : 0.65460E-05 0.23252E-02 Dimensionless distance yplus : 0.43589E-04 0.15470E-01 Friction thermal sca. tstar : -0.29187E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.30614E-04 0.10865E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.35615E-08 3 0.14484E-06 0.25053E-12 0.10139E+01 c Velocity[X] 0.84176E-32 c Velocity[Y] 0.12526E-12 c Velocity[Z] 0.12526E-12 c Pressure 0.96121E-14 15 0.74827E-07 0.74827E-07 0.11390E+01 c k 0.36255E-06 2 0.40159E-07 0.24812E-08 0.15068E+01 c omega 0.13153E+02 1 0.13846E-08 0.28569E+00 0.27826E-02 c TempK 0.94660E+02 1 0.10166E-06 0.23179E-01 0.16860E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.8404e-14 8.2085e-14 -1.0172e-17 -2.6325e-18 v Velocity[Y] -0.00012627 0.00012062 -7.9637e-10 -3.7778e-12 v Velocity[Z] -0.0001206 0.00012627 5.3631e-10 -2.1539e-12 v ǁVelocityǁ 3.4718e-10 0.00013546 1.0814e-05 7.3824e-06 v Pressure -0.0011821 0.021325 0.0011964 -1.0467e-19 v k 9.7482e-10 0.0011914 0.00079871 0.0010116 v omega 15.024 1.0313e+05 2666.4 499.82 v TempK 288 342.02 293.87 290.85 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.1433e-14 9.557e-05 5.8426e-05 7.6057e-05 v CourantNb 2.6247e-09 0.0002056 1.3806e-05 8.2199e-06 v FourierNb 0.1027 0.6281 0.19011 0.16104 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9497 4.9497 0.00052516 -5.2959e-07 v volume_forces[Z] -4.9497 4.9497 -0.00052503 6.3157e-07 v ǁvolume_forcesǁ 1.2722e-08 4.9508 0.53172 0.25653 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.08 291 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.01547 5.4714e-05 3.0616e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.10275 0.6281 0.19012 0.16105 INSTANT 0.675063000E+00 TIME STEP NUMBER 701 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.64752E-05 0.23246E-02 Friction velocity uk : 0.64761E-05 0.23245E-02 Dimensionless distance yplus : 0.43123E-04 0.15465E-01 Friction thermal sca. tstar : -0.31019E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.30287E-04 0.10862E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.64752E-05 0.23246E-02 Friction velocity uk : 0.64761E-05 0.23245E-02 Dimensionless distance yplus : 0.43123E-04 0.15465E-01 Friction thermal sca. tstar : -0.31019E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.30287E-04 0.10862E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.35627E-08 3 0.14447E-06 0.25003E-12 0.10128E+01 c Velocity[X] 0.83802E-32 c Velocity[Y] 0.12502E-12 c Velocity[Z] 0.12502E-12 c Pressure 0.95953E-14 15 0.74695E-07 0.74695E-07 0.11373E+01 c k 0.36203E-06 2 0.40083E-07 0.24683E-08 0.15050E+01 c omega 0.13153E+02 1 0.13805E-08 0.28430E+00 0.27759E-02 c TempK 0.94661E+02 1 0.10145E-06 0.23129E-01 0.16842E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.8338e-14 8.2032e-14 -1.0166e-17 -2.631e-18 v Velocity[Y] -0.00012623 0.00012057 -7.9439e-10 -3.7716e-12 v Velocity[Z] -0.00012054 0.00012624 5.3408e-10 -2.1543e-12 v ǁVelocityǁ 3.4249e-10 0.00013542 1.0817e-05 7.3886e-06 v Pressure -0.0011838 0.02134 0.0011975 7.4618e-20 v k 9.7115e-10 0.0011899 0.00079749 0.0010101 v omega 15.006 1.0313e+05 2666.4 499.8 v TempK 288 342.02 293.87 290.86 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.139e-14 9.5558e-05 5.8405e-05 7.6033e-05 v CourantNb 2.6279e-09 0.00020549 1.3806e-05 8.2232e-06 v FourierNb 0.10261 0.6281 0.19006 0.161 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9497 4.9498 0.00052539 -5.2991e-07 v volume_forces[Z] -4.9497 4.9498 -0.00052526 6.3194e-07 v ǁvolume_forcesǁ 1.2551e-08 4.9509 0.53194 0.25672 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.08 291 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015465 5.4698e-05 3.0607e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.10266 0.6281 0.19008 0.161 INSTANT 0.676026000E+00 TIME STEP NUMBER 702 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.64043E-05 0.23239E-02 Friction velocity uk : 0.64051E-05 0.23239E-02 Dimensionless distance yplus : 0.42651E-04 0.15461E-01 Friction thermal sca. tstar : -0.33246E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.29955E-04 0.10859E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.64043E-05 0.23239E-02 Friction velocity uk : 0.64051E-05 0.23239E-02 Dimensionless distance yplus : 0.42651E-04 0.15461E-01 Friction thermal sca. tstar : -0.33246E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.29955E-04 0.10859E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.35639E-08 3 0.14411E-06 0.24954E-12 0.10118E+01 c Velocity[X] 0.83429E-32 c Velocity[Y] 0.12477E-12 c Velocity[Z] 0.12477E-12 c Pressure 0.95967E-14 15 0.74705E-07 0.74705E-07 0.11356E+01 c k 0.36152E-06 2 0.40007E-07 0.24555E-08 0.15033E+01 c omega 0.13153E+02 1 0.13765E-08 0.28293E+00 0.27691E-02 c TempK 0.94661E+02 1 0.10125E-06 0.23080E-01 0.16824E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.8273e-14 8.1979e-14 -1.0159e-17 -2.6295e-18 v Velocity[Y] -0.0001262 0.00012052 -7.924e-10 -3.7654e-12 v Velocity[Z] -0.00012049 0.0001262 5.3185e-10 -2.1547e-12 v ǁVelocityǁ 3.3782e-10 0.00013538 1.0821e-05 7.3947e-06 v Pressure -0.0011854 0.021355 0.0011985 -1.1046e-19 v k 9.6751e-10 0.0011883 0.00079627 0.0010087 v omega 14.988 1.0313e+05 2666.4 499.79 v TempK 288 342.02 293.87 290.86 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.1347e-14 9.5547e-05 5.8384e-05 7.6009e-05 v CourantNb 2.6311e-09 0.00020538 1.3805e-05 8.2266e-06 v FourierNb 0.10252 0.6281 0.19002 0.16095 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9498 4.9498 0.00052562 -5.3024e-07 v volume_forces[Z] -4.9498 4.9498 -0.00052549 6.323e-07 v ǁvolume_forcesǁ 1.2381e-08 4.951 0.53217 0.2569 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.08 291 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015461 5.4682e-05 3.0597e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.10257 0.6281 0.19004 0.16096 INSTANT 0.676989000E+00 TIME STEP NUMBER 703 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.63324E-05 0.23233E-02 Friction velocity uk : 0.63333E-05 0.23232E-02 Dimensionless distance yplus : 0.42172E-04 0.15457E-01 Friction thermal sca. tstar : -0.36030E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.29619E-04 0.10856E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.63324E-05 0.23233E-02 Friction velocity uk : 0.63333E-05 0.23232E-02 Dimensionless distance yplus : 0.42172E-04 0.15457E-01 Friction thermal sca. tstar : -0.36030E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.29619E-04 0.10856E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.35651E-08 3 0.14373E-06 0.24905E-12 0.10107E+01 c Velocity[X] 0.83058E-32 c Velocity[Y] 0.12453E-12 c Velocity[Z] 0.12453E-12 c Pressure 0.95509E-14 15 0.74348E-07 0.74348E-07 0.11339E+01 c k 0.36101E-06 2 0.39931E-07 0.24428E-08 0.15015E+01 c omega 0.13153E+02 1 0.13725E-08 0.28156E+00 0.27624E-02 c TempK 0.94662E+02 1 0.10104E-06 0.23031E-01 0.16806E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.8207e-14 8.1925e-14 -1.0153e-17 -2.628e-18 v Velocity[Y] -0.00012616 0.00012047 -7.9042e-10 -3.7592e-12 v Velocity[Z] -0.00012044 0.00012616 5.2961e-10 -2.155e-12 v ǁVelocityǁ 3.3319e-10 0.00013534 1.0824e-05 7.4008e-06 v Pressure -0.0011871 0.02137 0.0011995 4.2604e-20 v k 9.6388e-10 0.0011868 0.00079506 0.0010072 v omega 14.971 1.0313e+05 2666.4 499.77 v TempK 288 342.02 293.87 290.86 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.1305e-14 9.5535e-05 5.8364e-05 7.5986e-05 v CourantNb 2.6342e-09 0.00020527 1.3805e-05 8.23e-06 v FourierNb 0.10243 0.6281 0.18998 0.16091 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9499 4.9499 0.00052584 -5.3057e-07 v volume_forces[Z] -4.9499 4.9499 -0.00052572 6.3266e-07 v ǁvolume_forcesǁ 1.2212e-08 4.951 0.53239 0.25708 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.09 291 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015457 5.4666e-05 3.0588e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.10248 0.6281 0.18999 0.16092 INSTANT 0.677952000E+00 TIME STEP NUMBER 704 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.62595E-05 0.23226E-02 Friction velocity uk : 0.62604E-05 0.23226E-02 Dimensionless distance yplus : 0.41687E-04 0.15452E-01 Friction thermal sca. tstar : -0.39654E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.29278E-04 0.10853E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.62595E-05 0.23226E-02 Friction velocity uk : 0.62604E-05 0.23226E-02 Dimensionless distance yplus : 0.41687E-04 0.15452E-01 Friction thermal sca. tstar : -0.39654E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.29278E-04 0.10853E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.35663E-08 3 0.14337E-06 0.24857E-12 0.10097E+01 c Velocity[X] 0.82690E-32 c Velocity[Y] 0.12428E-12 c Velocity[Z] 0.12428E-12 c Pressure 0.95303E-14 15 0.74186E-07 0.74186E-07 0.11322E+01 c k 0.36049E-06 2 0.39856E-07 0.24302E-08 0.14998E+01 c omega 0.13153E+02 1 0.13685E-08 0.28020E+00 0.27558E-02 c TempK 0.94663E+02 1 0.10084E-06 0.22982E-01 0.16788E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.8142e-14 8.1872e-14 -1.0147e-17 -2.6264e-18 v Velocity[Y] -0.00012613 0.00012042 -7.8842e-10 -3.753e-12 v Velocity[Z] -0.00012039 0.00012613 5.2737e-10 -2.1554e-12 v ǁVelocityǁ 3.286e-10 0.0001353 1.0828e-05 7.407e-06 v Pressure -0.0011888 0.021385 0.0012006 -1.1198e-19 v k 9.6027e-10 0.0011852 0.00079385 0.0010057 v omega 14.953 1.0313e+05 2666.4 499.75 v TempK 288 342.02 293.88 290.86 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.1262e-14 9.5523e-05 5.8344e-05 7.5962e-05 v CourantNb 2.6374e-09 0.00020516 1.3805e-05 8.2334e-06 v FourierNb 0.10235 0.6281 0.18994 0.16087 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9499 4.9499 0.00052607 -5.3089e-07 v volume_forces[Z] -4.9499 4.9499 -0.00052594 6.3302e-07 v ǁvolume_forcesǁ 1.2045e-08 4.9511 0.53262 0.25727 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.09 291 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015452 5.4651e-05 3.0578e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.10239 0.6281 0.18995 0.16088 INSTANT 0.678915000E+00 TIME STEP NUMBER 705 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.61855E-05 0.23220E-02 Friction velocity uk : 0.61864E-05 0.23219E-02 Dimensionless distance yplus : 0.41195E-04 0.15448E-01 Friction thermal sca. tstar : -0.44646E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.28933E-04 0.10850E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.61855E-05 0.23220E-02 Friction velocity uk : 0.61864E-05 0.23219E-02 Dimensionless distance yplus : 0.41195E-04 0.15448E-01 Friction thermal sca. tstar : -0.44646E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.28933E-04 0.10850E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.35675E-08 3 0.14300E-06 0.24808E-12 0.10086E+01 c Velocity[X] 0.82324E-32 c Velocity[Y] 0.12404E-12 c Velocity[Z] 0.12404E-12 c Pressure 0.95112E-14 15 0.74036E-07 0.74036E-07 0.11305E+01 c k 0.35999E-06 2 0.39781E-07 0.24177E-08 0.14980E+01 c omega 0.13153E+02 1 0.13646E-08 0.27885E+00 0.27491E-02 c TempK 0.94663E+02 1 0.10064E-06 0.22933E-01 0.16770E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.8077e-14 8.182e-14 -1.014e-17 -2.6249e-18 v Velocity[Y] -0.00012609 0.00012036 -7.8642e-10 -3.7469e-12 v Velocity[Z] -0.00012034 0.00012609 5.2512e-10 -2.1557e-12 v ǁVelocityǁ 3.2404e-10 0.00013526 1.0831e-05 7.4131e-06 v Pressure -0.0011905 0.0214 0.0012016 9.6092e-21 v k 9.5668e-10 0.0011837 0.00079264 0.0010042 v omega 14.935 1.0313e+05 2666.4 499.74 v TempK 288 342.02 293.88 290.87 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.122e-14 9.5512e-05 5.8323e-05 7.5938e-05 v CourantNb 2.6405e-09 0.00020506 1.3804e-05 8.2368e-06 v FourierNb 0.10226 0.6281 0.18989 0.16083 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.95 4.95 0.0005263 -5.3121e-07 v volume_forces[Z] -4.95 4.95 -0.00052617 6.3338e-07 v ǁvolume_forcesǁ 1.1879e-08 4.9511 0.53284 0.25745 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.09 291.01 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015448 5.4635e-05 3.0569e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.1023 0.6281 0.18991 0.16084 INSTANT 0.679878000E+00 TIME STEP NUMBER 706 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.61105E-05 0.23213E-02 Friction velocity uk : 0.61114E-05 0.23213E-02 Dimensionless distance yplus : 0.40695E-04 0.15444E-01 Friction thermal sca. tstar : -0.52165E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.28582E-04 0.10847E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.61105E-05 0.23213E-02 Friction velocity uk : 0.61114E-05 0.23213E-02 Dimensionless distance yplus : 0.40695E-04 0.15444E-01 Friction thermal sca. tstar : -0.52165E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.28582E-04 0.10847E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.35687E-08 3 0.14269E-06 0.24759E-12 0.10075E+01 c Velocity[X] 0.81959E-32 c Velocity[Y] 0.12379E-12 c Velocity[Z] 0.12380E-12 c Pressure 0.94900E-14 15 0.73869E-07 0.73869E-07 0.11289E+01 c k 0.35948E-06 2 0.39706E-07 0.24052E-08 0.14963E+01 c omega 0.13153E+02 1 0.13606E-08 0.27750E+00 0.27425E-02 c TempK 0.94664E+02 1 0.10043E-06 0.22885E-01 0.16752E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.8012e-14 8.1767e-14 -1.0134e-17 -2.6234e-18 v Velocity[Y] -0.00012606 0.00012031 -7.8442e-10 -3.7407e-12 v Velocity[Z] -0.00012029 0.00012606 5.2288e-10 -2.1561e-12 v ǁVelocityǁ 3.1953e-10 0.00013523 1.0835e-05 7.4192e-06 v Pressure -0.0011921 0.021415 0.0012026 6.8833e-20 v k 9.5311e-10 0.0011821 0.00079144 0.0010028 v omega 14.918 1.0313e+05 2666.3 499.72 v TempK 288 342.02 293.88 290.87 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.1178e-14 9.55e-05 5.8303e-05 7.5915e-05 v CourantNb 2.6437e-09 0.00020495 1.3804e-05 8.2401e-06 v FourierNb 0.10217 0.6281 0.18985 0.16079 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.95 4.95 0.00052652 -5.3154e-07 v volume_forces[Z] -4.95 4.95 -0.0005264 6.3374e-07 v ǁvolume_forcesǁ 1.1714e-08 4.9512 0.53307 0.25763 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.09 291.01 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015444 5.4619e-05 3.0559e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.10221 0.6281 0.18987 0.16079 INSTANT 0.680841000E+00 TIME STEP NUMBER 707 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.60344E-05 0.23207E-02 Friction velocity uk : 0.60353E-05 0.23206E-02 Dimensionless distance yplus : 0.40188E-04 0.15440E-01 Friction thermal sca. tstar : -0.65459E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.28226E-04 0.10844E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.60344E-05 0.23207E-02 Friction velocity uk : 0.60353E-05 0.23206E-02 Dimensionless distance yplus : 0.40188E-04 0.15440E-01 Friction thermal sca. tstar : -0.65459E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.28226E-04 0.10844E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.35700E-08 3 0.14227E-06 0.24710E-12 0.10065E+01 c Velocity[X] 0.81595E-32 c Velocity[Y] 0.12355E-12 c Velocity[Z] 0.12355E-12 c Pressure 0.94702E-14 15 0.73714E-07 0.73714E-07 0.11272E+01 c k 0.35897E-06 2 0.39631E-07 0.23928E-08 0.14946E+01 c omega 0.13153E+02 1 0.13567E-08 0.27617E+00 0.27359E-02 c TempK 0.94664E+02 1 0.10023E-06 0.22836E-01 0.16734E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.7947e-14 8.1714e-14 -1.0128e-17 -2.6219e-18 v Velocity[Y] -0.00012602 0.00012026 -7.8241e-10 -3.7345e-12 v Velocity[Z] -0.00012024 0.00012602 5.2063e-10 -2.1564e-12 v ǁVelocityǁ 3.1506e-10 0.00013519 1.0838e-05 7.4254e-06 v Pressure -0.0011938 0.02143 0.0012037 7.9815e-20 v k 9.4956e-10 0.0011806 0.00079023 0.0010013 v omega 14.9 1.0313e+05 2666.3 499.71 v TempK 288 342.03 293.88 290.87 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.1136e-14 9.5488e-05 5.8282e-05 7.5891e-05 v CourantNb 2.6468e-09 0.00020484 1.3803e-05 8.2435e-06 v FourierNb 0.10208 0.6281 0.18981 0.16074 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9501 4.9501 0.00052675 -5.3186e-07 v volume_forces[Z] -4.9501 4.9501 -0.00052662 6.341e-07 v ǁvolume_forcesǁ 1.1551e-08 4.9512 0.53329 0.25781 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.1 291.01 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.01544 5.4603e-05 3.055e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.10212 0.6281 0.18982 0.16075 INSTANT 0.681804000E+00 TIME STEP NUMBER 708 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.59571E-05 0.23201E-02 Friction velocity uk : 0.59580E-05 0.23200E-02 Dimensionless distance yplus : 0.39674E-04 0.15435E-01 Friction thermal sca. tstar : -0.10033E+05 0.00000E+00 Dim-less thermal sca. tplus : 0.27864E-04 0.10841E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.59571E-05 0.23201E-02 Friction velocity uk : 0.59580E-05 0.23200E-02 Dimensionless distance yplus : 0.39674E-04 0.15435E-01 Friction thermal sca. tstar : -0.10033E+05 0.00000E+00 Dim-less thermal sca. tplus : 0.27864E-04 0.10841E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.35712E-08 3 0.14191E-06 0.24662E-12 0.10054E+01 c Velocity[X] 0.81234E-32 c Velocity[Y] 0.12331E-12 c Velocity[Z] 0.12331E-12 c Pressure 0.94496E-14 15 0.73553E-07 0.73553E-07 0.11255E+01 c k 0.35846E-06 2 0.39557E-07 0.23805E-08 0.14928E+01 c omega 0.13153E+02 1 0.13528E-08 0.27484E+00 0.27293E-02 c TempK 0.94665E+02 1 0.10003E-06 0.22788E-01 0.16717E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.7882e-14 8.1661e-14 -1.0121e-17 -2.6204e-18 v Velocity[Y] -0.00012599 0.00012021 -7.804e-10 -3.7284e-12 v Velocity[Z] -0.00012018 0.00012599 5.1837e-10 -2.1567e-12 v ǁVelocityǁ 3.1064e-10 0.00013515 1.0841e-05 7.4315e-06 v Pressure -0.0011955 0.021445 0.0012047 -1.0433e-19 v k 9.4602e-10 0.0011791 0.00078904 0.00099983 v omega 14.883 1.0313e+05 2666.3 499.69 v TempK 288 342.03 293.89 290.87 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.1095e-14 9.5477e-05 5.8262e-05 7.5868e-05 v CourantNb 2.6499e-09 0.00020473 1.3803e-05 8.2469e-06 v FourierNb 0.10199 0.6281 0.18977 0.1607 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9501 4.9502 0.00052698 -5.3218e-07 v volume_forces[Z] -4.9501 4.9502 -0.00052685 6.3445e-07 v ǁvolume_forcesǁ 1.1389e-08 4.9513 0.53352 0.25799 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.1 291.01 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015435 5.4587e-05 3.054e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.10203 0.6281 0.18978 0.16071 INSTANT 0.682767000E+00 TIME STEP NUMBER 709 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.58785E-05 0.23194E-02 Friction velocity uk : 0.58795E-05 0.23194E-02 Dimensionless distance yplus : 0.39151E-04 0.15431E-01 Friction thermal sca. tstar : -0.16997E+05 0.00000E+00 Dim-less thermal sca. tplus : 0.27497E-04 0.10838E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.58785E-05 0.23194E-02 Friction velocity uk : 0.58795E-05 0.23194E-02 Dimensionless distance yplus : 0.39151E-04 0.15431E-01 Friction thermal sca. tstar : -0.16997E+05 0.00000E+00 Dim-less thermal sca. tplus : 0.27497E-04 0.10838E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.35724E-08 3 0.14155E-06 0.24613E-12 0.10044E+01 c Velocity[X] 0.80875E-32 c Velocity[Y] 0.12307E-12 c Velocity[Z] 0.12307E-12 c Pressure 0.94302E-14 15 0.73401E-07 0.73401E-07 0.11239E+01 c k 0.35796E-06 2 0.39483E-07 0.23683E-08 0.14911E+01 c omega 0.13153E+02 1 0.13489E-08 0.27352E+00 0.27227E-02 c TempK 0.94665E+02 1 0.99833E-07 0.22740E-01 0.16699E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.7818e-14 8.1609e-14 -1.0115e-17 -2.6189e-18 v Velocity[Y] -0.00012595 0.00012016 -7.7839e-10 -3.7223e-12 v Velocity[Z] -0.00012013 0.00012596 5.1612e-10 -2.157e-12 v ǁVelocityǁ 3.0627e-10 0.00013511 1.0845e-05 7.4376e-06 v Pressure -0.0011971 0.021459 0.0012058 -2.7455e-21 v k 9.425e-10 0.0011776 0.00078784 0.00099838 v omega 14.865 1.0313e+05 2666.3 499.68 v TempK 288 342.03 293.89 290.87 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.1054e-14 9.5465e-05 5.8242e-05 7.5844e-05 v CourantNb 2.6531e-09 0.00020462 1.3803e-05 8.2503e-06 v FourierNb 0.1019 0.6281 0.18973 0.16066 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9502 4.9502 0.0005272 -5.325e-07 v volume_forces[Z] -4.9502 4.9502 -0.00052707 6.3481e-07 v ǁvolume_forcesǁ 1.123e-08 4.9514 0.53374 0.25818 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.1 291.02 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015431 5.4571e-05 3.0531e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.10195 0.6281 0.18974 0.16067 INSTANT 0.683730000E+00 TIME STEP NUMBER 710 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.43819E-05 0.23188E-02 Friction velocity uk : 0.43830E-05 0.23187E-02 Dimensionless distance yplus : 0.29167E-04 0.15427E-01 Friction thermal sca. tstar : -0.42221E+05 0.00000E+00 Dim-less thermal sca. tplus : 0.20485E-04 0.10835E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.43819E-05 0.23188E-02 Friction velocity uk : 0.43830E-05 0.23187E-02 Dimensionless distance yplus : 0.29167E-04 0.15427E-01 Friction thermal sca. tstar : -0.42221E+05 0.00000E+00 Dim-less thermal sca. tplus : 0.20485E-04 0.10835E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.35737E-08 3 0.14118E-06 0.24565E-12 0.10033E+01 c Velocity[X] 0.80520E-32 c Velocity[Y] 0.12282E-12 c Velocity[Z] 0.12283E-12 c Pressure 0.94021E-14 16 0.73181E-07 0.73181E-07 0.11222E+01 c k 0.35746E-06 2 0.39409E-07 0.23562E-08 0.14894E+01 c omega 0.13153E+02 1 0.13450E-08 0.27221E+00 0.27162E-02 c TempK 0.94666E+02 1 0.99634E-07 0.22692E-01 0.16681E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.7753e-14 8.1557e-14 -1.0109e-17 -2.6174e-18 v Velocity[Y] -0.00012592 0.00012011 -7.7648e-10 -3.8084e-12 v Velocity[Z] -0.00012008 0.00012592 5.1404e-10 -2.0106e-12 v ǁVelocityǁ 3.0186e-10 0.00013507 1.0848e-05 7.4438e-06 v Pressure -0.0011988 0.021474 0.0012068 4.3143e-21 v k 9.39e-10 0.001176 0.00078665 0.00099692 v omega 14.848 1.0313e+05 2666.3 499.66 v TempK 288 342.03 293.89 290.88 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.1012e-14 9.5453e-05 5.8221e-05 7.5821e-05 v CourantNb 2.6574e-09 0.00020452 1.3802e-05 8.2537e-06 v FourierNb 0.10182 0.6281 0.18968 0.16062 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9503 4.9503 0.00052743 -5.3282e-07 v volume_forces[Z] -4.9503 4.9503 -0.0005273 6.3517e-07 v ǁvolume_forcesǁ 1.1072e-08 4.9514 0.53397 0.25836 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.1 291.02 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015427 5.4556e-05 3.0521e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.10186 0.6281 0.1897 0.16063 INSTANT 0.684693000E+00 TIME STEP NUMBER 711 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.57139E-05 0.23181E-02 Friction velocity uk : 0.57149E-05 0.23181E-02 Dimensionless distance yplus : 0.38055E-04 0.15423E-01 Friction thermal sca. tstar : -0.84753E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.26727E-04 0.10832E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.57139E-05 0.23181E-02 Friction velocity uk : 0.57149E-05 0.23181E-02 Dimensionless distance yplus : 0.38055E-04 0.15423E-01 Friction thermal sca. tstar : -0.84753E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.26727E-04 0.10832E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.35749E-08 3 0.14081E-06 0.24517E-12 0.10023E+01 c Velocity[X] 0.80155E-32 c Velocity[Y] 0.12258E-12 c Velocity[Z] 0.12258E-12 c Pressure 0.93846E-14 16 0.73043E-07 0.73043E-07 0.11205E+01 c k 0.35695E-06 2 0.39335E-07 0.23441E-08 0.14877E+01 c omega 0.13153E+02 1 0.13411E-08 0.27091E+00 0.27097E-02 c TempK 0.94667E+02 1 0.99435E-07 0.22644E-01 0.16664E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.7689e-14 8.1504e-14 -1.0103e-17 -2.616e-18 v Velocity[Y] -0.00012588 0.00012006 -7.7444e-10 -3.7973e-12 v Velocity[Z] -0.00012003 0.00012589 5.1178e-10 -2.0067e-12 v ǁVelocityǁ 2.9772e-10 0.00013504 1.0852e-05 7.4499e-06 v Pressure -0.0012005 0.021489 0.0012078 -2.5592e-20 v k 9.3552e-10 0.0011745 0.00078546 0.00099547 v omega 14.831 1.0313e+05 2666.3 499.65 v TempK 288 342.03 293.9 290.88 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.0972e-14 9.5442e-05 5.8201e-05 7.5797e-05 v CourantNb 2.6608e-09 0.00020441 1.3802e-05 8.2571e-06 v FourierNb 0.10173 0.6281 0.18964 0.16058 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9503 4.9503 0.00052765 -5.3314e-07 v volume_forces[Z] -4.9503 4.9503 -0.00052752 6.3553e-07 v ǁvolume_forcesǁ 1.0912e-08 4.9515 0.53419 0.25854 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.11 291.02 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015423 5.4542e-05 3.0513e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.10177 0.6281 0.18966 0.16059 INSTANT 0.685656000E+00 TIME STEP NUMBER 712 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.56328E-05 0.23175E-02 Friction velocity uk : 0.56338E-05 0.23175E-02 Dimensionless distance yplus : 0.37515E-04 0.15418E-01 Friction thermal sca. tstar : -0.60552E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.26348E-04 0.10829E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.56328E-05 0.23175E-02 Friction velocity uk : 0.56338E-05 0.23175E-02 Dimensionless distance yplus : 0.37515E-04 0.15418E-01 Friction thermal sca. tstar : -0.60552E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.26348E-04 0.10829E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.35761E-08 3 0.14047E-06 0.24469E-12 0.10012E+01 c Velocity[X] 0.79805E-32 c Velocity[Y] 0.12234E-12 c Velocity[Z] 0.12234E-12 c Pressure 0.93642E-14 16 0.72884E-07 0.72884E-07 0.11189E+01 c k 0.35645E-06 2 0.39261E-07 0.23321E-08 0.14860E+01 c omega 0.13153E+02 1 0.13373E-08 0.26961E+00 0.27032E-02 c TempK 0.94667E+02 1 0.99237E-07 0.22597E-01 0.16646E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.7625e-14 8.1452e-14 -1.0096e-17 -2.6145e-18 v Velocity[Y] -0.00012585 0.00012001 -7.7242e-10 -3.7935e-12 v Velocity[Z] -0.00011998 0.00012585 5.0951e-10 -2.0097e-12 v ǁVelocityǁ 2.9352e-10 0.000135 1.0855e-05 7.4561e-06 v Pressure -0.0012022 0.021504 0.0012088 1.0472e-19 v k 9.3206e-10 0.001173 0.00078428 0.00099402 v omega 14.813 1.0313e+05 2666.3 499.63 v TempK 288 342.03 293.9 290.88 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.0931e-14 9.543e-05 5.8181e-05 7.5774e-05 v CourantNb 2.6638e-09 0.0002043 1.3802e-05 8.2605e-06 v FourierNb 0.10164 0.6281 0.1896 0.16054 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9504 4.9504 0.00052788 -5.3346e-07 v volume_forces[Z] -4.9504 4.9504 -0.00052775 6.3588e-07 v ǁvolume_forcesǁ 1.0763e-08 4.9515 0.53441 0.25872 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.11 291.02 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015418 5.4527e-05 3.0504e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.10169 0.6281 0.18961 0.16054 INSTANT 0.686619000E+00 TIME STEP NUMBER 713 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.55489E-05 0.23169E-02 Friction velocity uk : 0.55498E-05 0.23168E-02 Dimensionless distance yplus : 0.36956E-04 0.15414E-01 Friction thermal sca. tstar : -0.49617E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.25955E-04 0.10826E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.55489E-05 0.23169E-02 Friction velocity uk : 0.55498E-05 0.23168E-02 Dimensionless distance yplus : 0.36956E-04 0.15414E-01 Friction thermal sca. tstar : -0.49617E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.25955E-04 0.10826E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.35774E-08 3 0.14013E-06 0.24421E-12 0.10002E+01 c Velocity[X] 0.79458E-32 c Velocity[Y] 0.12210E-12 c Velocity[Z] 0.12210E-12 c Pressure 0.93621E-14 16 0.72866E-07 0.72866E-07 0.11173E+01 c k 0.35595E-06 2 0.39188E-07 0.23202E-08 0.14842E+01 c omega 0.13153E+02 1 0.13334E-08 0.26832E+00 0.26967E-02 c TempK 0.94668E+02 1 0.99040E-07 0.22549E-01 0.16628E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.7561e-14 8.14e-14 -1.009e-17 -2.613e-18 v Velocity[Y] -0.00012581 0.00011996 -7.7038e-10 -3.7876e-12 v Velocity[Z] -0.00011993 0.00012582 5.0723e-10 -2.01e-12 v ǁVelocityǁ 2.8939e-10 0.00013496 1.0859e-05 7.4622e-06 v Pressure -0.0012038 0.021519 0.0012099 5.7851e-20 v k 9.2861e-10 0.0011715 0.00078309 0.00099258 v omega 14.796 1.0313e+05 2666.3 499.61 v TempK 288 342.03 293.9 290.88 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.089e-14 9.5419e-05 5.8161e-05 7.5751e-05 v CourantNb 2.6669e-09 0.0002042 1.3801e-05 8.2639e-06 v FourierNb 0.10156 0.6281 0.18956 0.16049 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9504 4.9505 0.0005281 -5.3378e-07 v volume_forces[Z] -4.9504 4.9505 -0.00052797 6.3624e-07 v ǁvolume_forcesǁ 1.0611e-08 4.9516 0.53464 0.2589 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.11 291.02 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015414 5.4513e-05 3.0495e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.1016 0.6281 0.18957 0.1605 INSTANT 0.687582000E+00 TIME STEP NUMBER 714 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.54635E-05 0.23162E-02 Friction velocity uk : 0.54645E-05 0.23162E-02 Dimensionless distance yplus : 0.36387E-04 0.15410E-01 Friction thermal sca. tstar : -0.43049E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.25556E-04 0.10823E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.54635E-05 0.23162E-02 Friction velocity uk : 0.54645E-05 0.23162E-02 Dimensionless distance yplus : 0.36387E-04 0.15410E-01 Friction thermal sca. tstar : -0.43049E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.25556E-04 0.10823E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.35786E-08 3 0.13977E-06 0.24373E-12 0.99910E+00 c Velocity[X] 0.79111E-32 c Velocity[Y] 0.12186E-12 c Velocity[Z] 0.12186E-12 c Pressure 0.93271E-14 16 0.72593E-07 0.72593E-07 0.11156E+01 c k 0.35546E-06 2 0.39115E-07 0.23083E-08 0.14825E+01 c omega 0.13153E+02 1 0.13296E-08 0.26704E+00 0.26903E-02 c TempK 0.94668E+02 1 0.98844E-07 0.22502E-01 0.16611E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.7497e-14 8.1348e-14 -1.0084e-17 -2.6115e-18 v Velocity[Y] -0.00012578 0.00011991 -7.6834e-10 -3.7815e-12 v Velocity[Z] -0.00011988 0.00012578 5.0496e-10 -2.0106e-12 v ǁVelocityǁ 2.8533e-10 0.00013492 1.0862e-05 7.4684e-06 v Pressure -0.0012055 0.021534 0.0012109 -8.7365e-20 v k 9.2518e-10 0.00117 0.00078192 0.00099114 v omega 14.779 1.0313e+05 2666.2 499.6 v TempK 288 342.03 293.9 290.88 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.085e-14 9.5407e-05 5.814e-05 7.5727e-05 v CourantNb 2.67e-09 0.00020409 1.3801e-05 8.2673e-06 v FourierNb 0.10147 0.6281 0.18952 0.16045 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9505 4.9505 0.00052832 -5.341e-07 v volume_forces[Z] -4.9505 4.9505 -0.0005282 6.3659e-07 v ǁvolume_forcesǁ 1.0462e-08 4.9516 0.53486 0.25908 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.11 291.03 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.01541 5.4498e-05 3.0486e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.10151 0.6281 0.18953 0.16046 INSTANT 0.688545000E+00 TIME STEP NUMBER 715 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.53766E-05 0.23156E-02 Friction velocity uk : 0.53776E-05 0.23156E-02 Dimensionless distance yplus : 0.35809E-04 0.15406E-01 Friction thermal sca. tstar : -0.38549E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.25150E-04 0.10820E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.53766E-05 0.23156E-02 Friction velocity uk : 0.53776E-05 0.23156E-02 Dimensionless distance yplus : 0.35809E-04 0.15406E-01 Friction thermal sca. tstar : -0.38549E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.25150E-04 0.10820E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.35799E-08 3 0.16021E-06 0.24325E-12 0.99805E+00 c Velocity[X] 0.78766E-32 c Velocity[Y] 0.12162E-12 c Velocity[Z] 0.12162E-12 c Pressure 0.93151E-14 16 0.72498E-07 0.72498E-07 0.11140E+01 c k 0.35496E-06 2 0.39042E-07 0.22966E-08 0.14808E+01 c omega 0.13153E+02 1 0.13258E-08 0.26577E+00 0.26838E-02 c TempK 0.94669E+02 1 0.98648E-07 0.22455E-01 0.16593E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.7433e-14 8.1296e-14 -1.0078e-17 -2.61e-18 v Velocity[Y] -0.00012575 0.00011986 -7.6629e-10 -3.7755e-12 v Velocity[Z] -0.00011983 0.00012575 5.0268e-10 -2.0111e-12 v ǁVelocityǁ 2.8134e-10 0.00013489 1.0866e-05 7.4745e-06 v Pressure -0.0012072 0.021548 0.0012119 -4.0888e-20 v k 9.2176e-10 0.0011685 0.00078074 0.00098971 v omega 14.762 1.0313e+05 2666.2 499.58 v TempK 288 342.03 293.91 290.89 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.081e-14 9.5396e-05 5.812e-05 7.5704e-05 v CourantNb 2.6732e-09 0.00020398 1.3801e-05 8.2707e-06 v FourierNb 0.10139 0.6281 0.18948 0.16041 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9505 4.9506 0.00052855 -5.3442e-07 v volume_forces[Z] -4.9505 4.9506 -0.00052842 6.3695e-07 v ǁvolume_forcesǁ 1.0315e-08 4.9517 0.53508 0.25926 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.12 291.03 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015406 5.4483e-05 3.0477e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.10143 0.6281 0.18949 0.16042 INSTANT 0.689508000E+00 TIME STEP NUMBER 716 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.52880E-05 0.23150E-02 Friction velocity uk : 0.52890E-05 0.23149E-02 Dimensionless distance yplus : 0.35219E-04 0.15402E-01 Friction thermal sca. tstar : -0.35219E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.24736E-04 0.10817E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.52880E-05 0.23150E-02 Friction velocity uk : 0.52890E-05 0.23149E-02 Dimensionless distance yplus : 0.35219E-04 0.15402E-01 Friction thermal sca. tstar : -0.35219E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.24736E-04 0.10817E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.35811E-08 3 0.13906E-06 0.24277E-12 0.99699E+00 c Velocity[X] 0.78421E-32 c Velocity[Y] 0.12138E-12 c Velocity[Z] 0.12139E-12 c Pressure 0.92899E-14 16 0.72301E-07 0.72301E-07 0.11124E+01 c k 0.35446E-06 2 0.38970E-07 0.22849E-08 0.14791E+01 c omega 0.13153E+02 1 0.13220E-08 0.26450E+00 0.26774E-02 c TempK 0.94669E+02 1 0.98453E-07 0.22408E-01 0.16576E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.7369e-14 8.1245e-14 -1.0072e-17 -2.6086e-18 v Velocity[Y] -0.00012571 0.00011981 -7.6425e-10 -3.7694e-12 v Velocity[Z] -0.00011978 0.00012572 5.004e-10 -2.0116e-12 v ǁVelocityǁ 2.7743e-10 0.00013485 1.0869e-05 7.4806e-06 v Pressure -0.0012088 0.021563 0.001213 -6.8833e-20 v k 9.1837e-10 0.001167 0.00077957 0.00098828 v omega 14.744 1.0313e+05 2666.2 499.57 v TempK 288 342.03 293.91 290.89 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.077e-14 9.5384e-05 5.81e-05 7.5681e-05 v CourantNb 2.6763e-09 0.00020388 1.38e-05 8.2741e-06 v FourierNb 0.1013 0.6281 0.18943 0.16037 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9506 4.9506 0.00052877 -5.3473e-07 v volume_forces[Z] -4.9506 4.9506 -0.00052865 6.373e-07 v ǁvolume_forcesǁ 1.0171e-08 4.9518 0.53531 0.25944 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.12 291.03 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015402 5.4469e-05 3.0468e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.10134 0.6281 0.18945 0.16038 INSTANT 0.690471000E+00 TIME STEP NUMBER 717 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.51977E-05 0.23143E-02 Friction velocity uk : 0.51987E-05 0.23143E-02 Dimensionless distance yplus : 0.34618E-04 0.15397E-01 Friction thermal sca. tstar : -0.32626E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.24313E-04 0.10814E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.51977E-05 0.23143E-02 Friction velocity uk : 0.51987E-05 0.23143E-02 Dimensionless distance yplus : 0.34618E-04 0.15397E-01 Friction thermal sca. tstar : -0.32626E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.24313E-04 0.10814E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.35824E-08 3 0.13871E-06 0.24229E-12 0.99594E+00 c Velocity[X] 0.78079E-32 c Velocity[Y] 0.12115E-12 c Velocity[Z] 0.12115E-12 c Pressure 0.92797E-14 16 0.72220E-07 0.72220E-07 0.11107E+01 c k 0.35397E-06 2 0.38898E-07 0.22732E-08 0.14774E+01 c omega 0.13153E+02 1 0.13182E-08 0.26324E+00 0.26711E-02 c TempK 0.94670E+02 1 0.98258E-07 0.22361E-01 0.16558E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.7306e-14 8.1193e-14 -1.0066e-17 -2.6071e-18 v Velocity[Y] -0.00012568 0.00011976 -7.6219e-10 -3.7634e-12 v Velocity[Z] -0.00011973 0.00012568 4.9812e-10 -2.0122e-12 v ǁVelocityǁ 2.7359e-10 0.00013481 1.0873e-05 7.4868e-06 v Pressure -0.0012105 0.021578 0.001214 9.9033e-21 v k 9.1499e-10 0.0011655 0.0007784 0.00098685 v omega 14.727 1.0313e+05 2666.2 499.55 v TempK 288 342.03 293.91 290.89 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.073e-14 9.5372e-05 5.808e-05 7.5657e-05 v CourantNb 2.6794e-09 0.00020377 1.38e-05 8.2776e-06 v FourierNb 0.10121 0.6281 0.18939 0.16033 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9507 4.9507 0.000529 -5.3505e-07 v volume_forces[Z] -4.9507 4.9507 -0.00052887 6.3765e-07 v ǁvolume_forcesǁ 1.0029e-08 4.9518 0.53553 0.25963 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.12 291.03 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015397 5.4454e-05 3.0459e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.10126 0.6281 0.18941 0.16034 INSTANT 0.691434000E+00 TIME STEP NUMBER 718 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.51055E-05 0.23137E-02 Friction velocity uk : 0.51066E-05 0.23137E-02 Dimensionless distance yplus : 0.34004E-04 0.15393E-01 Friction thermal sca. tstar : -0.30534E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.23882E-04 0.10811E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.51055E-05 0.23137E-02 Friction velocity uk : 0.51066E-05 0.23137E-02 Dimensionless distance yplus : 0.34004E-04 0.15393E-01 Friction thermal sca. tstar : -0.30534E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.23882E-04 0.10811E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.35837E-08 3 0.13836E-06 0.24182E-12 0.99488E+00 c Velocity[X] 0.77738E-32 c Velocity[Y] 0.12091E-12 c Velocity[Z] 0.12091E-12 c Pressure 0.92479E-14 16 0.71972E-07 0.71972E-07 0.11091E+01 c k 0.35348E-06 2 0.38825E-07 0.22617E-08 0.14758E+01 c omega 0.13153E+02 1 0.13144E-08 0.26199E+00 0.26647E-02 c TempK 0.94671E+02 1 0.98064E-07 0.22315E-01 0.16541E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.7243e-14 8.1142e-14 -1.0059e-17 -2.6056e-18 v Velocity[Y] -0.00012565 0.00011971 -7.6013e-10 -3.7575e-12 v Velocity[Z] -0.00011968 0.00012565 4.9583e-10 -2.0126e-12 v ǁVelocityǁ 2.6984e-10 0.00013478 1.0876e-05 7.4929e-06 v Pressure -0.0012122 0.021593 0.001215 -1.3825e-20 v k 9.1162e-10 0.001164 0.00077723 0.00098542 v omega 14.71 1.0313e+05 2666.2 499.54 v TempK 288 342.03 293.91 290.89 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.0691e-14 9.5361e-05 5.806e-05 7.5634e-05 v CourantNb 2.6825e-09 0.00020367 1.38e-05 8.281e-06 v FourierNb 0.10113 0.6281 0.18935 0.16029 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9507 4.9507 0.00052922 -5.3537e-07 v volume_forces[Z] -4.9507 4.9507 -0.00052909 6.38e-07 v ǁvolume_forcesǁ 9.8903e-09 4.9519 0.53575 0.25981 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.12 291.03 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015393 5.4439e-05 3.045e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.10117 0.6281 0.18937 0.1603 INSTANT 0.692397000E+00 TIME STEP NUMBER 719 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.50114E-05 0.23131E-02 Friction velocity uk : 0.50125E-05 0.23130E-02 Dimensionless distance yplus : 0.33378E-04 0.15389E-01 Friction thermal sca. tstar : -0.28799E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.23442E-04 0.10808E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.50114E-05 0.23131E-02 Friction velocity uk : 0.50125E-05 0.23130E-02 Dimensionless distance yplus : 0.33378E-04 0.15389E-01 Friction thermal sca. tstar : -0.28799E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.23442E-04 0.10808E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.35849E-08 3 0.13801E-06 0.24134E-12 0.99383E+00 c Velocity[X] 0.77399E-32 c Velocity[Y] 0.12067E-12 c Velocity[Z] 0.12067E-12 c Pressure 0.92273E-14 16 0.71810E-07 0.71810E-07 0.11075E+01 c k 0.35298E-06 2 0.38754E-07 0.22502E-08 0.14741E+01 c omega 0.13153E+02 1 0.13107E-08 0.26075E+00 0.26584E-02 c TempK 0.94671E+02 1 0.97871E-07 0.22268E-01 0.16524E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.7179e-14 8.109e-14 -1.0053e-17 -2.6042e-18 v Velocity[Y] -0.00012561 0.00011966 -7.5807e-10 -3.7515e-12 v Velocity[Z] -0.00011963 0.00012562 4.9354e-10 -2.0131e-12 v ǁVelocityǁ 2.6618e-10 0.00013474 1.088e-05 7.4991e-06 v Pressure -0.0012139 0.021607 0.001216 1.912e-20 v k 9.0828e-10 0.0011625 0.00077607 0.000984 v omega 14.693 1.0313e+05 2666.2 499.52 v TempK 288 342.03 293.91 290.89 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.0652e-14 9.5349e-05 5.804e-05 7.5611e-05 v CourantNb 2.6856e-09 0.00020356 1.38e-05 8.2844e-06 v FourierNb 0.10105 0.6281 0.18931 0.16025 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9508 4.9508 0.00052944 -5.3568e-07 v volume_forces[Z] -4.9508 4.9508 -0.00052932 6.3835e-07 v ǁvolume_forcesǁ 9.7547e-09 4.9519 0.53597 0.25999 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.13 291.04 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015389 5.4425e-05 3.0442e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.10109 0.6281 0.18932 0.16026 INSTANT 0.693360000E+00 TIME STEP NUMBER 720 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.49153E-05 0.23125E-02 Friction velocity uk : 0.49164E-05 0.23124E-02 Dimensionless distance yplus : 0.32738E-04 0.15385E-01 Friction thermal sca. tstar : -0.27330E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.22993E-04 0.10805E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.49153E-05 0.23125E-02 Friction velocity uk : 0.49164E-05 0.23124E-02 Dimensionless distance yplus : 0.32738E-04 0.15385E-01 Friction thermal sca. tstar : -0.27330E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.22993E-04 0.10805E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.35862E-08 3 0.13766E-06 0.24087E-12 0.99277E+00 c Velocity[X] 0.77062E-32 c Velocity[Y] 0.12043E-12 c Velocity[Z] 0.12043E-12 c Pressure 0.92080E-14 16 0.71659E-07 0.71659E-07 0.11059E+01 c k 0.35249E-06 2 0.38682E-07 0.22388E-08 0.14724E+01 c omega 0.13153E+02 1 0.13069E-08 0.25951E+00 0.26521E-02 c TempK 0.94672E+02 1 0.97678E-07 0.22222E-01 0.16506E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.7116e-14 8.1039e-14 -1.0047e-17 -2.6027e-18 v Velocity[Y] -0.00012558 0.00011961 -7.5601e-10 -3.7455e-12 v Velocity[Z] -0.00011959 0.00012558 4.9124e-10 -2.0136e-12 v ǁVelocityǁ 2.6261e-10 0.0001347 1.0883e-05 7.5052e-06 v Pressure -0.0012155 0.021622 0.0012171 8.4031e-20 v k 9.0495e-10 0.001161 0.00077491 0.00098259 v omega 14.676 1.0313e+05 2666.2 499.51 v TempK 288 342.03 293.92 290.9 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.0613e-14 9.5338e-05 5.802e-05 7.5588e-05 v CourantNb 2.6887e-09 0.00020345 1.3799e-05 8.2878e-06 v FourierNb 0.10096 0.6281 0.18927 0.16021 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9508 4.9509 0.00052966 -5.36e-07 v volume_forces[Z] -4.9508 4.9509 -0.00052954 6.387e-07 v ǁvolume_forcesǁ 9.6223e-09 4.952 0.53619 0.26017 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.13 291.04 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015385 5.441e-05 3.0433e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.101 0.6281 0.18928 0.16021 INSTANT 0.694323000E+00 TIME STEP NUMBER 721 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.48170E-05 0.23118E-02 Friction velocity uk : 0.48181E-05 0.23118E-02 Dimensionless distance yplus : 0.32083E-04 0.15381E-01 Friction thermal sca. tstar : -0.26066E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.22533E-04 0.10802E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.48170E-05 0.23118E-02 Friction velocity uk : 0.48181E-05 0.23118E-02 Dimensionless distance yplus : 0.32083E-04 0.15381E-01 Friction thermal sca. tstar : -0.26066E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.22533E-04 0.10802E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.35874E-08 3 0.13732E-06 0.24039E-12 0.99172E+00 c Velocity[X] 0.76727E-32 c Velocity[Y] 0.12020E-12 c Velocity[Z] 0.12020E-12 c Pressure 0.91902E-14 16 0.71519E-07 0.71519E-07 0.11043E+01 c k 0.35200E-06 2 0.38611E-07 0.22275E-08 0.14707E+01 c omega 0.13153E+02 1 0.13032E-08 0.25828E+00 0.26458E-02 c TempK 0.94672E+02 1 0.97486E-07 0.22176E-01 0.16489E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.7053e-14 8.0988e-14 -1.0041e-17 -2.6012e-18 v Velocity[Y] -0.00012555 0.00011956 -7.5394e-10 -3.7396e-12 v Velocity[Z] -0.00011954 0.00012555 4.8895e-10 -2.0141e-12 v ǁVelocityǁ 2.5914e-10 0.00013467 1.0887e-05 7.5114e-06 v Pressure -0.0012172 0.021637 0.0012181 -4.1672e-20 v k 9.0164e-10 0.0011595 0.00077375 0.00098117 v omega 14.659 1.0313e+05 2666.2 499.49 v TempK 288 342.03 293.92 290.9 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.0574e-14 9.5327e-05 5.8e-05 7.5565e-05 v CourantNb 2.6918e-09 0.00020335 1.3799e-05 8.2912e-06 v FourierNb 0.10088 0.6281 0.18923 0.16017 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9509 4.9509 0.00052989 -5.3631e-07 v volume_forces[Z] -4.9509 4.9509 -0.00052976 6.3905e-07 v ǁvolume_forcesǁ 9.4932e-09 4.952 0.53641 0.26035 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.13 291.04 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015381 5.4395e-05 3.0424e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.10092 0.6281 0.18924 0.16017 INSTANT 0.695286000E+00 TIME STEP NUMBER 722 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.47165E-05 0.23112E-02 Friction velocity uk : 0.47176E-05 0.23112E-02 Dimensionless distance yplus : 0.31414E-04 0.15376E-01 Friction thermal sca. tstar : -0.24963E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.22063E-04 0.10799E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.47165E-05 0.23112E-02 Friction velocity uk : 0.47176E-05 0.23112E-02 Dimensionless distance yplus : 0.31414E-04 0.15376E-01 Friction thermal sca. tstar : -0.24963E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.22063E-04 0.10799E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.35887E-08 3 0.13697E-06 0.23992E-12 0.99066E+00 c Velocity[X] 0.76393E-32 c Velocity[Y] 0.11996E-12 c Velocity[Z] 0.11996E-12 c Pressure 0.91718E-14 16 0.71375E-07 0.71375E-07 0.11027E+01 c k 0.35152E-06 2 0.38539E-07 0.22162E-08 0.14690E+01 c omega 0.13153E+02 1 0.12995E-08 0.25706E+00 0.26395E-02 c TempK 0.94673E+02 1 0.97295E-07 0.22130E-01 0.16472E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.699e-14 8.0937e-14 -1.0035e-17 -2.5998e-18 v Velocity[Y] -0.00012551 0.00011952 -7.5186e-10 -3.7337e-12 v Velocity[Z] -0.00011949 0.00012552 4.8665e-10 -2.0146e-12 v ǁVelocityǁ 2.5577e-10 0.00013463 1.089e-05 7.5175e-06 v Pressure -0.0012189 0.021652 0.0012191 1.2188e-19 v k 8.9834e-10 0.0011581 0.0007726 0.00097976 v omega 14.642 1.0313e+05 2666.1 499.48 v TempK 288 342.03 293.92 290.9 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.0535e-14 9.5315e-05 5.798e-05 7.5542e-05 v CourantNb 2.6948e-09 0.00020324 1.3799e-05 8.2947e-06 v FourierNb 0.10079 0.6281 0.18919 0.16012 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9509 4.951 0.00053011 -5.3663e-07 v volume_forces[Z] -4.9509 4.951 -0.00052998 6.394e-07 v ǁvolume_forcesǁ 9.3678e-09 4.9521 0.53663 0.26053 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.13 291.04 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015376 5.4381e-05 3.0415e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.10083 0.6281 0.1892 0.16013 INSTANT 0.696249000E+00 TIME STEP NUMBER 723 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.46135E-05 0.23106E-02 Friction velocity uk : 0.46146E-05 0.23105E-02 Dimensionless distance yplus : 0.30728E-04 0.15372E-01 Friction thermal sca. tstar : -0.23989E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.21582E-04 0.10797E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.46135E-05 0.23106E-02 Friction velocity uk : 0.46146E-05 0.23105E-02 Dimensionless distance yplus : 0.30728E-04 0.15372E-01 Friction thermal sca. tstar : -0.23989E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.21582E-04 0.10797E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.35900E-08 3 0.13663E-06 0.23945E-12 0.98961E+00 c Velocity[X] 0.76061E-32 c Velocity[Y] 0.11972E-12 c Velocity[Z] 0.11972E-12 c Pressure 0.91529E-14 16 0.71226E-07 0.71226E-07 0.11011E+01 c k 0.35103E-06 2 0.38469E-07 0.22050E-08 0.14674E+01 c omega 0.13153E+02 1 0.12958E-08 0.25584E+00 0.26333E-02 c TempK 0.94673E+02 1 0.97104E-07 0.22084E-01 0.16455E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.6928e-14 8.0886e-14 -1.0029e-17 -2.5983e-18 v Velocity[Y] -0.00012548 0.00011947 -7.4978e-10 -3.7278e-12 v Velocity[Z] -0.00011944 0.00012548 4.8434e-10 -2.015e-12 v ǁVelocityǁ 2.5251e-10 0.0001346 1.0894e-05 7.5237e-06 v Pressure -0.0012205 0.021666 0.0012201 -1.8532e-20 v k 8.9506e-10 0.0011566 0.00077145 0.00097836 v omega 14.625 1.0313e+05 2666.1 499.46 v TempK 288 342.04 293.92 290.9 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.0496e-14 9.5304e-05 5.796e-05 7.5518e-05 v CourantNb 2.6979e-09 0.00020314 1.3799e-05 8.2981e-06 v FourierNb 0.10071 0.6281 0.18915 0.16008 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.951 4.951 0.00053033 -5.3694e-07 v volume_forces[Z] -4.951 4.951 -0.00053021 6.3975e-07 v ǁvolume_forcesǁ 9.246e-09 4.9522 0.53686 0.26071 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.14 291.04 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015372 5.4366e-05 3.0406e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.10075 0.6281 0.18916 0.16009 INSTANT 0.697212000E+00 TIME STEP NUMBER 724 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.45079E-05 0.23100E-02 Friction velocity uk : 0.45090E-05 0.23099E-02 Dimensionless distance yplus : 0.30025E-04 0.15368E-01 Friction thermal sca. tstar : -0.23121E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.21088E-04 0.10794E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.45079E-05 0.23100E-02 Friction velocity uk : 0.45090E-05 0.23099E-02 Dimensionless distance yplus : 0.30025E-04 0.15368E-01 Friction thermal sca. tstar : -0.23121E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.21088E-04 0.10794E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.35913E-08 3 0.13629E-06 0.23898E-12 0.98855E+00 c Velocity[X] 0.75732E-32 c Velocity[Y] 0.11949E-12 c Velocity[Z] 0.11949E-12 c Pressure 0.91329E-14 16 0.71070E-07 0.71070E-07 0.10995E+01 c k 0.35054E-06 2 0.38398E-07 0.21939E-08 0.14657E+01 c omega 0.13153E+02 1 0.12921E-08 0.25464E+00 0.26270E-02 c TempK 0.94674E+02 1 0.96914E-07 0.22039E-01 0.16438E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.6865e-14 8.0835e-14 -1.0023e-17 -2.5969e-18 v Velocity[Y] -0.00012545 0.00011942 -7.477e-10 -3.7219e-12 v Velocity[Z] -0.00011939 0.00012545 4.8204e-10 -2.0154e-12 v ǁVelocityǁ 2.4937e-10 0.00013456 1.0898e-05 7.5298e-06 v Pressure -0.0012222 0.021681 0.0012212 -1.0296e-20 v k 8.9179e-10 0.0011551 0.0007703 0.00097695 v omega 14.609 1.0313e+05 2666.1 499.45 v TempK 288 342.04 293.93 290.9 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.0458e-14 9.5292e-05 5.794e-05 7.5495e-05 v CourantNb 2.701e-09 0.00020304 1.3798e-05 8.3015e-06 v FourierNb 0.10063 0.6281 0.18911 0.16004 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9511 4.9511 0.00053055 -5.3726e-07 v volume_forces[Z] -4.9511 4.9511 -0.00053043 6.401e-07 v ǁvolume_forcesǁ 9.1283e-09 4.9522 0.53708 0.26089 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.14 291.05 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015368 5.4351e-05 3.0397e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.10067 0.6281 0.18912 0.16005 INSTANT 0.698175000E+00 TIME STEP NUMBER 725 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.43995E-05 0.23093E-02 Friction velocity uk : 0.44007E-05 0.23093E-02 Dimensionless distance yplus : 0.29304E-04 0.15364E-01 Friction thermal sca. tstar : -0.22342E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.20581E-04 0.10791E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.43995E-05 0.23093E-02 Friction velocity uk : 0.44007E-05 0.23093E-02 Dimensionless distance yplus : 0.29304E-04 0.15364E-01 Friction thermal sca. tstar : -0.22342E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.20581E-04 0.10791E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.35926E-08 3 0.13595E-06 0.23851E-12 0.98750E+00 c Velocity[X] 0.75403E-32 c Velocity[Y] 0.11925E-12 c Velocity[Z] 0.11925E-12 c Pressure 0.91188E-14 16 0.70959E-07 0.70959E-07 0.10979E+01 c k 0.35006E-06 2 0.38327E-07 0.21828E-08 0.14640E+01 c omega 0.13153E+02 1 0.12885E-08 0.25344E+00 0.26208E-02 c TempK 0.94675E+02 1 0.96725E-07 0.21993E-01 0.16421E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.6802e-14 8.0785e-14 -1.0017e-17 -2.5955e-18 v Velocity[Y] -0.00012541 0.00011937 -7.4561e-10 -3.7161e-12 v Velocity[Z] -0.00011934 0.00012542 4.7973e-10 -2.0159e-12 v ǁVelocityǁ 2.4635e-10 0.00013452 1.0901e-05 7.536e-06 v Pressure -0.0012239 0.021696 0.0012222 1.5983e-20 v k 8.8855e-10 0.0011537 0.00076915 0.00097556 v omega 14.592 1.0313e+05 2666.1 499.43 v TempK 288 342.04 293.93 290.91 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.042e-14 9.5281e-05 5.792e-05 7.5472e-05 v CourantNb 2.7041e-09 0.00020293 1.3798e-05 8.305e-06 v FourierNb 0.10054 0.6281 0.18906 0.16 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9511 4.9511 0.00053078 -5.3757e-07 v volume_forces[Z] -4.9511 4.9511 -0.00053065 6.4044e-07 v ǁvolume_forcesǁ 9.0147e-09 4.9523 0.5373 0.26107 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.14 291.05 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015364 5.4337e-05 3.0388e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.10058 0.6281 0.18908 0.16001 INSTANT 0.699138000E+00 TIME STEP NUMBER 726 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.42881E-05 0.23087E-02 Friction velocity uk : 0.42893E-05 0.23087E-02 Dimensionless distance yplus : 0.28562E-04 0.15360E-01 Friction thermal sca. tstar : -0.21636E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.20060E-04 0.10788E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.42881E-05 0.23087E-02 Friction velocity uk : 0.42893E-05 0.23087E-02 Dimensionless distance yplus : 0.28562E-04 0.15360E-01 Friction thermal sca. tstar : -0.21636E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.20060E-04 0.10788E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.35938E-08 3 0.13561E-06 0.23804E-12 0.98644E+00 c Velocity[X] 0.75077E-32 c Velocity[Y] 0.11902E-12 c Velocity[Z] 0.11902E-12 c Pressure 0.90964E-14 16 0.70784E-07 0.70784E-07 0.10963E+01 c k 0.34958E-06 2 0.38257E-07 0.21718E-08 0.14624E+01 c omega 0.13153E+02 1 0.12848E-08 0.25224E+00 0.26147E-02 c TempK 0.94675E+02 1 0.96536E-07 0.21948E-01 0.16403E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.674e-14 8.0734e-14 -1.0011e-17 -2.594e-18 v Velocity[Y] -0.00012538 0.00011932 -7.4352e-10 -3.7103e-12 v Velocity[Z] -0.00011929 0.00012539 4.7742e-10 -2.0164e-12 v ǁVelocityǁ 2.4345e-10 0.00013449 1.0905e-05 7.5421e-06 v Pressure -0.0012256 0.02171 0.0012232 9.3738e-20 v k 8.8531e-10 0.0011522 0.00076801 0.00097416 v omega 14.575 1.0313e+05 2666.1 499.42 v TempK 288 342.04 293.93 290.91 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.0382e-14 9.5269e-05 5.79e-05 7.5449e-05 v CourantNb 2.7071e-09 0.00020283 1.3798e-05 8.3084e-06 v FourierNb 0.10046 0.6281 0.18902 0.15996 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9512 4.9512 0.000531 -5.3788e-07 v volume_forces[Z] -4.9512 4.9512 -0.00053087 6.4079e-07 v ǁvolume_forcesǁ 8.9054e-09 4.9523 0.53752 0.26125 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.14 291.05 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.01536 5.4322e-05 3.0379e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.1005 0.6281 0.18904 0.15997 INSTANT 0.700101000E+00 TIME STEP NUMBER 727 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.41734E-05 0.23081E-02 Friction velocity uk : 0.41747E-05 0.23080E-02 Dimensionless distance yplus : 0.27799E-04 0.15356E-01 Friction thermal sca. tstar : -0.20994E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.19524E-04 0.10785E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.41734E-05 0.23081E-02 Friction velocity uk : 0.41747E-05 0.23080E-02 Dimensionless distance yplus : 0.27799E-04 0.15356E-01 Friction thermal sca. tstar : -0.20994E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.19524E-04 0.10785E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.35951E-08 3 0.13528E-06 0.23757E-12 0.98539E+00 c Velocity[X] 0.74752E-32 c Velocity[Y] 0.11878E-12 c Velocity[Z] 0.11878E-12 c Pressure 0.90924E-14 16 0.70751E-07 0.70751E-07 0.10947E+01 c k 0.34909E-06 2 0.38187E-07 0.21609E-08 0.14607E+01 c omega 0.13153E+02 1 0.12812E-08 0.25105E+00 0.26085E-02 c TempK 0.94676E+02 1 0.96348E-07 0.21903E-01 0.16386E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.6678e-14 8.0684e-14 -1.0005e-17 -2.5926e-18 v Velocity[Y] -0.00012535 0.00011927 -7.4143e-10 -3.7045e-12 v Velocity[Z] -0.00011925 0.00012535 4.751e-10 -2.0168e-12 v ǁVelocityǁ 2.4069e-10 0.00013445 1.0908e-05 7.5483e-06 v Pressure -0.0012272 0.021725 0.0012242 1.6081e-19 v k 8.821e-10 0.0011507 0.00076687 0.00097277 v omega 14.558 1.0313e+05 2666.1 499.4 v TempK 288 342.04 293.93 290.91 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.0344e-14 9.5258e-05 5.7881e-05 7.5426e-05 v CourantNb 2.7102e-09 0.00020272 1.3798e-05 8.3119e-06 v FourierNb 0.10038 0.6281 0.18898 0.15992 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9512 4.9513 0.00053122 -5.3819e-07 v volume_forces[Z] -4.9512 4.9513 -0.00053109 6.4114e-07 v ǁvolume_forcesǁ 8.8007e-09 4.9524 0.53774 0.26143 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.15 291.05 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015356 5.4307e-05 3.0371e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.10042 0.6281 0.189 0.15993 INSTANT 0.701064000E+00 TIME STEP NUMBER 728 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.40553E-05 0.23075E-02 Friction velocity uk : 0.40566E-05 0.23074E-02 Dimensionless distance yplus : 0.27012E-04 0.15352E-01 Friction thermal sca. tstar : -0.20405E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.18972E-04 0.10782E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.40553E-05 0.23075E-02 Friction velocity uk : 0.40566E-05 0.23074E-02 Dimensionless distance yplus : 0.27012E-04 0.15352E-01 Friction thermal sca. tstar : -0.20405E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.18972E-04 0.10782E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.35964E-08 3 0.13495E-06 0.23710E-12 0.98433E+00 c Velocity[X] 0.74429E-32 c Velocity[Y] 0.11855E-12 c Velocity[Z] 0.11855E-12 c Pressure 0.90610E-14 16 0.70506E-07 0.70506E-07 0.10932E+01 c k 0.34861E-06 2 0.38117E-07 0.21501E-08 0.14591E+01 c omega 0.13153E+02 1 0.12776E-08 0.24988E+00 0.26024E-02 c TempK 0.94676E+02 1 0.96160E-07 0.21858E-01 0.16370E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.6616e-14 8.0633e-14 -9.9988e-18 -2.5911e-18 v Velocity[Y] -0.00012532 0.00011923 -7.3933e-10 -3.6988e-12 v Velocity[Z] -0.0001192 0.00012532 4.7278e-10 -2.0173e-12 v ǁVelocityǁ 2.3806e-10 0.00013442 1.0912e-05 7.5545e-06 v Pressure -0.0012289 0.02174 0.0012252 8.2659e-20 v k 8.789e-10 0.0011493 0.00076574 0.00097138 v omega 14.542 1.0313e+05 2666.1 499.39 v TempK 288 342.04 293.94 290.91 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.0307e-14 9.5247e-05 5.7861e-05 7.5403e-05 v CourantNb 2.7132e-09 0.00020262 1.3798e-05 8.3153e-06 v FourierNb 0.1003 0.6281 0.18894 0.15988 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9513 4.9513 0.00053144 -5.3851e-07 v volume_forces[Z] -4.9513 4.9513 -0.00053131 6.4148e-07 v ǁvolume_forcesǁ 8.7008e-09 4.9524 0.53796 0.26161 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.15 291.05 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015352 5.4293e-05 3.0362e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.10034 0.6281 0.18896 0.15989 INSTANT 0.702027000E+00 TIME STEP NUMBER 729 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.39333E-05 0.23069E-02 Friction velocity uk : 0.39346E-05 0.23068E-02 Dimensionless distance yplus : 0.26200E-04 0.15348E-01 Friction thermal sca. tstar : -0.19864E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.18401E-04 0.10779E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.39333E-05 0.23069E-02 Friction velocity uk : 0.39346E-05 0.23068E-02 Dimensionless distance yplus : 0.26200E-04 0.15348E-01 Friction thermal sca. tstar : -0.19864E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.18401E-04 0.10779E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.35977E-08 3 0.14990E-06 0.23663E-12 0.98328E+00 c Velocity[X] 0.74110E-32 c Velocity[Y] 0.11832E-12 c Velocity[Z] 0.11832E-12 c Pressure 0.90415E-14 16 0.70353E-07 0.70353E-07 0.10916E+01 c k 0.34813E-06 2 0.38047E-07 0.21393E-08 0.14574E+01 c omega 0.13153E+02 1 0.12740E-08 0.24870E+00 0.25963E-02 c TempK 0.94677E+02 1 0.95973E-07 0.21813E-01 0.16353E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.6554e-14 8.0583e-14 -9.9928e-18 -2.5897e-18 v Velocity[Y] -0.00012528 0.00011918 -7.3722e-10 -3.693e-12 v Velocity[Z] -0.00011915 0.00012529 4.7046e-10 -2.0177e-12 v ǁVelocityǁ 2.3558e-10 0.00013438 1.0915e-05 7.5606e-06 v Pressure -0.0012306 0.021754 0.0012262 -1.3316e-19 v k 8.7571e-10 0.0011478 0.0007646 0.00096999 v omega 14.525 1.0313e+05 2666.1 499.37 v TempK 288 342.04 293.94 290.91 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.0269e-14 9.5235e-05 5.7841e-05 7.538e-05 v CourantNb 2.7163e-09 0.00020252 1.3798e-05 8.3188e-06 v FourierNb 0.10021 0.6281 0.1889 0.15984 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9513 4.9514 0.00053166 -5.3882e-07 v volume_forces[Z] -4.9513 4.9514 -0.00053154 6.4183e-07 v ǁvolume_forcesǁ 8.6058e-09 4.9525 0.53818 0.26178 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.15 291.06 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015348 5.4278e-05 3.0353e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.10026 0.6281 0.18892 0.15985 INSTANT 0.702990000E+00 TIME STEP NUMBER 730 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.38071E-05 0.23062E-02 Friction velocity uk : 0.38085E-05 0.23062E-02 Dimensionless distance yplus : 0.25360E-04 0.15343E-01 Friction thermal sca. tstar : -0.19364E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.17811E-04 0.10776E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.38071E-05 0.23062E-02 Friction velocity uk : 0.38085E-05 0.23062E-02 Dimensionless distance yplus : 0.25360E-04 0.15343E-01 Friction thermal sca. tstar : -0.19364E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.17811E-04 0.10776E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.35990E-08 3 0.13427E-06 0.23617E-12 0.98222E+00 c Velocity[X] 0.73791E-32 c Velocity[Y] 0.11808E-12 c Velocity[Z] 0.11808E-12 c Pressure 0.90394E-14 16 0.70336E-07 0.70336E-07 0.10900E+01 c k 0.34765E-06 2 0.37978E-07 0.21285E-08 0.14558E+01 c omega 0.13153E+02 1 0.12704E-08 0.24754E+00 0.25902E-02 c TempK 0.94677E+02 1 0.95787E-07 0.21768E-01 0.16336E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.6492e-14 8.0533e-14 -9.9869e-18 -2.5883e-18 v Velocity[Y] -0.00012525 0.00011913 -7.3511e-10 -3.6872e-12 v Velocity[Z] -0.0001191 0.00012526 4.6814e-10 -2.0181e-12 v ǁVelocityǁ 2.3324e-10 0.00013435 1.0919e-05 7.5668e-06 v Pressure -0.0012322 0.021769 0.0012273 1.2188e-19 v k 8.7254e-10 0.0011464 0.00076347 0.00096861 v omega 14.508 1.0313e+05 2666.1 499.36 v TempK 288 342.04 293.94 290.92 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.0232e-14 9.5224e-05 5.7821e-05 7.5358e-05 v CourantNb 2.7193e-09 0.00020241 1.3797e-05 8.3222e-06 v FourierNb 0.10013 0.6281 0.18886 0.1598 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9514 4.9514 0.00053188 -5.3913e-07 v volume_forces[Z] -4.9514 4.9514 -0.00053176 6.4217e-07 v ǁvolume_forcesǁ 8.5161e-09 4.9525 0.53839 0.26196 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.15 291.06 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015343 5.4264e-05 3.0344e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.10017 0.6281 0.18888 0.15981 INSTANT 0.703953000E+00 TIME STEP NUMBER 731 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.36763E-05 0.23056E-02 Friction velocity uk : 0.36777E-05 0.23056E-02 Dimensionless distance yplus : 0.24489E-04 0.15339E-01 Friction thermal sca. tstar : -0.18899E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.17200E-04 0.10773E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.36763E-05 0.23056E-02 Friction velocity uk : 0.36777E-05 0.23056E-02 Dimensionless distance yplus : 0.24489E-04 0.15339E-01 Friction thermal sca. tstar : -0.18899E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.17200E-04 0.10773E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.36003E-08 3 0.13786E-06 0.23570E-12 0.98117E+00 c Velocity[X] 0.73471E-32 c Velocity[Y] 0.11785E-12 c Velocity[Z] 0.11785E-12 c Pressure 0.90046E-14 16 0.70064E-07 0.70064E-07 0.10885E+01 c k 0.34718E-06 2 0.37909E-07 0.21179E-08 0.14541E+01 c omega 0.13153E+02 1 0.12668E-08 0.24638E+00 0.25841E-02 c TempK 0.94678E+02 1 0.95601E-07 0.21724E-01 0.16319E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.643e-14 8.0483e-14 -9.9809e-18 -2.5869e-18 v Velocity[Y] -0.00012522 0.00011908 -7.33e-10 -3.6815e-12 v Velocity[Z] -0.00011905 0.00012522 4.6581e-10 -2.0186e-12 v ǁVelocityǁ 2.3106e-10 0.00013431 1.0922e-05 7.5729e-06 v Pressure -0.0012339 0.021783 0.0012283 -8.4914e-20 v k 8.6939e-10 0.0011449 0.00076235 0.00096724 v omega 14.492 1.0313e+05 2666 499.35 v TempK 288 342.04 293.94 290.92 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.0195e-14 9.5213e-05 5.7802e-05 7.5335e-05 v CourantNb 2.7224e-09 0.00020231 1.3797e-05 8.3257e-06 v FourierNb 0.10005 0.6281 0.18882 0.15976 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9515 4.9515 0.0005321 -5.3944e-07 v volume_forces[Z] -4.9515 4.9515 -0.00053198 6.4251e-07 v ǁvolume_forcesǁ 8.4317e-09 4.9526 0.53861 0.26214 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.16 291.06 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015339 5.4249e-05 3.0335e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.10009 0.6281 0.18884 0.15977 INSTANT 0.704916000E+00 TIME STEP NUMBER 732 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.35403E-05 0.23050E-02 Friction velocity uk : 0.35418E-05 0.23050E-02 Dimensionless distance yplus : 0.23584E-04 0.15335E-01 Friction thermal sca. tstar : -0.18467E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.16564E-04 0.10771E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.35403E-05 0.23050E-02 Friction velocity uk : 0.35418E-05 0.23050E-02 Dimensionless distance yplus : 0.23584E-04 0.15335E-01 Friction thermal sca. tstar : -0.18467E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.16564E-04 0.10771E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.36016E-08 3 0.14467E-06 0.23524E-12 0.98011E+00 c Velocity[X] 0.73157E-32 c Velocity[Y] 0.11762E-12 c Velocity[Z] 0.11762E-12 c Pressure 0.89964E-14 16 0.69999E-07 0.69999E-07 0.10869E+01 c k 0.34670E-06 2 0.37840E-07 0.21073E-08 0.14525E+01 c omega 0.13153E+02 1 0.12632E-08 0.24522E+00 0.25780E-02 c TempK 0.94679E+02 1 0.95416E-07 0.21679E-01 0.16302E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.6369e-14 8.0433e-14 -9.9749e-18 -2.5854e-18 v Velocity[Y] -0.00012519 0.00011904 -7.3089e-10 -3.6757e-12 v Velocity[Z] -0.00011901 0.00012519 4.6348e-10 -2.019e-12 v ǁVelocityǁ 2.2905e-10 0.00013428 1.0926e-05 7.5791e-06 v Pressure -0.0012356 0.021798 0.0012293 6.0891e-20 v k 8.6625e-10 0.0011435 0.00076122 0.00096586 v omega 14.475 1.0313e+05 2666 499.33 v TempK 288 342.04 293.95 290.92 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.0158e-14 9.5201e-05 5.7782e-05 7.5312e-05 v CourantNb 2.7254e-09 0.00020221 1.3797e-05 8.3292e-06 v FourierNb 0.09997 0.6281 0.18878 0.15972 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9515 4.9515 0.00053232 -5.3975e-07 v volume_forces[Z] -4.9515 4.9515 -0.0005322 6.4286e-07 v ǁvolume_forcesǁ 8.3529e-09 4.9526 0.53883 0.26232 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.16 291.06 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015335 5.4235e-05 3.0327e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.10001 0.6281 0.1888 0.15973 INSTANT 0.705879000E+00 TIME STEP NUMBER 733 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.33986E-05 0.23044E-02 Friction velocity uk : 0.34001E-05 0.23043E-02 Dimensionless distance yplus : 0.22641E-04 0.15331E-01 Friction thermal sca. tstar : -0.18063E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.15901E-04 0.10768E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.33986E-05 0.23044E-02 Friction velocity uk : 0.34001E-05 0.23043E-02 Dimensionless distance yplus : 0.22641E-04 0.15331E-01 Friction thermal sca. tstar : -0.18063E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.15901E-04 0.10768E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.36029E-08 3 0.13326E-06 0.23477E-12 0.97906E+00 c Velocity[X] 0.72843E-32 c Velocity[Y] 0.11738E-12 c Velocity[Z] 0.11739E-12 c Pressure 0.89732E-14 16 0.69817E-07 0.69817E-07 0.10853E+01 c k 0.34623E-06 2 0.37771E-07 0.20968E-08 0.14509E+01 c omega 0.13153E+02 1 0.12597E-08 0.24408E+00 0.25720E-02 c TempK 0.94679E+02 1 0.95232E-07 0.21635E-01 0.16285E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.6307e-14 8.0383e-14 -9.969e-18 -2.584e-18 v Velocity[Y] -0.00012516 0.00011899 -7.2877e-10 -3.67e-12 v Velocity[Z] -0.00011896 0.00012516 4.6115e-10 -2.0194e-12 v ǁVelocityǁ 2.2719e-10 0.00013424 1.093e-05 7.5852e-06 v Pressure -0.0012372 0.021813 0.0012303 3.9319e-20 v k 8.6313e-10 0.001142 0.0007601 0.00096449 v omega 14.459 1.0313e+05 2666 499.32 v TempK 288 342.04 293.95 290.92 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.0122e-14 9.519e-05 5.7762e-05 7.5289e-05 v CourantNb 2.7285e-09 0.0002021 1.3797e-05 8.3326e-06 v FourierNb 0.09989 0.6281 0.18874 0.15968 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9516 4.9516 0.00053254 -5.4005e-07 v volume_forces[Z] -4.9516 4.9516 -0.00053242 6.432e-07 v ǁvolume_forcesǁ 8.28e-09 4.9527 0.53905 0.2625 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.16 291.06 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015331 5.422e-05 3.0318e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.09993 0.6281 0.18875 0.15969 INSTANT 0.706842000E+00 TIME STEP NUMBER 734 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.32503E-05 0.23038E-02 Friction velocity uk : 0.32519E-05 0.23037E-02 Dimensionless distance yplus : 0.21654E-04 0.15327E-01 Friction thermal sca. tstar : -0.17685E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.15208E-04 0.10765E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.32503E-05 0.23038E-02 Friction velocity uk : 0.32519E-05 0.23037E-02 Dimensionless distance yplus : 0.21654E-04 0.15327E-01 Friction thermal sca. tstar : -0.17685E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.15208E-04 0.10765E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.36042E-08 3 0.13294E-06 0.23431E-12 0.97800E+00 c Velocity[X] 0.72529E-32 c Velocity[Y] 0.11715E-12 c Velocity[Z] 0.11715E-12 c Pressure 0.89718E-14 16 0.69806E-07 0.69806E-07 0.10838E+01 c k 0.34575E-06 2 0.37703E-07 0.20863E-08 0.14492E+01 c omega 0.13153E+02 1 0.12561E-08 0.24294E+00 0.25660E-02 c TempK 0.94680E+02 1 0.95048E-07 0.21591E-01 0.16269E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.6246e-14 8.0333e-14 -9.9631e-18 -2.5826e-18 v Velocity[Y] -0.00012512 0.00011894 -7.2664e-10 -3.6643e-12 v Velocity[Z] -0.00011891 0.00012513 4.5881e-10 -2.0198e-12 v ǁVelocityǁ 2.2551e-10 0.00013421 1.0933e-05 7.5914e-06 v Pressure -0.0012389 0.021827 0.0012313 7.9423e-21 v k 8.6002e-10 0.0011406 0.00075898 0.00096312 v omega 14.442 1.0313e+05 2666 499.3 v TempK 288 342.04 293.95 290.92 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.0085e-14 9.5179e-05 5.7743e-05 7.5266e-05 v CourantNb 2.7315e-09 0.000202 1.3797e-05 8.3361e-06 v FourierNb 0.099809 0.6281 0.1887 0.15964 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9516 4.9516 0.00053276 -5.4036e-07 v volume_forces[Z] -4.9516 4.9516 -0.00053264 6.4354e-07 v ǁvolume_forcesǁ 8.2131e-09 4.9528 0.53927 0.26268 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.16 291.07 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015327 5.4206e-05 3.0309e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.09985 0.6281 0.18871 0.15965 INSTANT 0.707805000E+00 TIME STEP NUMBER 735 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.30946E-05 0.23032E-02 Friction velocity uk : 0.30962E-05 0.23031E-02 Dimensionless distance yplus : 0.20618E-04 0.15323E-01 Friction thermal sca. tstar : -0.17329E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.14480E-04 0.10762E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.30946E-05 0.23032E-02 Friction velocity uk : 0.30962E-05 0.23031E-02 Dimensionless distance yplus : 0.20618E-04 0.15323E-01 Friction thermal sca. tstar : -0.17329E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.14480E-04 0.10762E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.36055E-08 3 0.13261E-06 0.23385E-12 0.97695E+00 c Velocity[X] 0.72218E-32 c Velocity[Y] 0.11692E-12 c Velocity[Z] 0.11692E-12 c Pressure 0.89554E-14 16 0.69676E-07 0.69676E-07 0.10823E+01 c k 0.34528E-06 2 0.37634E-07 0.20759E-08 0.14476E+01 c omega 0.13153E+02 1 0.12526E-08 0.24181E+00 0.25600E-02 c TempK 0.94680E+02 1 0.94864E-07 0.21547E-01 0.16252E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.6185e-14 8.0284e-14 -9.9572e-18 -2.5812e-18 v Velocity[Y] -0.00012509 0.00011889 -7.2451e-10 -3.6586e-12 v Velocity[Z] -0.00011886 0.0001251 4.5647e-10 -2.0202e-12 v ǁVelocityǁ 2.2401e-10 0.00013417 1.0937e-05 7.5975e-06 v Pressure -0.0012406 0.021842 0.0012323 4.128e-20 v k 8.5693e-10 0.0011392 0.00075787 0.00096176 v omega 14.426 1.0313e+05 2666 499.29 v TempK 288 342.04 293.95 290.93 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.0049e-14 9.5167e-05 5.7723e-05 7.5243e-05 v CourantNb 2.7345e-09 0.0002019 1.3797e-05 8.3396e-06 v FourierNb 0.099729 0.6281 0.18866 0.1596 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9517 4.9517 0.00053298 -5.4067e-07 v volume_forces[Z] -4.9517 4.9517 -0.00053286 6.4388e-07 v ǁvolume_forcesǁ 8.1524e-09 4.9528 0.53949 0.26286 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.16 291.07 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015323 5.4191e-05 3.03e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.099769 0.6281 0.18867 0.15961 INSTANT 0.708768000E+00 TIME STEP NUMBER 736 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.29302E-05 0.23026E-02 Friction velocity uk : 0.29320E-05 0.23025E-02 Dimensionless distance yplus : 0.19524E-04 0.15319E-01 Friction thermal sca. tstar : -0.16994E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.13712E-04 0.10759E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.29302E-05 0.23026E-02 Friction velocity uk : 0.29320E-05 0.23025E-02 Dimensionless distance yplus : 0.19524E-04 0.15319E-01 Friction thermal sca. tstar : -0.16994E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.13712E-04 0.10759E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.36068E-08 3 0.13227E-06 0.23338E-12 0.97590E+00 c Velocity[X] 0.71908E-32 c Velocity[Y] 0.11669E-12 c Velocity[Z] 0.11669E-12 c Pressure 0.89102E-14 16 0.69324E-07 0.69324E-07 0.10807E+01 c k 0.34481E-06 2 0.37566E-07 0.20656E-08 0.14460E+01 c omega 0.13153E+02 1 0.12491E-08 0.24068E+00 0.25540E-02 c TempK 0.94681E+02 1 0.94682E-07 0.21503E-01 0.16235E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.6123e-14 8.0234e-14 -9.9513e-18 -2.5798e-18 v Velocity[Y] -0.00012506 0.00011885 -7.2238e-10 -3.6529e-12 v Velocity[Z] -0.00011882 0.00012506 4.5413e-10 -2.0206e-12 v ǁVelocityǁ 2.2269e-10 0.00013414 1.094e-05 7.6037e-06 v Pressure -0.0012423 0.021856 0.0012333 3.275e-20 v k 8.5385e-10 0.0011377 0.00075676 0.0009604 v omega 14.409 1.0313e+05 2666 499.27 v TempK 288 342.04 293.96 290.93 v Density 1.205 1.205 1.205 1.205 v TurbVisc 1.0013e-14 9.5156e-05 5.7703e-05 7.5221e-05 v CourantNb 2.7375e-09 0.0002018 1.3797e-05 8.343e-06 v FourierNb 0.099649 0.6281 0.18862 0.15956 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9517 4.9518 0.0005332 -5.4098e-07 v volume_forces[Z] -4.9517 4.9518 -0.00053307 6.4422e-07 v ǁvolume_forcesǁ 8.098e-09 4.9529 0.5397 0.26304 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.17 291.07 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015319 5.4177e-05 3.0292e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.099689 0.6281 0.18863 0.15957 INSTANT 0.709731000E+00 TIME STEP NUMBER 737 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.27557E-05 0.23019E-02 Friction velocity uk : 0.27575E-05 0.23019E-02 Dimensionless distance yplus : 0.18362E-04 0.15315E-01 Friction thermal sca. tstar : -0.16678E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.12896E-04 0.10756E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.27557E-05 0.23019E-02 Friction velocity uk : 0.27575E-05 0.23019E-02 Dimensionless distance yplus : 0.18362E-04 0.15315E-01 Friction thermal sca. tstar : -0.16678E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.12896E-04 0.10756E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.36081E-08 3 0.13194E-06 0.23292E-12 0.97484E+00 c Velocity[X] 0.71602E-32 c Velocity[Y] 0.11646E-12 c Velocity[Z] 0.11646E-12 c Pressure 0.88918E-14 16 0.69180E-07 0.69180E-07 0.10792E+01 c k 0.34434E-06 2 0.37498E-07 0.20553E-08 0.14444E+01 c omega 0.13153E+02 1 0.12456E-08 0.23956E+00 0.25481E-02 c TempK 0.94681E+02 1 0.94500E-07 0.21459E-01 0.16219E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.6062e-14 8.0185e-14 -9.9454e-18 -2.5784e-18 v Velocity[Y] -0.00012503 0.0001188 -7.2024e-10 -3.6472e-12 v Velocity[Z] -0.00011877 0.00012503 4.5179e-10 -2.021e-12 v ǁVelocityǁ 2.2156e-10 0.0001341 1.0944e-05 7.6099e-06 v Pressure -0.0012439 0.021871 0.0012343 7.9227e-20 v k 8.5079e-10 0.0011363 0.00075565 0.00095904 v omega 14.393 1.0313e+05 2666 499.26 v TempK 288 342.04 293.96 290.93 v Density 1.205 1.205 1.205 1.205 v TurbVisc 9.9766e-15 9.5145e-05 5.7684e-05 7.5198e-05 v CourantNb 2.7405e-09 0.0002017 1.3797e-05 8.3465e-06 v FourierNb 0.099569 0.6281 0.18858 0.15952 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9518 4.9518 0.00053342 -5.4128e-07 v volume_forces[Z] -4.9518 4.9518 -0.00053329 6.4456e-07 v ǁvolume_forcesǁ 8.0503e-09 4.9529 0.53992 0.26321 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.17 291.07 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015315 5.4162e-05 3.0283e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.09961 0.6281 0.18859 0.15953 INSTANT 0.710694000E+00 TIME STEP NUMBER 738 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.25689E-05 0.23013E-02 Friction velocity uk : 0.25709E-05 0.23013E-02 Dimensionless distance yplus : 0.17119E-04 0.15311E-01 Friction thermal sca. tstar : -0.16379E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.12023E-04 0.10753E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.25689E-05 0.23013E-02 Friction velocity uk : 0.25709E-05 0.23013E-02 Dimensionless distance yplus : 0.17119E-04 0.15311E-01 Friction thermal sca. tstar : -0.16379E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.12023E-04 0.10753E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.36094E-08 3 0.13161E-06 0.23246E-12 0.97379E+00 c Velocity[X] 0.71296E-32 c Velocity[Y] 0.11623E-12 c Velocity[Z] 0.11623E-12 c Pressure 0.88733E-14 16 0.69035E-07 0.69035E-07 0.10776E+01 c k 0.34387E-06 2 0.37430E-07 0.20451E-08 0.14428E+01 c omega 0.13153E+02 1 0.12421E-08 0.23845E+00 0.25422E-02 c TempK 0.94682E+02 1 0.94318E-07 0.21416E-01 0.16202E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.6002e-14 8.0135e-14 -9.9395e-18 -2.577e-18 v Velocity[Y] -0.000125 0.00011875 -7.181e-10 -3.6415e-12 v Velocity[Z] -0.00011872 0.000125 4.4944e-10 -2.0214e-12 v ǁVelocityǁ 2.2061e-10 0.00013407 1.0948e-05 7.616e-06 v Pressure -0.0012456 0.021885 0.0012354 1.1472e-20 v k 8.4774e-10 0.0011349 0.00075454 0.00095769 v omega 14.377 1.0313e+05 2666 499.24 v TempK 288 342.04 293.96 290.93 v Density 1.205 1.205 1.205 1.205 v TurbVisc 9.9408e-15 9.5133e-05 5.7664e-05 7.5175e-05 v CourantNb 2.7436e-09 0.00020159 1.3797e-05 8.35e-06 v FourierNb 0.09949 0.6281 0.18854 0.15948 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9518 4.9519 0.00053363 -5.4159e-07 v volume_forces[Z] -4.9518 4.9519 -0.00053351 6.449e-07 v ǁvolume_forcesǁ 8.0093e-09 4.953 0.54014 0.26339 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.17 291.07 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015311 5.4148e-05 3.0274e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.09953 0.6281 0.18855 0.15949 INSTANT 0.711657000E+00 TIME STEP NUMBER 739 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.23669E-05 0.23007E-02 Friction velocity uk : 0.23691E-05 0.23007E-02 Dimensionless distance yplus : 0.15775E-04 0.15307E-01 Friction thermal sca. tstar : -0.16095E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.11080E-04 0.10751E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.23669E-05 0.23007E-02 Friction velocity uk : 0.23691E-05 0.23007E-02 Dimensionless distance yplus : 0.15775E-04 0.15307E-01 Friction thermal sca. tstar : -0.16095E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.11080E-04 0.10751E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.36108E-08 3 0.13132E-06 0.23200E-12 0.97273E+00 c Velocity[X] 0.70993E-32 c Velocity[Y] 0.11600E-12 c Velocity[Z] 0.11600E-12 c Pressure 0.88586E-14 16 0.68920E-07 0.68920E-07 0.10761E+01 c k 0.34340E-06 2 0.37363E-07 0.20350E-08 0.14412E+01 c omega 0.13153E+02 1 0.12387E-08 0.23734E+00 0.25363E-02 c TempK 0.94683E+02 1 0.94137E-07 0.21373E-01 0.16186E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.5941e-14 8.0086e-14 -9.9336e-18 -2.5756e-18 v Velocity[Y] -0.00012497 0.00011871 -7.1596e-10 -3.6358e-12 v Velocity[Z] -0.00011868 0.00012497 4.4709e-10 -2.0217e-12 v ǁVelocityǁ 2.1987e-10 0.00013403 1.0951e-05 7.6222e-06 v Pressure -0.0012473 0.0219 0.0012364 2.7455e-21 v k 8.4471e-10 0.0011335 0.00075344 0.00095634 v omega 14.361 1.0313e+05 2665.9 499.23 v TempK 288 342.05 293.96 290.93 v Density 1.205 1.205 1.205 1.205 v TurbVisc 9.9052e-15 9.5122e-05 5.7645e-05 7.5153e-05 v CourantNb 2.7466e-09 0.00020149 1.3796e-05 8.3535e-06 v FourierNb 0.099411 0.6281 0.1885 0.15944 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9519 4.9519 0.00053385 -5.4189e-07 v volume_forces[Z] -4.9519 4.9519 -0.00053373 6.4524e-07 v ǁvolume_forcesǁ 7.9752e-09 4.953 0.54036 0.26357 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.17 291.08 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015307 5.4133e-05 3.0266e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.099451 0.6281 0.18852 0.15945 INSTANT 0.712620000E+00 TIME STEP NUMBER 740 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.21455E-05 0.23001E-02 Friction velocity uk : 0.21479E-05 0.23001E-02 Dimensionless distance yplus : 0.14302E-04 0.15303E-01 Friction thermal sca. tstar : -0.15826E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.10045E-04 0.10748E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.21455E-05 0.23001E-02 Friction velocity uk : 0.21479E-05 0.23001E-02 Dimensionless distance yplus : 0.14302E-04 0.15303E-01 Friction thermal sca. tstar : -0.15826E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.10045E-04 0.10748E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.36121E-08 3 0.13096E-06 0.23155E-12 0.97168E+00 c Velocity[X] 0.70693E-32 c Velocity[Y] 0.11577E-12 c Velocity[Z] 0.11577E-12 c Pressure 0.88377E-14 16 0.68756E-07 0.68756E-07 0.10746E+01 c k 0.34293E-06 2 0.37296E-07 0.20249E-08 0.14396E+01 c omega 0.13153E+02 1 0.12352E-08 0.23624E+00 0.25304E-02 c TempK 0.94683E+02 1 0.93957E-07 0.21329E-01 0.16169E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.588e-14 8.0037e-14 -9.9278e-18 -2.5742e-18 v Velocity[Y] -0.00012494 0.00011866 -7.1381e-10 -3.6302e-12 v Velocity[Z] -0.00011863 0.00012494 4.4474e-10 -2.0221e-12 v ǁVelocityǁ 2.1931e-10 0.000134 1.0955e-05 7.6283e-06 v Pressure -0.0012489 0.021914 0.0012374 -7.9619e-20 v k 8.4169e-10 0.0011321 0.00075234 0.00095499 v omega 14.344 1.0313e+05 2665.9 499.21 v TempK 288 342.05 293.97 290.94 v Density 1.205 1.205 1.205 1.205 v TurbVisc 9.8698e-15 9.5111e-05 5.7625e-05 7.513e-05 v CourantNb 2.7496e-09 0.00020139 1.3796e-05 8.357e-06 v FourierNb 0.099332 0.6281 0.18846 0.1594 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9519 4.952 0.00053407 -5.422e-07 v volume_forces[Z] -4.9519 4.952 -0.00053395 6.4557e-07 v ǁvolume_forcesǁ 7.9481e-09 4.9531 0.54057 0.26375 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.18 291.08 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015303 5.4119e-05 3.0257e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.099372 0.6281 0.18848 0.15941 INSTANT 0.713583000E+00 TIME STEP NUMBER 741 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.18978E-05 0.22995E-02 Friction velocity uk : 0.19005E-05 0.22995E-02 Dimensionless distance yplus : 0.12655E-04 0.15299E-01 Friction thermal sca. tstar : -0.15570E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.88882E-05 0.10745E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.18978E-05 0.22995E-02 Friction velocity uk : 0.19005E-05 0.22995E-02 Dimensionless distance yplus : 0.12655E-04 0.15299E-01 Friction thermal sca. tstar : -0.15570E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.88882E-05 0.10745E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.36134E-08 3 0.13064E-06 0.23109E-12 0.97063E+00 c Velocity[X] 0.70390E-32 c Velocity[Y] 0.11554E-12 c Velocity[Z] 0.11555E-12 c Pressure 0.88305E-14 16 0.68698E-07 0.68698E-07 0.10731E+01 c k 0.34247E-06 2 0.37229E-07 0.20149E-08 0.14380E+01 c omega 0.13153E+02 1 0.12318E-08 0.23515E+00 0.25245E-02 c TempK 0.94684E+02 1 0.93777E-07 0.21286E-01 0.16153E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.582e-14 7.9988e-14 -9.9219e-18 -2.5728e-18 v Velocity[Y] -0.0001249 0.00011863 -7.1166e-10 -3.6245e-12 v Velocity[Z] -0.00011859 0.00012491 4.4238e-10 -2.0225e-12 v ǁVelocityǁ 2.1896e-10 0.00013397 1.0958e-05 7.6345e-06 v Pressure -0.0012506 0.021929 0.0012384 -4.5497e-20 v k 8.3868e-10 0.0011307 0.00075124 0.00095365 v omega 14.328 1.0313e+05 2665.9 499.2 v TempK 288 342.05 293.97 290.94 v Density 1.205 1.205 1.205 1.205 v TurbVisc 9.8345e-15 9.51e-05 5.7606e-05 7.5107e-05 v CourantNb 2.7526e-09 0.00020129 1.3796e-05 8.3604e-06 v FourierNb 0.099253 0.6281 0.18842 0.15936 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.952 4.952 0.00053429 -5.425e-07 v volume_forces[Z] -4.952 4.952 -0.00053417 6.4591e-07 v ǁvolume_forcesǁ 7.9282e-09 4.9531 0.54079 0.26392 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.18 291.08 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015299 5.4105e-05 3.0248e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.099294 0.6281 0.18844 0.15937 INSTANT 0.714546000E+00 TIME STEP NUMBER 742 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.16119E-05 0.22989E-02 Friction velocity uk : 0.16150E-05 0.22989E-02 Dimensionless distance yplus : 0.10754E-04 0.15295E-01 Friction thermal sca. tstar : -0.15326E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.75531E-05 0.10742E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.16119E-05 0.22989E-02 Friction velocity uk : 0.16150E-05 0.22989E-02 Dimensionless distance yplus : 0.10754E-04 0.15295E-01 Friction thermal sca. tstar : -0.15326E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.75531E-05 0.10742E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.36147E-08 3 0.13032E-06 0.23063E-12 0.96957E+00 c Velocity[X] 0.70090E-32 c Velocity[Y] 0.11532E-12 c Velocity[Z] 0.11532E-12 c Pressure 0.88022E-14 16 0.68477E-07 0.68477E-07 0.10716E+01 c k 0.34200E-06 2 0.37162E-07 0.20049E-08 0.14364E+01 c omega 0.13153E+02 1 0.12283E-08 0.23406E+00 0.25187E-02 c TempK 0.94684E+02 1 0.93598E-07 0.21243E-01 0.16136E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.5759e-14 7.9939e-14 -9.9161e-18 -2.5714e-18 v Velocity[Y] -0.00012487 0.00011859 -7.0951e-10 -3.6189e-12 v Velocity[Z] -0.00011855 0.00012488 4.4003e-10 -2.0229e-12 v ǁVelocityǁ 2.1882e-10 0.00013393 1.0962e-05 7.6406e-06 v Pressure -0.0012523 0.021943 0.0012394 4.3241e-20 v k 8.3569e-10 0.0011292 0.00075014 0.00095231 v omega 14.312 1.0313e+05 2665.9 499.19 v TempK 288 342.05 293.97 290.94 v Density 1.205 1.205 1.205 1.205 v TurbVisc 9.7994e-15 9.5089e-05 5.7586e-05 7.5085e-05 v CourantNb 2.7556e-09 0.00020119 1.3796e-05 8.3639e-06 v FourierNb 0.099175 0.6281 0.18838 0.15932 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9521 4.9521 0.00053451 -5.4281e-07 v volume_forces[Z] -4.9521 4.9521 -0.00053438 6.4625e-07 v ǁvolume_forcesǁ 7.9156e-09 4.9532 0.541 0.2641 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.18 291.08 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015295 5.409e-05 3.0239e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.099215 0.6281 0.1884 0.15933 INSTANT 0.715509000E+00 TIME STEP NUMBER 743 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12619E-05 0.22983E-02 Friction velocity uk : 0.12659E-05 0.22983E-02 Dimensionless distance yplus : 0.84293E-05 0.15291E-01 Friction thermal sca. tstar : -0.15093E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.59202E-05 0.10739E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12619E-05 0.22983E-02 Friction velocity uk : 0.12659E-05 0.22983E-02 Dimensionless distance yplus : 0.84293E-05 0.15291E-01 Friction thermal sca. tstar : -0.15093E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.59202E-05 0.10739E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.36161E-08 3 0.12999E-06 0.23018E-12 0.96852E+00 c Velocity[X] 0.69793E-32 c Velocity[Y] 0.11509E-12 c Velocity[Z] 0.11509E-12 c Pressure 0.87845E-14 16 0.68338E-07 0.68338E-07 0.10701E+01 c k 0.34154E-06 2 0.37095E-07 0.19950E-08 0.14348E+01 c omega 0.13153E+02 1 0.12249E-08 0.23298E+00 0.25128E-02 c TempK 0.94685E+02 1 0.93419E-07 0.21201E-01 0.16120E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.5699e-14 7.989e-14 -9.9103e-18 -2.57e-18 v Velocity[Y] -0.00012484 0.00011855 -7.0735e-10 -3.6133e-12 v Velocity[Z] -0.00011851 0.00012485 4.3767e-10 -2.0232e-12 v ǁVelocityǁ 2.1888e-10 0.0001339 1.0966e-05 7.6468e-06 v Pressure -0.0012539 0.021958 0.0012404 1.6571e-20 v k 8.3272e-10 0.0011278 0.00074905 0.00095097 v omega 14.296 1.0313e+05 2665.9 499.17 v TempK 288 342.05 293.97 290.94 v Density 1.205 1.205 1.205 1.205 v TurbVisc 9.7645e-15 9.5077e-05 5.7567e-05 7.5062e-05 v CourantNb 2.7586e-09 0.00020109 1.3796e-05 8.3674e-06 v FourierNb 0.099096 0.6281 0.18834 0.15928 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9521 4.9521 0.00053472 -5.4311e-07 v volume_forces[Z] -4.9521 4.9521 -0.0005346 6.4658e-07 v ǁvolume_forcesǁ 7.9103e-09 4.9532 0.54122 0.26428 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.18 291.08 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015291 5.4076e-05 3.0231e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.099137 0.6281 0.18836 0.15929 INSTANT 0.716472000E+00 TIME STEP NUMBER 744 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.76442E-06 0.22977E-02 Friction velocity uk : 0.77095E-06 0.22977E-02 Dimensionless distance yplus : 0.51337E-05 0.15287E-01 Friction thermal sca. tstar : -0.14870E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.36056E-05 0.10736E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.76442E-06 0.22977E-02 Friction velocity uk : 0.77095E-06 0.22977E-02 Dimensionless distance yplus : 0.51337E-05 0.15287E-01 Friction thermal sca. tstar : -0.14870E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.36056E-05 0.10736E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.36174E-08 3 0.12967E-06 0.22972E-12 0.96747E+00 c Velocity[X] 0.69498E-32 c Velocity[Y] 0.11486E-12 c Velocity[Z] 0.11486E-12 c Pressure 0.87664E-14 16 0.68197E-07 0.68197E-07 0.10685E+01 c k 0.34108E-06 2 0.37029E-07 0.19852E-08 0.14332E+01 c omega 0.13153E+02 1 0.12215E-08 0.23190E+00 0.25070E-02 c TempK 0.94685E+02 1 0.93241E-07 0.21158E-01 0.16103E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.5639e-14 7.9842e-14 -9.9045e-18 -2.5686e-18 v Velocity[Y] -0.00012481 0.00011852 -7.0519e-10 -3.6077e-12 v Velocity[Z] -0.00011848 0.00012482 4.353e-10 -2.0235e-12 v ǁVelocityǁ 2.1914e-10 0.00013386 1.0969e-05 7.6529e-06 v Pressure -0.0012556 0.021972 0.0012414 -1.0903e-19 v k 8.2976e-10 0.0011264 0.00074796 0.00094964 v omega 14.28 1.0313e+05 2665.9 499.16 v TempK 288 342.05 293.98 290.94 v Density 1.205 1.205 1.205 1.205 v TurbVisc 9.7297e-15 9.5066e-05 5.7548e-05 7.504e-05 v CourantNb 2.7616e-09 0.00020099 1.3796e-05 8.3709e-06 v FourierNb 0.099019 0.6281 0.1883 0.15924 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9522 4.9522 0.00053494 -5.4341e-07 v volume_forces[Z] -4.9522 4.9522 -0.00053482 6.4692e-07 v ǁvolume_forcesǁ 7.9123e-09 4.9533 0.54144 0.26446 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.19 291.09 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015287 5.4062e-05 3.0222e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.099059 0.6281 0.18832 0.15925 INSTANT 0.717435000E+00 TIME STEP NUMBER 745 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.64498E-06 0.22971E-02 Friction velocity uk : 0.65266E-06 0.22971E-02 Dimensionless distance yplus : 0.43460E-05 0.15283E-01 Friction thermal sca. tstar : -0.14657E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.30523E-05 0.10734E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.64498E-06 0.22971E-02 Friction velocity uk : 0.65266E-06 0.22971E-02 Dimensionless distance yplus : 0.43460E-05 0.15283E-01 Friction thermal sca. tstar : -0.14657E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.30523E-05 0.10734E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.36187E-08 3 0.12935E-06 0.22927E-12 0.96641E+00 c Velocity[X] 0.69204E-32 c Velocity[Y] 0.11463E-12 c Velocity[Z] 0.11463E-12 c Pressure 0.87487E-14 16 0.68059E-07 0.68059E-07 0.10670E+01 c k 0.34062E-06 2 0.36962E-07 0.19754E-08 0.14316E+01 c omega 0.13153E+02 1 0.12181E-08 0.23083E+00 0.25012E-02 c TempK 0.94686E+02 1 0.93064E-07 0.21115E-01 0.16087E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.5579e-14 7.9793e-14 -9.8987e-18 -2.5673e-18 v Velocity[Y] -0.00012478 0.00011848 -7.0302e-10 -3.6021e-12 v Velocity[Z] -0.00011844 0.00012479 4.3294e-10 -2.0239e-12 v ǁVelocityǁ 2.1961e-10 0.00013383 1.0973e-05 7.6591e-06 v Pressure -0.0012573 0.021987 0.0012424 -1.0658e-19 v k 8.2681e-10 0.001125 0.00074687 0.00094831 v omega 14.264 1.0313e+05 2665.9 499.14 v TempK 288 342.05 293.98 290.95 v Density 1.205 1.205 1.205 1.205 v TurbVisc 9.6951e-15 9.5055e-05 5.7528e-05 7.5017e-05 v CourantNb 2.7645e-09 0.00020089 1.3796e-05 8.3744e-06 v FourierNb 0.098941 0.6281 0.18826 0.1592 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9522 4.9522 0.00053516 -5.4372e-07 v volume_forces[Z] -4.9522 4.9522 -0.00053504 6.4725e-07 v ǁvolume_forcesǁ 7.9219e-09 4.9534 0.54165 0.26463 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.19 291.09 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015283 5.4047e-05 3.0214e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.098981 0.6281 0.18828 0.15921 INSTANT 0.718398000E+00 TIME STEP NUMBER 746 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11952E-05 0.22965E-02 Friction velocity uk : 0.11993E-05 0.22965E-02 Dimensionless distance yplus : 0.79863E-05 0.15279E-01 Friction thermal sca. tstar : -0.14453E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.56091E-05 0.10731E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11952E-05 0.22965E-02 Friction velocity uk : 0.11993E-05 0.22965E-02 Dimensionless distance yplus : 0.79863E-05 0.15279E-01 Friction thermal sca. tstar : -0.14453E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.56091E-05 0.10731E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.36201E-08 3 0.16869E-06 0.22881E-12 0.96536E+00 c Velocity[X] 0.68911E-32 c Velocity[Y] 0.11441E-12 c Velocity[Z] 0.11441E-12 c Pressure 0.87547E-14 16 0.68104E-07 0.68104E-07 0.10655E+01 c k 0.34016E-06 2 0.36896E-07 0.19657E-08 0.14300E+01 c omega 0.13153E+02 1 0.12147E-08 0.22977E+00 0.24955E-02 c TempK 0.94686E+02 1 0.92887E-07 0.21073E-01 0.16071E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.5519e-14 7.9744e-14 -9.8929e-18 -2.5659e-18 v Velocity[Y] -0.00012475 0.00011845 -7.0085e-10 -3.5965e-12 v Velocity[Z] -0.00011841 0.00012476 4.3057e-10 -2.0242e-12 v ǁVelocityǁ 2.2029e-10 0.0001338 1.0977e-05 7.6652e-06 v Pressure -0.0012589 0.022001 0.0012434 -2.2062e-20 v k 8.2388e-10 0.0011236 0.00074579 0.00094698 v omega 14.248 1.0313e+05 2665.9 499.13 v TempK 288 342.05 293.98 290.95 v Density 1.205 1.205 1.205 1.205 v TurbVisc 9.6607e-15 9.5044e-05 5.7509e-05 7.4995e-05 v CourantNb 2.7675e-09 0.00020079 1.3796e-05 8.3779e-06 v FourierNb 0.098864 0.6281 0.18822 0.15916 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9523 4.9523 0.00053537 -5.4402e-07 v volume_forces[Z] -4.9523 4.9523 -0.00053525 6.4759e-07 v ǁvolume_forcesǁ 7.9389e-09 4.9534 0.54187 0.26481 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.19 291.09 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015279 5.4033e-05 3.0205e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.098904 0.6281 0.18824 0.15917 INSTANT 0.719361000E+00 TIME STEP NUMBER 747 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15631E-05 0.22959E-02 Friction velocity uk : 0.15662E-05 0.22959E-02 Dimensionless distance yplus : 0.10429E-04 0.15275E-01 Friction thermal sca. tstar : -0.14257E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.73250E-05 0.10728E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15631E-05 0.22959E-02 Friction velocity uk : 0.15662E-05 0.22959E-02 Dimensionless distance yplus : 0.10429E-04 0.15275E-01 Friction thermal sca. tstar : -0.14257E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.73250E-05 0.10728E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.36214E-08 3 0.12873E-06 0.22836E-12 0.96431E+00 c Velocity[X] 0.68620E-32 c Velocity[Y] 0.11418E-12 c Velocity[Z] 0.11418E-12 c Pressure 0.87301E-14 16 0.67911E-07 0.67911E-07 0.10640E+01 c k 0.33970E-06 2 0.36830E-07 0.19561E-08 0.14284E+01 c omega 0.13153E+02 1 0.12114E-08 0.22871E+00 0.24897E-02 c TempK 0.94687E+02 1 0.92710E-07 0.21031E-01 0.16055E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.5459e-14 7.9696e-14 -9.8872e-18 -2.5645e-18 v Velocity[Y] -0.00012472 0.00011841 -6.9868e-10 -3.591e-12 v Velocity[Z] -0.00011837 0.00012473 4.282e-10 -2.0246e-12 v ǁVelocityǁ 2.2117e-10 0.00013376 1.098e-05 7.6714e-06 v Pressure -0.0012606 0.022016 0.0012444 1.7826e-19 v k 8.2096e-10 0.0011223 0.00074471 0.00094565 v omega 14.232 1.0313e+05 2665.9 499.12 v TempK 288 342.05 293.98 290.95 v Density 1.205 1.205 1.205 1.205 v TurbVisc 9.6264e-15 9.5033e-05 5.749e-05 7.4972e-05 v CourantNb 2.7705e-09 0.00020069 1.3796e-05 8.3814e-06 v FourierNb 0.098787 0.6281 0.18819 0.15912 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9523 4.9523 0.00053559 -5.4432e-07 v volume_forces[Z] -4.9523 4.9523 -0.00053547 6.4792e-07 v ǁvolume_forcesǁ 7.9633e-09 4.9535 0.54208 0.26499 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.19 291.09 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015275 5.4019e-05 3.0196e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.098827 0.6281 0.1882 0.15913 INSTANT 0.720324000E+00 TIME STEP NUMBER 748 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.18602E-05 0.22953E-02 Friction velocity uk : 0.18628E-05 0.22953E-02 Dimensionless distance yplus : 0.12404E-04 0.15271E-01 Friction thermal sca. tstar : -0.14069E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.87119E-05 0.10725E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.18602E-05 0.22953E-02 Friction velocity uk : 0.18628E-05 0.22953E-02 Dimensionless distance yplus : 0.12404E-04 0.15271E-01 Friction thermal sca. tstar : -0.14069E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.87119E-05 0.10725E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.36227E-08 3 0.12841E-06 0.22791E-12 0.96326E+00 c Velocity[X] 0.68331E-32 c Velocity[Y] 0.11395E-12 c Velocity[Z] 0.11395E-12 c Pressure 0.86997E-14 16 0.67674E-07 0.67674E-07 0.10626E+01 c k 0.33924E-06 2 0.36765E-07 0.19465E-08 0.14268E+01 c omega 0.13153E+02 1 0.12080E-08 0.22766E+00 0.24840E-02 c TempK 0.94688E+02 1 0.92535E-07 0.20989E-01 0.16039E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.54e-14 7.9648e-14 -9.8814e-18 -2.5631e-18 v Velocity[Y] -0.00012469 0.00011837 -6.965e-10 -3.5854e-12 v Velocity[Z] -0.00011833 0.00012469 4.2582e-10 -2.0249e-12 v ǁVelocityǁ 2.2226e-10 0.00013373 1.0984e-05 7.6775e-06 v Pressure -0.0012623 0.02203 0.0012454 -6.4127e-20 v k 8.1806e-10 0.0011209 0.00074363 0.00094433 v omega 14.216 1.0313e+05 2665.8 499.1 v TempK 288 342.05 293.99 290.95 v Density 1.205 1.205 1.205 1.205 v TurbVisc 9.5923e-15 9.5022e-05 5.747e-05 7.495e-05 v CourantNb 2.7735e-09 0.00020059 1.3796e-05 8.3849e-06 v FourierNb 0.09871 0.6281 0.18815 0.15908 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9524 4.9524 0.00053581 -5.4462e-07 v volume_forces[Z] -4.9524 4.9524 -0.00053569 6.4826e-07 v ǁvolume_forcesǁ 7.9953e-09 4.9535 0.5423 0.26516 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.2 291.09 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015271 5.4005e-05 3.0188e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.098745 0.6281 0.18816 0.15909 INSTANT 0.721287000E+00 TIME STEP NUMBER 749 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.21165E-05 0.22947E-02 Friction velocity uk : 0.21188E-05 0.22947E-02 Dimensionless distance yplus : 0.14109E-04 0.15267E-01 Friction thermal sca. tstar : -0.13888E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.99089E-05 0.10722E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.21165E-05 0.22947E-02 Friction velocity uk : 0.21188E-05 0.22947E-02 Dimensionless distance yplus : 0.14109E-04 0.15267E-01 Friction thermal sca. tstar : -0.13888E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.99089E-05 0.10722E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.36241E-08 3 0.12809E-06 0.22746E-12 0.96220E+00 c Velocity[X] 0.68044E-32 c Velocity[Y] 0.11373E-12 c Velocity[Z] 0.11373E-12 c Pressure 0.86806E-14 16 0.67524E-07 0.67524E-07 0.10611E+01 c k 0.33878E-06 2 0.36699E-07 0.19369E-08 0.14253E+01 c omega 0.13153E+02 1 0.12047E-08 0.22661E+00 0.24783E-02 c TempK 0.94688E+02 1 0.92359E-07 0.20947E-01 0.16022E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.534e-14 7.96e-14 -9.8757e-18 -2.5618e-18 v Velocity[Y] -0.00012466 0.00011834 -6.9432e-10 -3.5799e-12 v Velocity[Z] -0.0001183 0.00012466 4.2345e-10 -2.0253e-12 v ǁVelocityǁ 2.2355e-10 0.0001337 1.0987e-05 7.6837e-06 v Pressure -0.001264 0.022045 0.0012464 -4.1476e-20 v k 8.1517e-10 0.0011195 0.00074256 0.00094302 v omega 14.2 1.0313e+05 2665.8 499.09 v TempK 288 342.05 293.99 290.95 v Density 1.205 1.205 1.205 1.205 v TurbVisc 9.5584e-15 9.501e-05 5.7451e-05 7.4927e-05 v CourantNb 2.7764e-09 0.00020049 1.3796e-05 8.3883e-06 v FourierNb 0.098633 0.6281 0.18811 0.15904 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9524 4.9525 0.00053602 -5.4492e-07 v volume_forces[Z] -4.9524 4.9525 -0.0005359 6.4859e-07 v ǁvolume_forcesǁ 8.0346e-09 4.9536 0.54251 0.26534 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.2 291.1 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015267 5.3991e-05 3.0179e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.098653 0.6281 0.18812 0.15905 INSTANT 0.722250000E+00 TIME STEP NUMBER 750 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.23454E-05 0.22941E-02 Friction velocity uk : 0.23474E-05 0.22941E-02 Dimensionless distance yplus : 0.15631E-04 0.15263E-01 Friction thermal sca. tstar : -0.13713E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.10978E-04 0.10720E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.23454E-05 0.22941E-02 Friction velocity uk : 0.23474E-05 0.22941E-02 Dimensionless distance yplus : 0.15631E-04 0.15263E-01 Friction thermal sca. tstar : -0.13713E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.10978E-04 0.10720E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.36254E-08 3 0.12778E-06 0.22700E-12 0.96115E+00 c Velocity[X] 0.67758E-32 c Velocity[Y] 0.11350E-12 c Velocity[Z] 0.11350E-12 c Pressure 0.86617E-14 16 0.67376E-07 0.67376E-07 0.10596E+01 c k 0.33833E-06 2 0.36634E-07 0.19274E-08 0.14237E+01 c omega 0.13153E+02 1 0.12013E-08 0.22557E+00 0.24726E-02 c TempK 0.94689E+02 1 0.92185E-07 0.20905E-01 0.16006E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.5281e-14 7.9552e-14 -9.8699e-18 -2.5604e-18 v Velocity[Y] -0.00012463 0.0001183 -6.9213e-10 -3.5744e-12 v Velocity[Z] -0.00011826 0.00012463 4.2107e-10 -2.0256e-12 v ǁVelocityǁ 2.2504e-10 0.00013366 1.0991e-05 7.6898e-06 v Pressure -0.0012656 0.022059 0.0012474 -5.7655e-20 v k 8.1229e-10 0.0011181 0.00074148 0.0009417 v omega 14.184 1.0313e+05 2665.8 499.07 v TempK 288 342.05 293.99 290.96 v Density 1.205 1.205 1.205 1.205 v TurbVisc 9.5246e-15 9.4999e-05 5.7432e-05 7.4905e-05 v CourantNb 2.7794e-09 0.00020039 1.3796e-05 8.3918e-06 v FourierNb 0.098541 0.6281 0.18807 0.159 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9525 4.9525 0.00053624 -5.4522e-07 v volume_forces[Z] -4.9525 4.9525 -0.00053612 6.4892e-07 v ǁvolume_forcesǁ 8.0813e-09 4.9536 0.54273 0.26552 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.2 291.1 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015263 5.3976e-05 3.0171e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.098561 0.6281 0.18808 0.15901 INSTANT 0.723213000E+00 TIME STEP NUMBER 751 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.25543E-05 0.22935E-02 Friction velocity uk : 0.25562E-05 0.22935E-02 Dimensionless distance yplus : 0.17021E-04 0.15259E-01 Friction thermal sca. tstar : -0.13546E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.11955E-04 0.10717E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.25543E-05 0.22935E-02 Friction velocity uk : 0.25562E-05 0.22935E-02 Dimensionless distance yplus : 0.17021E-04 0.15259E-01 Friction thermal sca. tstar : -0.13546E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.11955E-04 0.10717E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.36268E-08 3 0.12747E-06 0.22655E-12 0.96010E+00 c Velocity[X] 0.67473E-32 c Velocity[Y] 0.11328E-12 c Velocity[Z] 0.11328E-12 c Pressure 0.86553E-14 16 0.67326E-07 0.67326E-07 0.10581E+01 c k 0.33787E-06 2 0.36569E-07 0.19180E-08 0.14221E+01 c omega 0.13153E+02 1 0.11980E-08 0.22454E+00 0.24669E-02 c TempK 0.94689E+02 1 0.92011E-07 0.20863E-01 0.15990E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.5221e-14 7.9504e-14 -9.8642e-18 -2.5591e-18 v Velocity[Y] -0.0001246 0.00011827 -6.8995e-10 -3.5689e-12 v Velocity[Z] -0.00011823 0.0001246 4.1869e-10 -2.0259e-12 v ǁVelocityǁ 2.2673e-10 0.00013363 1.0995e-05 7.696e-06 v Pressure -0.0012673 0.022073 0.0012484 4.8536e-20 v k 8.0943e-10 0.0011167 0.00074041 0.00094039 v omega 14.168 1.0313e+05 2665.8 499.06 v TempK 288 342.05 293.99 290.96 v Density 1.205 1.205 1.205 1.205 v TurbVisc 9.491e-15 9.4988e-05 5.7413e-05 7.4883e-05 v CourantNb 2.7824e-09 0.00020029 1.3796e-05 8.3953e-06 v FourierNb 0.09845 0.6281 0.18803 0.15896 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9525 4.9526 0.00053645 -5.4552e-07 v volume_forces[Z] -4.9525 4.9526 -0.00053633 6.4925e-07 v ǁvolume_forcesǁ 8.1352e-09 4.9537 0.54294 0.26569 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.2 291.1 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015259 5.3962e-05 3.0162e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.09847 0.6281 0.18804 0.15897 INSTANT 0.724176000E+00 TIME STEP NUMBER 752 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.27478E-05 0.22929E-02 Friction velocity uk : 0.27495E-05 0.22929E-02 Dimensionless distance yplus : 0.18309E-04 0.15255E-01 Friction thermal sca. tstar : -0.13384E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.12859E-04 0.10714E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.27478E-05 0.22929E-02 Friction velocity uk : 0.27495E-05 0.22929E-02 Dimensionless distance yplus : 0.18309E-04 0.15255E-01 Friction thermal sca. tstar : -0.13384E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.12859E-04 0.10714E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.36281E-08 3 0.12715E-06 0.22610E-12 0.95905E+00 c Velocity[X] 0.67189E-32 c Velocity[Y] 0.11305E-12 c Velocity[Z] 0.11305E-12 c Pressure 0.86273E-14 16 0.67107E-07 0.67107E-07 0.10566E+01 c k 0.33742E-06 2 0.36504E-07 0.19086E-08 0.14206E+01 c omega 0.13153E+02 1 0.11947E-08 0.22351E+00 0.24613E-02 c TempK 0.94690E+02 1 0.91837E-07 0.20822E-01 0.15974E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.5162e-14 7.9456e-14 -9.8585e-18 -2.5577e-18 v Velocity[Y] -0.00012457 0.00011823 -6.8775e-10 -3.5635e-12 v Velocity[Z] -0.00011819 0.00012457 4.163e-10 -2.0263e-12 v ǁVelocityǁ 2.2862e-10 0.0001336 1.0998e-05 7.7021e-06 v Pressure -0.001269 0.022088 0.0012494 -3.9221e-22 v k 8.0658e-10 0.0011153 0.00073934 0.00093909 v omega 14.152 1.0313e+05 2665.8 499.05 v TempK 288 342.05 294 290.96 v Density 1.205 1.205 1.205 1.205 v TurbVisc 9.4576e-15 9.4977e-05 5.7394e-05 7.486e-05 v CourantNb 2.7853e-09 0.00020019 1.3796e-05 8.3988e-06 v FourierNb 0.098359 0.6281 0.18799 0.15892 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9526 4.9526 0.00053667 -5.4582e-07 v volume_forces[Z] -4.9526 4.9526 -0.00053655 6.4958e-07 v ǁvolume_forcesǁ 8.1964e-09 4.9537 0.54315 0.26587 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.21 291.1 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015255 5.3948e-05 3.0153e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.098379 0.6281 0.188 0.15893 INSTANT 0.725139000E+00 TIME STEP NUMBER 753 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.29289E-05 0.22923E-02 Friction velocity uk : 0.29305E-05 0.22923E-02 Dimensionless distance yplus : 0.19514E-04 0.15251E-01 Friction thermal sca. tstar : -0.13228E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.13705E-04 0.10711E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.29289E-05 0.22923E-02 Friction velocity uk : 0.29305E-05 0.22923E-02 Dimensionless distance yplus : 0.19514E-04 0.15251E-01 Friction thermal sca. tstar : -0.13228E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.13705E-04 0.10711E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.36295E-08 3 0.12685E-06 0.22566E-12 0.95799E+00 c Velocity[X] 0.66908E-32 c Velocity[Y] 0.11283E-12 c Velocity[Z] 0.11283E-12 c Pressure 0.86435E-14 16 0.67232E-07 0.67232E-07 0.10552E+01 c k 0.33697E-06 2 0.36439E-07 0.18993E-08 0.14190E+01 c omega 0.13153E+02 1 0.11914E-08 0.22249E+00 0.24556E-02 c TempK 0.94690E+02 1 0.91664E-07 0.20780E-01 0.15958E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.5103e-14 7.9408e-14 -9.8528e-18 -2.5563e-18 v Velocity[Y] -0.00012454 0.0001182 -6.8556e-10 -3.558e-12 v Velocity[Z] -0.00011816 0.00012455 4.1392e-10 -2.0266e-12 v ǁVelocityǁ 2.307e-10 0.00013357 1.1002e-05 7.7083e-06 v Pressure -0.0012706 0.022102 0.0012504 -5.5596e-20 v k 8.0374e-10 0.001114 0.00073828 0.00093778 v omega 14.137 1.0313e+05 2665.8 499.03 v TempK 288 342.05 294 290.96 v Density 1.205 1.205 1.205 1.205 v TurbVisc 9.4243e-15 9.4966e-05 5.7374e-05 7.4838e-05 v CourantNb 2.7883e-09 0.00020009 1.3796e-05 8.4023e-06 v FourierNb 0.098268 0.6281 0.18795 0.15888 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9526 4.9527 0.00053689 -5.4612e-07 v volume_forces[Z] -4.9526 4.9527 -0.00053676 6.4991e-07 v ǁvolume_forcesǁ 8.2646e-09 4.9538 0.54337 0.26605 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.21 291.1 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015251 5.3934e-05 3.0145e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.098288 0.6281 0.18796 0.15889 INSTANT 0.726102000E+00 TIME STEP NUMBER 754 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.30998E-05 0.22917E-02 Friction velocity uk : 0.31013E-05 0.22917E-02 Dimensionless distance yplus : 0.20651E-04 0.15247E-01 Friction thermal sca. tstar : -0.13077E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.14504E-04 0.10708E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.30998E-05 0.22917E-02 Friction velocity uk : 0.31013E-05 0.22917E-02 Dimensionless distance yplus : 0.20651E-04 0.15247E-01 Friction thermal sca. tstar : -0.13077E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.14504E-04 0.10708E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.36308E-08 3 0.12654E-06 0.22521E-12 0.95694E+00 c Velocity[X] 0.66628E-32 c Velocity[Y] 0.11260E-12 c Velocity[Z] 0.11260E-12 c Pressure 0.85985E-14 16 0.66881E-07 0.66881E-07 0.10537E+01 c k 0.33652E-06 2 0.36375E-07 0.18901E-08 0.14175E+01 c omega 0.13153E+02 1 0.11882E-08 0.22147E+00 0.24500E-02 c TempK 0.94691E+02 1 0.91492E-07 0.20739E-01 0.15942E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.5044e-14 7.936e-14 -9.8472e-18 -2.555e-18 v Velocity[Y] -0.00012451 0.00011816 -6.8336e-10 -3.5526e-12 v Velocity[Z] -0.00011812 0.00012452 4.1153e-10 -2.0269e-12 v ǁVelocityǁ 2.3296e-10 0.00013353 1.1006e-05 7.7144e-06 v Pressure -0.0012723 0.022116 0.0012514 -3.3338e-20 v k 8.0092e-10 0.0011126 0.00073722 0.00093648 v omega 14.121 1.0313e+05 2665.8 499.02 v TempK 288 342.05 294 290.96 v Density 1.205 1.205 1.205 1.205 v TurbVisc 9.3912e-15 9.4955e-05 5.7355e-05 7.4816e-05 v CourantNb 2.7912e-09 0.00019999 1.3796e-05 8.4058e-06 v FourierNb 0.098177 0.6281 0.18791 0.15885 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9527 4.9527 0.0005371 -5.4642e-07 v volume_forces[Z] -4.9527 4.9527 -0.00053698 6.5024e-07 v ǁvolume_forcesǁ 8.3397e-09 4.9538 0.54358 0.26622 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.21 291.11 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015247 5.392e-05 3.0136e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.098197 0.6281 0.18793 0.15885 INSTANT 0.727065000E+00 TIME STEP NUMBER 755 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.32621E-05 0.22911E-02 Friction velocity uk : 0.32635E-05 0.22911E-02 Dimensionless distance yplus : 0.21731E-04 0.15243E-01 Friction thermal sca. tstar : -0.12931E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.15263E-04 0.10706E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.32621E-05 0.22911E-02 Friction velocity uk : 0.32635E-05 0.22911E-02 Dimensionless distance yplus : 0.21731E-04 0.15243E-01 Friction thermal sca. tstar : -0.12931E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.15263E-04 0.10706E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.36322E-08 3 0.12622E-06 0.22476E-12 0.95589E+00 c Velocity[X] 0.66350E-32 c Velocity[Y] 0.11238E-12 c Velocity[Z] 0.11238E-12 c Pressure 0.85758E-14 16 0.66703E-07 0.66703E-07 0.10522E+01 c k 0.33607E-06 2 0.36310E-07 0.18808E-08 0.14159E+01 c omega 0.13153E+02 1 0.11849E-08 0.22046E+00 0.24444E-02 c TempK 0.94692E+02 1 0.91320E-07 0.20698E-01 0.15926E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.4985e-14 7.9313e-14 -9.8415e-18 -2.5536e-18 v Velocity[Y] -0.00012448 0.00011813 -6.8116e-10 -3.5472e-12 v Velocity[Z] -0.00011809 0.00012449 4.0914e-10 -2.0273e-12 v ǁVelocityǁ 2.3541e-10 0.0001335 1.1009e-05 7.7206e-06 v Pressure -0.001274 0.022131 0.0012524 2.8239e-20 v k 7.9811e-10 0.0011112 0.00073616 0.00093518 v omega 14.105 1.0313e+05 2665.8 499 v TempK 288 342.05 294 290.97 v Density 1.205 1.205 1.205 1.205 v TurbVisc 9.3582e-15 9.4944e-05 5.7336e-05 7.4793e-05 v CourantNb 2.7941e-09 0.00019989 1.3796e-05 8.4093e-06 v FourierNb 0.098087 0.6281 0.18787 0.15881 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9528 4.9528 0.00053731 -5.4671e-07 v volume_forces[Z] -4.9528 4.9528 -0.00053719 6.5057e-07 v ǁvolume_forcesǁ 8.4217e-09 4.9539 0.5438 0.2664 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.21 291.11 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015243 5.3906e-05 3.0128e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.098107 0.6281 0.18789 0.15881 INSTANT 0.728028000E+00 TIME STEP NUMBER 756 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.34170E-05 0.22905E-02 Friction velocity uk : 0.34183E-05 0.22905E-02 Dimensionless distance yplus : 0.22762E-04 0.15239E-01 Friction thermal sca. tstar : -0.13106E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.15987E-04 0.10703E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.34170E-05 0.22905E-02 Friction velocity uk : 0.34183E-05 0.22905E-02 Dimensionless distance yplus : 0.22762E-04 0.15239E-01 Friction thermal sca. tstar : -0.13106E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.15987E-04 0.10703E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.36335E-08 3 0.12592E-06 0.22431E-12 0.95483E+00 c Velocity[X] 0.66072E-32 c Velocity[Y] 0.11216E-12 c Velocity[Z] 0.11216E-12 c Pressure 0.85589E-14 16 0.66571E-07 0.66571E-07 0.10508E+01 c k 0.33562E-06 2 0.36246E-07 0.18717E-08 0.14144E+01 c omega 0.13153E+02 1 0.11816E-08 0.21946E+00 0.24389E-02 c TempK 0.94692E+02 1 0.91148E-07 0.20657E-01 0.15910E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.4926e-14 7.9265e-14 -9.8358e-18 -2.5523e-18 v Velocity[Y] -0.00012445 0.00011809 -6.7895e-10 -3.5418e-12 v Velocity[Z] -0.00011805 0.00012446 4.0674e-10 -2.0276e-12 v ǁVelocityǁ 2.3805e-10 0.00013347 1.1013e-05 7.7267e-06 v Pressure -0.0012756 0.022145 0.0012534 1.7061e-20 v k 7.9532e-10 0.0011099 0.0007351 0.00093389 v omega 14.089 1.0313e+05 2665.8 498.99 v TempK 288 342.05 294.01 290.97 v Density 1.205 1.205 1.205 1.205 v TurbVisc 9.3254e-15 9.4933e-05 5.7317e-05 7.4771e-05 v CourantNb 2.7971e-09 0.00019979 1.3797e-05 8.4128e-06 v FourierNb 0.097996 0.6281 0.18783 0.15877 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9528 4.9528 0.00053753 -5.4701e-07 v volume_forces[Z] -4.9528 4.9528 -0.00053741 6.509e-07 v ǁvolume_forcesǁ 8.5103e-09 4.9539 0.54401 0.26657 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.21 291.11 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015239 5.3892e-05 3.0119e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.098016 0.6281 0.18785 0.15878 INSTANT 0.728991000E+00 TIME STEP NUMBER 757 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.35655E-05 0.22899E-02 Friction velocity uk : 0.35668E-05 0.22899E-02 Dimensionless distance yplus : 0.23751E-04 0.15235E-01 Friction thermal sca. tstar : -0.13370E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.16681E-04 0.10700E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.35655E-05 0.22899E-02 Friction velocity uk : 0.35668E-05 0.22899E-02 Dimensionless distance yplus : 0.23751E-04 0.15235E-01 Friction thermal sca. tstar : -0.13370E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.16681E-04 0.10700E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.36349E-08 3 0.12561E-06 0.22387E-12 0.95378E+00 c Velocity[X] 0.65797E-32 c Velocity[Y] 0.11193E-12 c Velocity[Z] 0.11193E-12 c Pressure 0.85420E-14 16 0.66439E-07 0.66439E-07 0.10493E+01 c k 0.33517E-06 2 0.36182E-07 0.18626E-08 0.14128E+01 c omega 0.13153E+02 1 0.11784E-08 0.21846E+00 0.24333E-02 c TempK 0.94693E+02 1 0.90978E-07 0.20616E-01 0.15895E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.4868e-14 7.9218e-14 -9.8302e-18 -2.5509e-18 v Velocity[Y] -0.00012442 0.00011806 -6.7674e-10 -3.5365e-12 v Velocity[Z] -0.00011802 0.00012443 4.0435e-10 -2.028e-12 v ǁVelocityǁ 2.4085e-10 0.00013344 1.1017e-05 7.7329e-06 v Pressure -0.0012773 0.022159 0.0012544 -3.6181e-20 v k 7.9253e-10 0.0011085 0.00073405 0.0009326 v omega 14.074 1.0313e+05 2665.7 498.98 v TempK 288 342.06 294.01 290.97 v Density 1.205 1.205 1.205 1.205 v TurbVisc 9.2927e-15 9.4922e-05 5.7298e-05 7.4749e-05 v CourantNb 2.8e-09 0.0001997 1.3797e-05 8.4163e-06 v FourierNb 0.097907 0.6281 0.1878 0.15873 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9529 4.9529 0.00053774 -5.4731e-07 v volume_forces[Z] -4.9529 4.9529 -0.00053762 6.5123e-07 v ǁvolume_forcesǁ 8.6053e-09 4.954 0.54422 0.26675 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.22 291.11 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015235 5.3877e-05 3.0111e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.097926 0.6281 0.18781 0.15874 INSTANT 0.729954000E+00 TIME STEP NUMBER 758 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.37084E-05 0.22894E-02 Friction velocity uk : 0.37096E-05 0.22893E-02 Dimensionless distance yplus : 0.24702E-04 0.15231E-01 Friction thermal sca. tstar : -0.13650E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.17349E-04 0.10697E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.37084E-05 0.22894E-02 Friction velocity uk : 0.37096E-05 0.22893E-02 Dimensionless distance yplus : 0.24702E-04 0.15231E-01 Friction thermal sca. tstar : -0.13650E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.17349E-04 0.10697E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.36363E-08 3 0.12530E-06 0.22342E-12 0.95273E+00 c Velocity[X] 0.65523E-32 c Velocity[Y] 0.11171E-12 c Velocity[Z] 0.11171E-12 c Pressure 0.85251E-14 16 0.66306E-07 0.66306E-07 0.10479E+01 c k 0.33472E-06 2 0.36118E-07 0.18536E-08 0.14113E+01 c omega 0.13153E+02 1 0.11752E-08 0.21747E+00 0.24278E-02 c TempK 0.94693E+02 1 0.90807E-07 0.20575E-01 0.15879E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.4809e-14 7.917e-14 -9.8246e-18 -2.5496e-18 v Velocity[Y] -0.00012439 0.00011802 -6.7453e-10 -3.5311e-12 v Velocity[Z] -0.00011798 0.0001244 4.0195e-10 -2.0283e-12 v ǁVelocityǁ 2.4383e-10 0.0001334 1.102e-05 7.739e-06 v Pressure -0.001279 0.022174 0.0012554 1.2394e-19 v k 7.8976e-10 0.0011072 0.000733 0.00093131 v omega 14.058 1.0313e+05 2665.7 498.96 v TempK 288 342.06 294.01 290.97 v Density 1.205 1.205 1.205 1.205 v TurbVisc 9.2602e-15 9.4911e-05 5.7279e-05 7.4727e-05 v CourantNb 2.8029e-09 0.0001996 1.3797e-05 8.4199e-06 v FourierNb 0.097817 0.6281 0.18776 0.15869 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9529 4.9529 0.00053796 -5.476e-07 v volume_forces[Z] -4.9529 4.9529 -0.00053784 6.5155e-07 v ǁvolume_forcesǁ 8.7067e-09 4.954 0.54443 0.26692 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.22 291.11 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015231 5.3863e-05 3.0102e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.097837 0.6281 0.18777 0.1587 INSTANT 0.730917000E+00 TIME STEP NUMBER 759 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.38462E-05 0.22888E-02 Friction velocity uk : 0.38474E-05 0.22887E-02 Dimensionless distance yplus : 0.25619E-04 0.15227E-01 Friction thermal sca. tstar : -0.13949E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.17993E-04 0.10695E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.38462E-05 0.22888E-02 Friction velocity uk : 0.38474E-05 0.22887E-02 Dimensionless distance yplus : 0.25619E-04 0.15227E-01 Friction thermal sca. tstar : -0.13949E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.17993E-04 0.10695E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.36376E-08 3 0.12500E-06 0.22298E-12 0.95168E+00 c Velocity[X] 0.65251E-32 c Velocity[Y] 0.11149E-12 c Velocity[Z] 0.11149E-12 c Pressure 0.85086E-14 16 0.66177E-07 0.66177E-07 0.10464E+01 c k 0.33428E-06 2 0.36054E-07 0.18446E-08 0.14097E+01 c omega 0.13153E+02 1 0.11719E-08 0.21648E+00 0.24222E-02 c TempK 0.94694E+02 1 0.90638E-07 0.20535E-01 0.15863E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.4751e-14 7.9123e-14 -9.8189e-18 -2.5483e-18 v Velocity[Y] -0.00012436 0.00011799 -6.7231e-10 -3.5258e-12 v Velocity[Z] -0.00011795 0.00012437 3.9955e-10 -2.0286e-12 v ǁVelocityǁ 2.4697e-10 0.00013337 1.1024e-05 7.7452e-06 v Pressure -0.0012806 0.022188 0.0012564 -1.3237e-20 v k 7.8701e-10 0.0011058 0.00073195 0.00093002 v omega 14.043 1.0313e+05 2665.7 498.95 v TempK 288 342.06 294.01 290.97 v Density 1.205 1.205 1.205 1.205 v TurbVisc 9.2278e-15 9.49e-05 5.726e-05 7.4705e-05 v CourantNb 2.8059e-09 0.0001995 1.3797e-05 8.4234e-06 v FourierNb 0.097727 0.6281 0.18772 0.15865 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.953 4.953 0.00053817 -5.479e-07 v volume_forces[Z] -4.953 4.953 -0.00053805 6.5188e-07 v ǁvolume_forcesǁ 8.8143e-09 4.9541 0.54465 0.2671 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.22 291.12 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015227 5.3849e-05 3.0094e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.097747 0.6281 0.18773 0.15866 INSTANT 0.731880000E+00 TIME STEP NUMBER 760 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.39796E-05 0.22882E-02 Friction velocity uk : 0.39807E-05 0.22881E-02 Dimensionless distance yplus : 0.26507E-04 0.15223E-01 Friction thermal sca. tstar : -0.14269E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.18617E-04 0.10692E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.39796E-05 0.22882E-02 Friction velocity uk : 0.39807E-05 0.22881E-02 Dimensionless distance yplus : 0.26507E-04 0.15223E-01 Friction thermal sca. tstar : -0.14269E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.18617E-04 0.10692E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.36390E-08 3 0.12470E-06 0.22253E-12 0.95063E+00 c Velocity[X] 0.64980E-32 c Velocity[Y] 0.11127E-12 c Velocity[Z] 0.11127E-12 c Pressure 0.85035E-14 16 0.66136E-07 0.66136E-07 0.10450E+01 c k 0.33383E-06 2 0.35991E-07 0.18356E-08 0.14082E+01 c omega 0.13153E+02 1 0.11687E-08 0.21550E+00 0.24167E-02 c TempK 0.94694E+02 1 0.90468E-07 0.20494E-01 0.15847E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.4693e-14 7.9076e-14 -9.8133e-18 -2.5469e-18 v Velocity[Y] -0.00012434 0.00011796 -6.7009e-10 -3.5205e-12 v Velocity[Z] -0.00011791 0.00012434 3.9714e-10 -2.0289e-12 v ǁVelocityǁ 2.5027e-10 0.00013334 1.1028e-05 7.7513e-06 v Pressure -0.0012823 0.022202 0.0012573 -2.2454e-20 v k 7.8427e-10 0.0011045 0.0007309 0.00092874 v omega 14.027 1.0313e+05 2665.7 498.93 v TempK 288 342.06 294.01 290.98 v Density 1.205 1.205 1.205 1.205 v TurbVisc 9.1956e-15 9.4889e-05 5.7241e-05 7.4682e-05 v CourantNb 2.8088e-09 0.0001994 1.3797e-05 8.4269e-06 v FourierNb 0.097638 0.6281 0.18768 0.15861 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.953 4.953 0.00053838 -5.4819e-07 v volume_forces[Z] -4.953 4.953 -0.00053827 6.5221e-07 v ǁvolume_forcesǁ 8.9278e-09 4.9541 0.54486 0.26728 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.22 291.12 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015223 5.3835e-05 3.0085e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.097658 0.6281 0.18769 0.15862 INSTANT 0.732843000E+00 TIME STEP NUMBER 761 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.41089E-05 0.22876E-02 Friction velocity uk : 0.41099E-05 0.22876E-02 Dimensionless distance yplus : 0.27367E-04 0.15219E-01 Friction thermal sca. tstar : -0.14612E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.19221E-04 0.10689E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.41089E-05 0.22876E-02 Friction velocity uk : 0.41099E-05 0.22876E-02 Dimensionless distance yplus : 0.27367E-04 0.15219E-01 Friction thermal sca. tstar : -0.14612E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.19221E-04 0.10689E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.36404E-08 3 0.12442E-06 0.22209E-12 0.94958E+00 c Velocity[X] 0.64710E-32 c Velocity[Y] 0.11104E-12 c Velocity[Z] 0.11105E-12 c Pressure 0.85129E-14 16 0.66209E-07 0.66209E-07 0.10436E+01 c k 0.33339E-06 2 0.35927E-07 0.18268E-08 0.14067E+01 c omega 0.13153E+02 1 0.11655E-08 0.21452E+00 0.24112E-02 c TempK 0.94695E+02 1 0.90300E-07 0.20454E-01 0.15831E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.4634e-14 7.9029e-14 -9.8077e-18 -2.5456e-18 v Velocity[Y] -0.00012431 0.00011792 -6.6787e-10 -3.5152e-12 v Velocity[Z] -0.00011788 0.00012431 3.9474e-10 -2.0292e-12 v ǁVelocityǁ 2.5372e-10 0.00013331 1.1031e-05 7.7575e-06 v Pressure -0.001284 0.022217 0.0012583 -7.0206e-20 v k 7.8154e-10 0.0011031 0.00072986 0.00092746 v omega 14.012 1.0313e+05 2665.7 498.92 v TempK 288 342.06 294.02 290.98 v Density 1.205 1.205 1.205 1.205 v TurbVisc 9.1636e-15 9.4878e-05 5.7222e-05 7.466e-05 v CourantNb 2.8117e-09 0.0001993 1.3797e-05 8.4304e-06 v FourierNb 0.097549 0.6281 0.18764 0.15857 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9531 4.9531 0.0005386 -5.4849e-07 v volume_forces[Z] -4.9531 4.9531 -0.00053848 6.5253e-07 v ǁvolume_forcesǁ 9.0472e-09 4.9542 0.54507 0.26745 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.23 291.12 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015219 5.3821e-05 3.0077e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.097569 0.6281 0.18766 0.15858 INSTANT 0.733806000E+00 TIME STEP NUMBER 762 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.42345E-05 0.22870E-02 Friction velocity uk : 0.42355E-05 0.22870E-02 Dimensionless distance yplus : 0.28204E-04 0.15216E-01 Friction thermal sca. tstar : -0.14981E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.19808E-04 0.10686E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.42345E-05 0.22870E-02 Friction velocity uk : 0.42355E-05 0.22870E-02 Dimensionless distance yplus : 0.28204E-04 0.15216E-01 Friction thermal sca. tstar : -0.14981E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.19808E-04 0.10686E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.36417E-08 3 0.12410E-06 0.22165E-12 0.94852E+00 c Velocity[X] 0.64441E-32 c Velocity[Y] 0.11082E-12 c Velocity[Z] 0.11083E-12 c Pressure 0.84587E-14 16 0.65786E-07 0.65786E-07 0.10421E+01 c k 0.33295E-06 2 0.35864E-07 0.18179E-08 0.14052E+01 c omega 0.13153E+02 1 0.11623E-08 0.21355E+00 0.24058E-02 c TempK 0.94695E+02 1 0.90132E-07 0.20414E-01 0.15816E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.4576e-14 7.8982e-14 -9.8021e-18 -2.5443e-18 v Velocity[Y] -0.00012428 0.00011789 -6.6564e-10 -3.5099e-12 v Velocity[Z] -0.00011785 0.00012428 3.9233e-10 -2.0295e-12 v ǁVelocityǁ 2.5733e-10 0.00013328 1.1035e-05 7.7636e-06 v Pressure -0.0012856 0.022231 0.0012593 5.6478e-20 v k 7.7882e-10 0.0011018 0.00072882 0.00092619 v omega 13.996 1.0313e+05 2665.7 498.91 v TempK 288 342.06 294.02 290.98 v Density 1.205 1.205 1.205 1.205 v TurbVisc 9.1317e-15 9.4867e-05 5.7203e-05 7.4638e-05 v CourantNb 2.8146e-09 0.00019921 1.3797e-05 8.4339e-06 v FourierNb 0.097461 0.6281 0.1876 0.15853 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9531 4.9531 0.00053881 -5.4878e-07 v volume_forces[Z] -4.9531 4.9531 -0.00053869 6.5286e-07 v ǁvolume_forcesǁ 9.1721e-09 4.9542 0.54528 0.26763 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.23 291.12 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015216 5.3807e-05 3.0069e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.097481 0.6281 0.18762 0.15854 INSTANT 0.734769000E+00 TIME STEP NUMBER 763 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.43567E-05 0.22864E-02 Friction velocity uk : 0.43577E-05 0.22864E-02 Dimensionless distance yplus : 0.29017E-04 0.15212E-01 Friction thermal sca. tstar : -0.15379E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.20380E-04 0.10684E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.43567E-05 0.22864E-02 Friction velocity uk : 0.43577E-05 0.22864E-02 Dimensionless distance yplus : 0.29017E-04 0.15212E-01 Friction thermal sca. tstar : -0.15379E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.20380E-04 0.10684E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.36431E-08 3 0.12380E-06 0.22121E-12 0.94747E+00 c Velocity[X] 0.64175E-32 c Velocity[Y] 0.11060E-12 c Velocity[Z] 0.11060E-12 c Pressure 0.84428E-14 16 0.65661E-07 0.65661E-07 0.10407E+01 c k 0.33250E-06 2 0.35801E-07 0.18092E-08 0.14036E+01 c omega 0.13153E+02 1 0.11592E-08 0.21258E+00 0.24003E-02 c TempK 0.94696E+02 1 0.89964E-07 0.20374E-01 0.15800E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.4518e-14 7.8935e-14 -9.7966e-18 -2.5429e-18 v Velocity[Y] -0.00012425 0.00011785 -6.6341e-10 -3.5046e-12 v Velocity[Z] -0.00011781 0.00012425 3.8992e-10 -2.0297e-12 v ǁVelocityǁ 2.6108e-10 0.00013325 1.1039e-05 7.7697e-06 v Pressure -0.0012873 0.022245 0.0012603 -2.0003e-20 v k 7.7611e-10 0.0011004 0.00072778 0.00092491 v omega 13.981 1.0313e+05 2665.7 498.89 v TempK 288 342.06 294.02 290.98 v Density 1.205 1.205 1.205 1.205 v TurbVisc 9.0999e-15 9.4856e-05 5.7184e-05 7.4616e-05 v CourantNb 2.8175e-09 0.00019911 1.3797e-05 8.4374e-06 v FourierNb 0.097372 0.6281 0.18757 0.1585 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9532 4.9532 0.00053902 -5.4908e-07 v volume_forces[Z] -4.9532 4.9532 -0.00053891 6.5318e-07 v ǁvolume_forcesǁ 9.3025e-09 4.9543 0.54549 0.2678 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.23 291.12 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015212 5.3793e-05 3.006e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.097392 0.6281 0.18758 0.1585 INSTANT 0.735732000E+00 TIME STEP NUMBER 764 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.44758E-05 0.22858E-02 Friction velocity uk : 0.44768E-05 0.22858E-02 Dimensionless distance yplus : 0.29810E-04 0.15208E-01 Friction thermal sca. tstar : -0.15811E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.20937E-04 0.10681E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.44758E-05 0.22858E-02 Friction velocity uk : 0.44768E-05 0.22858E-02 Dimensionless distance yplus : 0.29810E-04 0.15208E-01 Friction thermal sca. tstar : -0.15811E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.20937E-04 0.10681E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.36445E-08 3 0.12350E-06 0.22076E-12 0.94642E+00 c Velocity[X] 0.63910E-32 c Velocity[Y] 0.11038E-12 c Velocity[Z] 0.11038E-12 c Pressure 0.84267E-14 16 0.65536E-07 0.65536E-07 0.10393E+01 c k 0.33206E-06 2 0.35738E-07 0.18005E-08 0.14021E+01 c omega 0.13153E+02 1 0.11560E-08 0.21162E+00 0.23949E-02 c TempK 0.94697E+02 1 0.89797E-07 0.20334E-01 0.15785E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.4461e-14 7.8889e-14 -9.791e-18 -2.5416e-18 v Velocity[Y] -0.00012422 0.00011782 -6.6118e-10 -3.4993e-12 v Velocity[Z] -0.00011778 0.00012422 3.8751e-10 -2.03e-12 v ǁVelocityǁ 2.6497e-10 0.00013321 1.1042e-05 7.7759e-06 v Pressure -0.001289 0.022259 0.0012613 -1.4914e-19 v k 7.7342e-10 0.0010991 0.00072675 0.00092365 v omega 13.965 1.0313e+05 2665.7 498.88 v TempK 288 342.06 294.02 290.98 v Density 1.205 1.205 1.205 1.205 v TurbVisc 9.0683e-15 9.4845e-05 5.7165e-05 7.4594e-05 v CourantNb 2.8204e-09 0.00019901 1.3797e-05 8.4409e-06 v FourierNb 0.097284 0.6281 0.18753 0.15846 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9532 4.9532 0.00053924 -5.4937e-07 v volume_forces[Z] -4.9532 4.9532 -0.00053912 6.535e-07 v ǁvolume_forcesǁ 9.4381e-09 4.9543 0.5457 0.26798 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.23 291.13 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015208 5.3779e-05 3.0052e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.097304 0.6281 0.18754 0.15847 INSTANT 0.736695000E+00 TIME STEP NUMBER 765 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.45922E-05 0.22853E-02 Friction velocity uk : 0.45931E-05 0.22852E-02 Dimensionless distance yplus : 0.30585E-04 0.15204E-01 Friction thermal sca. tstar : -0.16281E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.21481E-04 0.10678E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.45922E-05 0.22853E-02 Friction velocity uk : 0.45931E-05 0.22852E-02 Dimensionless distance yplus : 0.30585E-04 0.15204E-01 Friction thermal sca. tstar : -0.16281E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.21481E-04 0.10678E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.36459E-08 3 0.12320E-06 0.22032E-12 0.94537E+00 c Velocity[X] 0.63647E-32 c Velocity[Y] 0.11016E-12 c Velocity[Z] 0.11016E-12 c Pressure 0.84092E-14 16 0.65398E-07 0.65398E-07 0.10378E+01 c k 0.33162E-06 2 0.35676E-07 0.17918E-08 0.14006E+01 c omega 0.13153E+02 1 0.11529E-08 0.21067E+00 0.23895E-02 c TempK 0.94697E+02 1 0.89631E-07 0.20294E-01 0.15769E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.4403e-14 7.8842e-14 -9.7854e-18 -2.5403e-18 v Velocity[Y] -0.00012419 0.00011779 -6.5894e-10 -3.494e-12 v Velocity[Z] -0.00011774 0.0001242 3.8509e-10 -2.0302e-12 v ǁVelocityǁ 2.69e-10 0.00013318 1.1046e-05 7.782e-06 v Pressure -0.0012906 0.022274 0.0012623 -1.0423e-19 v k 7.7074e-10 0.0010978 0.00072571 0.00092238 v omega 13.95 1.0313e+05 2665.7 498.87 v TempK 288 342.06 294.03 290.99 v Density 1.205 1.205 1.205 1.205 v TurbVisc 9.0369e-15 9.4834e-05 5.7147e-05 7.4572e-05 v CourantNb 2.8233e-09 0.00019892 1.3797e-05 8.4445e-06 v FourierNb 0.097197 0.6281 0.18749 0.15842 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9533 4.9533 0.00053945 -5.4966e-07 v volume_forces[Z] -4.9533 4.9533 -0.00053933 6.5383e-07 v ǁvolume_forcesǁ 9.5788e-09 4.9544 0.54592 0.26815 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.24 291.13 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015204 5.3765e-05 3.0043e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.097216 0.6281 0.1875 0.15843 INSTANT 0.737658000E+00 TIME STEP NUMBER 766 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.47058E-05 0.22847E-02 Friction velocity uk : 0.47067E-05 0.22846E-02 Dimensionless distance yplus : 0.31341E-04 0.15200E-01 Friction thermal sca. tstar : -0.16796E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.22012E-04 0.10675E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.47058E-05 0.22847E-02 Friction velocity uk : 0.47067E-05 0.22846E-02 Dimensionless distance yplus : 0.31341E-04 0.15200E-01 Friction thermal sca. tstar : -0.16796E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.22012E-04 0.10675E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.36472E-08 3 0.12290E-06 0.21988E-12 0.94432E+00 c Velocity[X] 0.63385E-32 c Velocity[Y] 0.10994E-12 c Velocity[Z] 0.10994E-12 c Pressure 0.83971E-14 16 0.65303E-07 0.65303E-07 0.10364E+01 c k 0.33119E-06 2 0.35613E-07 0.17832E-08 0.13991E+01 c omega 0.13153E+02 1 0.11497E-08 0.20972E+00 0.23841E-02 c TempK 0.94698E+02 1 0.89464E-07 0.20254E-01 0.15753E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.4345e-14 7.8796e-14 -9.7799e-18 -2.539e-18 v Velocity[Y] -0.00012416 0.00011775 -6.567e-10 -3.4887e-12 v Velocity[Z] -0.00011771 0.00012417 3.8267e-10 -2.0303e-12 v ǁVelocityǁ 2.7316e-10 0.00013315 1.105e-05 7.7881e-06 v Pressure -0.0012923 0.022288 0.0012633 5.491e-20 v k 7.6808e-10 0.0010964 0.00072468 0.00092112 v omega 13.935 1.0313e+05 2665.7 498.85 v TempK 288 342.06 294.03 290.99 v Density 1.205 1.205 1.205 1.205 v TurbVisc 9.0056e-15 9.4823e-05 5.7128e-05 7.455e-05 v CourantNb 2.8262e-09 0.00019882 1.3798e-05 8.448e-06 v FourierNb 0.097109 0.6281 0.18745 0.15838 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9533 4.9534 0.00053966 -5.4995e-07 v volume_forces[Z] -4.9533 4.9534 -0.00053954 6.5415e-07 v ǁvolume_forcesǁ 9.7243e-09 4.9544 0.54613 0.26832 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.24 291.13 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.0152 5.3751e-05 3.0035e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.097129 0.6281 0.18747 0.15839 INSTANT 0.738621000E+00 TIME STEP NUMBER 767 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.48170E-05 0.22841E-02 Friction velocity uk : 0.48179E-05 0.22840E-02 Dimensionless distance yplus : 0.32082E-04 0.15196E-01 Friction thermal sca. tstar : -0.17363E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.22532E-04 0.10673E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.48170E-05 0.22841E-02 Friction velocity uk : 0.48179E-05 0.22840E-02 Dimensionless distance yplus : 0.32082E-04 0.15196E-01 Friction thermal sca. tstar : -0.17363E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.22532E-04 0.10673E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.36486E-08 3 0.12261E-06 0.21945E-12 0.94327E+00 c Velocity[X] 0.63124E-32 c Velocity[Y] 0.10972E-12 c Velocity[Z] 0.10972E-12 c Pressure 0.83810E-14 16 0.65177E-07 0.65177E-07 0.10350E+01 c k 0.33075E-06 2 0.35551E-07 0.17746E-08 0.13976E+01 c omega 0.13153E+02 1 0.11466E-08 0.20877E+00 0.23787E-02 c TempK 0.94698E+02 1 0.89299E-07 0.20215E-01 0.15738E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.4288e-14 7.8749e-14 -9.7744e-18 -2.5377e-18 v Velocity[Y] -0.00012413 0.00011772 -6.5446e-10 -3.4834e-12 v Velocity[Z] -0.00011768 0.00012414 3.8026e-10 -2.0306e-12 v ǁVelocityǁ 2.7744e-10 0.00013312 1.1054e-05 7.7943e-06 v Pressure -0.0012939 0.022302 0.0012643 1.814e-20 v k 7.6542e-10 0.0010951 0.00072366 0.00091986 v omega 13.919 1.0313e+05 2665.6 498.84 v TempK 288 342.06 294.03 290.99 v Density 1.205 1.205 1.205 1.205 v TurbVisc 8.9744e-15 9.4812e-05 5.7109e-05 7.4528e-05 v CourantNb 2.8291e-09 0.00019872 1.3798e-05 8.4515e-06 v FourierNb 0.097022 0.6281 0.18741 0.15834 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9534 4.9534 0.00053987 -5.5024e-07 v volume_forces[Z] -4.9534 4.9534 -0.00053976 6.5447e-07 v ǁvolume_forcesǁ 9.8746e-09 4.9545 0.54634 0.2685 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.24 291.13 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015196 5.3738e-05 3.0026e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.097041 0.6281 0.18743 0.15835 INSTANT 0.739584000E+00 TIME STEP NUMBER 768 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.49259E-05 0.22835E-02 Friction velocity uk : 0.49268E-05 0.22835E-02 Dimensionless distance yplus : 0.32807E-04 0.15192E-01 Friction thermal sca. tstar : -0.17991E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.23041E-04 0.10670E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.49259E-05 0.22835E-02 Friction velocity uk : 0.49268E-05 0.22835E-02 Dimensionless distance yplus : 0.32807E-04 0.15192E-01 Friction thermal sca. tstar : -0.17991E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.23041E-04 0.10670E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.36500E-08 3 0.12231E-06 0.21901E-12 0.94222E+00 c Velocity[X] 0.62865E-32 c Velocity[Y] 0.10950E-12 c Velocity[Z] 0.10950E-12 c Pressure 0.83608E-14 16 0.65019E-07 0.65019E-07 0.10336E+01 c k 0.33031E-06 2 0.35489E-07 0.17661E-08 0.13961E+01 c omega 0.13153E+02 1 0.11435E-08 0.20783E+00 0.23734E-02 c TempK 0.94699E+02 1 0.89134E-07 0.20175E-01 0.15722E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.423e-14 7.8703e-14 -9.7688e-18 -2.5363e-18 v Velocity[Y] -0.00012411 0.00011769 -6.5221e-10 -3.4782e-12 v Velocity[Z] -0.00011764 0.00012411 3.7783e-10 -2.0308e-12 v ǁVelocityǁ 2.8184e-10 0.00013309 1.1057e-05 7.8004e-06 v Pressure -0.0012956 0.022316 0.0012652 9.5601e-20 v k 7.6278e-10 0.0010938 0.00072263 0.0009186 v omega 13.904 1.0313e+05 2665.6 498.83 v TempK 288 342.06 294.03 290.99 v Density 1.205 1.205 1.205 1.205 v TurbVisc 8.9434e-15 9.4801e-05 5.709e-05 7.4506e-05 v CourantNb 2.832e-09 0.00019863 1.3798e-05 8.455e-06 v FourierNb 0.096934 0.6281 0.18738 0.1583 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9534 4.9535 0.00054009 -5.5054e-07 v volume_forces[Z] -4.9534 4.9535 -0.00053997 6.5479e-07 v ǁvolume_forcesǁ 1.0029e-08 4.9545 0.54655 0.26867 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.24 291.13 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015192 5.3724e-05 3.0018e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.096954 0.6281 0.18739 0.15831 INSTANT 0.740547000E+00 TIME STEP NUMBER 769 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.50327E-05 0.22829E-02 Friction velocity uk : 0.50335E-05 0.22829E-02 Dimensionless distance yplus : 0.33518E-04 0.15188E-01 Friction thermal sca. tstar : -0.18694E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.23541E-04 0.10667E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.50327E-05 0.22829E-02 Friction velocity uk : 0.50335E-05 0.22829E-02 Dimensionless distance yplus : 0.33518E-04 0.15188E-01 Friction thermal sca. tstar : -0.18694E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.23541E-04 0.10667E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.36514E-08 3 0.12202E-06 0.21857E-12 0.94116E+00 c Velocity[X] 0.62607E-32 c Velocity[Y] 0.10928E-12 c Velocity[Z] 0.10929E-12 c Pressure 0.83435E-14 16 0.64883E-07 0.64883E-07 0.10322E+01 c k 0.32988E-06 2 0.35427E-07 0.17576E-08 0.13946E+01 c omega 0.13153E+02 1 0.11404E-08 0.20690E+00 0.23680E-02 c TempK 0.94699E+02 1 0.88970E-07 0.20136E-01 0.15707E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.4173e-14 7.8657e-14 -9.7633e-18 -2.535e-18 v Velocity[Y] -0.00012408 0.00011765 -6.4997e-10 -3.473e-12 v Velocity[Z] -0.00011761 0.00012408 3.7541e-10 -2.0311e-12 v ǁVelocityǁ 2.8636e-10 0.00013306 1.1061e-05 7.8065e-06 v Pressure -0.0012973 0.02233 0.0012662 8.7267e-20 v k 7.6015e-10 0.0010924 0.00072161 0.00091734 v omega 13.889 1.0313e+05 2665.6 498.81 v TempK 288 342.06 294.04 290.99 v Density 1.205 1.205 1.205 1.205 v TurbVisc 8.9125e-15 9.4791e-05 5.7071e-05 7.4484e-05 v CourantNb 2.8348e-09 0.00019853 1.3798e-05 8.4585e-06 v FourierNb 0.096848 0.6281 0.18734 0.15826 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9535 4.9535 0.0005403 -5.5083e-07 v volume_forces[Z] -4.9535 4.9535 -0.00054018 6.5511e-07 v ǁvolume_forcesǁ 1.0189e-08 4.9546 0.54676 0.26885 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.25 291.14 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015188 5.371e-05 3.001e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.096867 0.6281 0.18735 0.15827 INSTANT 0.741510000E+00 TIME STEP NUMBER 770 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.51375E-05 0.22823E-02 Friction velocity uk : 0.51383E-05 0.22823E-02 Dimensionless distance yplus : 0.34215E-04 0.15185E-01 Friction thermal sca. tstar : -0.19485E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.24031E-04 0.10665E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.51375E-05 0.22823E-02 Friction velocity uk : 0.51383E-05 0.22823E-02 Dimensionless distance yplus : 0.34215E-04 0.15185E-01 Friction thermal sca. tstar : -0.19485E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.24031E-04 0.10665E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.36528E-08 3 0.12172E-06 0.21813E-12 0.94011E+00 c Velocity[X] 0.62351E-32 c Velocity[Y] 0.10906E-12 c Velocity[Z] 0.10907E-12 c Pressure 0.83296E-14 16 0.64774E-07 0.64774E-07 0.10308E+01 c k 0.32944E-06 2 0.35366E-07 0.17492E-08 0.13931E+01 c omega 0.13153E+02 1 0.11373E-08 0.20597E+00 0.23627E-02 c TempK 0.94700E+02 1 0.88806E-07 0.20097E-01 0.15692E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.4116e-14 7.861e-14 -9.7578e-18 -2.5337e-18 v Velocity[Y] -0.00012405 0.00011762 -6.4771e-10 -3.4678e-12 v Velocity[Z] -0.00011758 0.00012405 3.7299e-10 -2.0313e-12 v ǁVelocityǁ 2.9099e-10 0.00013303 1.1065e-05 7.8127e-06 v Pressure -0.0012989 0.022345 0.0012672 -1.0943e-19 v k 7.5753e-10 0.0010911 0.00072059 0.00091609 v omega 13.874 1.0313e+05 2665.6 498.8 v TempK 288 342.06 294.04 291 v Density 1.205 1.205 1.205 1.205 v TurbVisc 8.8818e-15 9.478e-05 5.7053e-05 7.4462e-05 v CourantNb 2.8377e-09 0.00019843 1.3798e-05 8.4621e-06 v FourierNb 0.096761 0.6281 0.1873 0.15823 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9535 4.9536 0.00054051 -5.5112e-07 v volume_forces[Z] -4.9535 4.9536 -0.00054039 6.5543e-07 v ǁvolume_forcesǁ 1.0352e-08 4.9546 0.54697 0.26902 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.25 291.14 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015185 5.3696e-05 3.0001e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.096781 0.6281 0.18731 0.15823 INSTANT 0.742473000E+00 TIME STEP NUMBER 771 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.52404E-05 0.22818E-02 Friction velocity uk : 0.52411E-05 0.22817E-02 Dimensionless distance yplus : 0.34900E-04 0.15181E-01 Friction thermal sca. tstar : -0.20386E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.24512E-04 0.10662E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.52404E-05 0.22818E-02 Friction velocity uk : 0.52411E-05 0.22817E-02 Dimensionless distance yplus : 0.34900E-04 0.15181E-01 Friction thermal sca. tstar : -0.20386E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.24512E-04 0.10662E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.36542E-08 3 0.12143E-06 0.21769E-12 0.93906E+00 c Velocity[X] 0.62096E-32 c Velocity[Y] 0.10885E-12 c Velocity[Z] 0.10885E-12 c Pressure 0.83191E-14 16 0.64692E-07 0.64692E-07 0.10294E+01 c k 0.32901E-06 2 0.35304E-07 0.17408E-08 0.13916E+01 c omega 0.13153E+02 1 0.11342E-08 0.20504E+00 0.23574E-02 c TempK 0.94701E+02 1 0.88642E-07 0.20058E-01 0.15676E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.4059e-14 7.8564e-14 -9.7523e-18 -2.5324e-18 v Velocity[Y] -0.00012402 0.00011759 -6.4546e-10 -3.4626e-12 v Velocity[Z] -0.00011754 0.00012403 3.7056e-10 -2.0315e-12 v ǁVelocityǁ 2.9573e-10 0.000133 1.1068e-05 7.8188e-06 v Pressure -0.0013006 0.022359 0.0012682 8.7463e-20 v k 7.5493e-10 0.0010898 0.00071957 0.00091484 v omega 13.859 1.0313e+05 2665.6 498.79 v TempK 288 342.06 294.04 291 v Density 1.205 1.205 1.205 1.205 v TurbVisc 8.8512e-15 9.4769e-05 5.7034e-05 7.444e-05 v CourantNb 2.8406e-09 0.00019834 1.3798e-05 8.4656e-06 v FourierNb 0.096675 0.6281 0.18726 0.15819 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9536 4.9536 0.00054072 -5.5141e-07 v volume_forces[Z] -4.9536 4.9536 -0.0005406 6.5575e-07 v ǁvolume_forcesǁ 1.0519e-08 4.9547 0.54718 0.2692 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.25 291.14 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015181 5.3682e-05 2.9993e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.096694 0.6281 0.18728 0.1582 INSTANT 0.743436000E+00 TIME STEP NUMBER 772 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.53415E-05 0.22812E-02 Friction velocity uk : 0.53422E-05 0.22811E-02 Dimensionless distance yplus : 0.35573E-04 0.15177E-01 Friction thermal sca. tstar : -0.21424E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.24984E-04 0.10659E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.53415E-05 0.22812E-02 Friction velocity uk : 0.53422E-05 0.22811E-02 Dimensionless distance yplus : 0.35573E-04 0.15177E-01 Friction thermal sca. tstar : -0.21424E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.24984E-04 0.10659E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.36556E-08 3 0.12114E-06 0.21726E-12 0.93801E+00 c Velocity[X] 0.61842E-32 c Velocity[Y] 0.10863E-12 c Velocity[Z] 0.10863E-12 c Pressure 0.82970E-14 16 0.64519E-07 0.64519E-07 0.10280E+01 c k 0.32858E-06 2 0.35243E-07 0.17325E-08 0.13901E+01 c omega 0.13153E+02 1 0.11312E-08 0.20413E+00 0.23521E-02 c TempK 0.94701E+02 1 0.88479E-07 0.20019E-01 0.15661E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.4002e-14 7.8518e-14 -9.7469e-18 -2.5311e-18 v Velocity[Y] -0.00012399 0.00011755 -6.432e-10 -3.4574e-12 v Velocity[Z] -0.00011751 0.000124 3.6813e-10 -2.0317e-12 v ǁVelocityǁ 3.0058e-10 0.00013297 1.1072e-05 7.8249e-06 v Pressure -0.0013023 0.022373 0.0012692 3.5299e-21 v k 7.5234e-10 0.0010885 0.00071856 0.0009136 v omega 13.844 1.0313e+05 2665.6 498.77 v TempK 288 342.06 294.04 291 v Density 1.205 1.205 1.205 1.205 v TurbVisc 8.8208e-15 9.4758e-05 5.7015e-05 7.4419e-05 v CourantNb 2.8435e-09 0.00019824 1.3798e-05 8.4691e-06 v FourierNb 0.096589 0.6281 0.18722 0.15815 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9536 4.9537 0.00054093 -5.5169e-07 v volume_forces[Z] -4.9536 4.9537 -0.00054081 6.5607e-07 v ǁvolume_forcesǁ 1.0691e-08 4.9547 0.54739 0.26937 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.25 291.14 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015177 5.3668e-05 2.9984e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.096608 0.6281 0.18724 0.15816 INSTANT 0.744399000E+00 TIME STEP NUMBER 773 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.54369E-05 0.22806E-02 Friction velocity uk : 0.54376E-05 0.22806E-02 Dimensionless distance yplus : 0.36212E-04 0.15173E-01 Friction thermal sca. tstar : -0.22640E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.25433E-04 0.10657E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.54369E-05 0.22806E-02 Friction velocity uk : 0.54376E-05 0.22806E-02 Dimensionless distance yplus : 0.36212E-04 0.15173E-01 Friction thermal sca. tstar : -0.22640E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.25433E-04 0.10657E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.36569E-08 3 0.12085E-06 0.21682E-12 0.93696E+00 c Velocity[X] 0.61589E-32 c Velocity[Y] 0.10841E-12 c Velocity[Z] 0.10841E-12 c Pressure 0.82791E-14 16 0.64379E-07 0.64379E-07 0.10266E+01 c k 0.32815E-06 2 0.35182E-07 0.17242E-08 0.13886E+01 c omega 0.13153E+02 1 0.11281E-08 0.20321E+00 0.23468E-02 c TempK 0.94702E+02 1 0.88317E-07 0.19980E-01 0.15646E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.3945e-14 7.8473e-14 -9.7414e-18 -2.5298e-18 v Velocity[Y] -0.00012397 0.00011752 -6.4094e-10 -3.4523e-12 v Velocity[Z] -0.00011748 0.00012397 3.657e-10 -2.0319e-12 v ǁVelocityǁ 3.0552e-10 0.00013293 1.1076e-05 7.8311e-06 v Pressure -0.0013039 0.022387 0.0012702 1.1962e-20 v k 7.4976e-10 0.0010872 0.00071754 0.00091236 v omega 13.829 1.0313e+05 2665.6 498.76 v TempK 288 342.06 294.05 291 v Density 1.205 1.205 1.205 1.205 v TurbVisc 8.7905e-15 9.4747e-05 5.6997e-05 7.4397e-05 v CourantNb 2.8463e-09 0.00019815 1.3799e-05 8.4726e-06 v FourierNb 0.096503 0.6281 0.18719 0.15811 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9537 4.9537 0.00054114 -5.5198e-07 v volume_forces[Z] -4.9537 4.9537 -0.00054102 6.5639e-07 v ǁvolume_forcesǁ 1.0866e-08 4.9548 0.5476 0.26954 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.25 291.14 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015173 5.3654e-05 2.9976e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.096522 0.6281 0.1872 0.15812 INSTANT 0.745362000E+00 TIME STEP NUMBER 774 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.53213E-05 0.22800E-02 Friction velocity uk : 0.53220E-05 0.22800E-02 Dimensionless distance yplus : 0.35442E-04 0.15169E-01 Friction thermal sca. tstar : -0.24089E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.24892E-04 0.10654E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.53213E-05 0.22800E-02 Friction velocity uk : 0.53220E-05 0.22800E-02 Dimensionless distance yplus : 0.35442E-04 0.15169E-01 Friction thermal sca. tstar : -0.24089E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.24892E-04 0.10654E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.36583E-08 3 0.12056E-06 0.21639E-12 0.93591E+00 c Velocity[X] 0.61338E-32 c Velocity[Y] 0.10819E-12 c Velocity[Z] 0.10820E-12 c Pressure 0.82631E-14 16 0.64253E-07 0.64253E-07 0.10252E+01 c k 0.32772E-06 2 0.35121E-07 0.17160E-08 0.13871E+01 c omega 0.13153E+02 1 0.11251E-08 0.20230E+00 0.23416E-02 c TempK 0.94702E+02 1 0.88155E-07 0.19942E-01 0.15630E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.3888e-14 7.8427e-14 -9.736e-18 -2.5285e-18 v Velocity[Y] -0.00012394 0.00011749 -6.3867e-10 -3.4472e-12 v Velocity[Z] -0.00011744 0.00012394 3.6326e-10 -2.0321e-12 v ǁVelocityǁ 3.1056e-10 0.0001329 1.1079e-05 7.8372e-06 v Pressure -0.0013056 0.022401 0.0012711 3.1475e-20 v k 7.4719e-10 0.0010859 0.00071653 0.00091112 v omega 13.813 1.0313e+05 2665.6 498.75 v TempK 288 342.07 294.05 291 v Density 1.205 1.205 1.205 1.205 v TurbVisc 8.7604e-15 9.4736e-05 5.6978e-05 7.4375e-05 v CourantNb 2.8492e-09 0.00019805 1.3799e-05 8.4762e-06 v FourierNb 0.096417 0.6281 0.18715 0.15807 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9537 4.9538 0.00054135 -5.5227e-07 v volume_forces[Z] -4.9537 4.9538 -0.00054124 6.5671e-07 v ǁvolume_forcesǁ 1.1045e-08 4.9548 0.5478 0.26972 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.26 291.15 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015169 5.364e-05 2.9968e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.096437 0.6281 0.18716 0.15808 INSTANT 0.746325000E+00 TIME STEP NUMBER 775 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.52027E-05 0.22795E-02 Friction velocity uk : 0.52035E-05 0.22794E-02 Dimensionless distance yplus : 0.34653E-04 0.15165E-01 Friction thermal sca. tstar : -0.25856E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.24338E-04 0.10651E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.52027E-05 0.22795E-02 Friction velocity uk : 0.52035E-05 0.22794E-02 Dimensionless distance yplus : 0.34653E-04 0.15165E-01 Friction thermal sca. tstar : -0.25856E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.24338E-04 0.10651E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.36597E-08 3 0.12027E-06 0.21595E-12 0.93486E+00 c Velocity[X] 0.61089E-32 c Velocity[Y] 0.10798E-12 c Velocity[Z] 0.10798E-12 c Pressure 0.82502E-14 16 0.64152E-07 0.64152E-07 0.10238E+01 c k 0.32729E-06 2 0.35060E-07 0.17079E-08 0.13856E+01 c omega 0.13153E+02 1 0.11220E-08 0.20140E+00 0.23364E-02 c TempK 0.94703E+02 1 0.87993E-07 0.19903E-01 0.15615E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.3832e-14 7.8381e-14 -9.7305e-18 -2.5272e-18 v Velocity[Y] -0.00012391 0.00011746 -6.364e-10 -3.442e-12 v Velocity[Z] -0.00011741 0.00012391 3.6083e-10 -2.0323e-12 v ǁVelocityǁ 3.1569e-10 0.00013287 1.1083e-05 7.8433e-06 v Pressure -0.0013073 0.022415 0.0012721 1.8346e-19 v k 7.4463e-10 0.0010846 0.00071553 0.00090988 v omega 13.798 1.0313e+05 2665.6 498.73 v TempK 288 342.07 294.05 291.01 v Density 1.205 1.205 1.205 1.205 v TurbVisc 8.7303e-15 9.4725e-05 5.6959e-05 7.4353e-05 v CourantNb 2.852e-09 0.00019795 1.3799e-05 8.4797e-06 v FourierNb 0.096332 0.6281 0.18711 0.15804 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9538 4.9538 0.00054156 -5.5256e-07 v volume_forces[Z] -4.9538 4.9538 -0.00054145 6.5703e-07 v ǁvolume_forcesǁ 1.1227e-08 4.9549 0.54801 0.26989 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.26 291.15 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015165 5.3626e-05 2.9959e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.096351 0.6281 0.18713 0.15804 INSTANT 0.747288000E+00 TIME STEP NUMBER 776 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.50812E-05 0.22789E-02 Friction velocity uk : 0.50819E-05 0.22788E-02 Dimensionless distance yplus : 0.33843E-04 0.15162E-01 Friction thermal sca. tstar : -0.28079E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.23769E-04 0.10648E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.50812E-05 0.22789E-02 Friction velocity uk : 0.50819E-05 0.22788E-02 Dimensionless distance yplus : 0.33843E-04 0.15162E-01 Friction thermal sca. tstar : -0.28079E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.23769E-04 0.10648E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.36611E-08 3 0.12002E-06 0.21552E-12 0.93381E+00 c Velocity[X] 0.60840E-32 c Velocity[Y] 0.10776E-12 c Velocity[Z] 0.10776E-12 c Pressure 0.82375E-14 16 0.64053E-07 0.64053E-07 0.10224E+01 c k 0.32686E-06 2 0.34999E-07 0.16997E-08 0.13841E+01 c omega 0.13153E+02 1 0.11190E-08 0.20050E+00 0.23311E-02 c TempK 0.94703E+02 1 0.87832E-07 0.19865E-01 0.15600E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.3775e-14 7.8336e-14 -9.7251e-18 -2.5259e-18 v Velocity[Y] -0.00012388 0.00011742 -6.3413e-10 -3.4369e-12 v Velocity[Z] -0.00011738 0.00012389 3.5839e-10 -2.0325e-12 v ǁVelocityǁ 3.2091e-10 0.00013284 1.1087e-05 7.8494e-06 v Pressure -0.0013089 0.022429 0.0012731 -9.7955e-20 v k 7.4208e-10 0.0010833 0.00071452 0.00090865 v omega 13.783 1.0313e+05 2665.5 498.72 v TempK 288 342.07 294.05 291.01 v Density 1.205 1.205 1.205 1.205 v TurbVisc 8.7005e-15 9.4715e-05 5.6941e-05 7.4331e-05 v CourantNb 2.8549e-09 0.00019786 1.3799e-05 8.4832e-06 v FourierNb 0.096247 0.6281 0.18707 0.158 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9538 4.9539 0.00054177 -5.5285e-07 v volume_forces[Z] -4.9538 4.9539 -0.00054166 6.5734e-07 v ǁvolume_forcesǁ 1.1412e-08 4.9549 0.54822 0.27006 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.26 291.15 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015162 5.3612e-05 2.9951e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.096266 0.6281 0.18709 0.15801 INSTANT 0.748251000E+00 TIME STEP NUMBER 777 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.49562E-05 0.22783E-02 Friction velocity uk : 0.49570E-05 0.22783E-02 Dimensionless distance yplus : 0.33012E-04 0.15158E-01 Friction thermal sca. tstar : -0.30996E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.23185E-04 0.10646E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.49562E-05 0.22783E-02 Friction velocity uk : 0.49570E-05 0.22783E-02 Dimensionless distance yplus : 0.33012E-04 0.15158E-01 Friction thermal sca. tstar : -0.30996E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.23185E-04 0.10646E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.36625E-08 3 0.11969E-06 0.21509E-12 0.93276E+00 c Velocity[X] 0.60594E-32 c Velocity[Y] 0.10754E-12 c Velocity[Z] 0.10755E-12 c Pressure 0.82152E-14 16 0.63879E-07 0.63879E-07 0.10210E+01 c k 0.32643E-06 2 0.34939E-07 0.16917E-08 0.13827E+01 c omega 0.13153E+02 1 0.11160E-08 0.19961E+00 0.23259E-02 c TempK 0.94704E+02 1 0.87672E-07 0.19826E-01 0.15585E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.3719e-14 7.829e-14 -9.7197e-18 -2.5247e-18 v Velocity[Y] -0.00012385 0.00011739 -6.3186e-10 -3.4318e-12 v Velocity[Z] -0.00011735 0.00012386 3.5595e-10 -2.0326e-12 v ǁVelocityǁ 3.2183e-10 0.00013281 1.1091e-05 7.8555e-06 v Pressure -0.0013106 0.022444 0.0012741 -3.9711e-20 v k 7.3955e-10 0.001082 0.00071352 0.00090742 v omega 13.769 1.0313e+05 2665.5 498.71 v TempK 288 342.07 294.05 291.01 v Density 1.205 1.205 1.205 1.205 v TurbVisc 8.6707e-15 9.4704e-05 5.6922e-05 7.431e-05 v CourantNb 2.8577e-09 0.00019776 1.3799e-05 8.4867e-06 v FourierNb 0.096162 0.6281 0.18704 0.15796 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9539 4.9539 0.00054198 -5.5313e-07 v volume_forces[Z] -4.9539 4.9539 -0.00054187 6.5766e-07 v ǁvolume_forcesǁ 1.1601e-08 4.955 0.54843 0.27024 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.26 291.15 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015158 5.3598e-05 2.9943e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.096181 0.6281 0.18705 0.15797 INSTANT 0.749214000E+00 TIME STEP NUMBER 778 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.48278E-05 0.22777E-02 Friction velocity uk : 0.48286E-05 0.22777E-02 Dimensionless distance yplus : 0.32156E-04 0.15154E-01 Friction thermal sca. tstar : -0.35061E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.22584E-04 0.10643E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.48278E-05 0.22777E-02 Friction velocity uk : 0.48286E-05 0.22777E-02 Dimensionless distance yplus : 0.32156E-04 0.15154E-01 Friction thermal sca. tstar : -0.35061E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.22584E-04 0.10643E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.36639E-08 3 0.11941E-06 0.21466E-12 0.93171E+00 c Velocity[X] 0.60347E-32 c Velocity[Y] 0.10733E-12 c Velocity[Z] 0.10733E-12 c Pressure 0.82009E-14 16 0.63766E-07 0.63766E-07 0.10197E+01 c k 0.32601E-06 2 0.34879E-07 0.16836E-08 0.13812E+01 c omega 0.13153E+02 1 0.11130E-08 0.19872E+00 0.23208E-02 c TempK 0.94704E+02 1 0.87512E-07 0.19788E-01 0.15570E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.3662e-14 7.8245e-14 -9.7143e-18 -2.5234e-18 v Velocity[Y] -0.00012383 0.00011736 -6.2958e-10 -3.4267e-12 v Velocity[Z] -0.00011731 0.00012383 3.5351e-10 -2.0328e-12 v ǁVelocityǁ 3.1815e-10 0.00013278 1.1094e-05 7.8617e-06 v Pressure -0.0013123 0.022458 0.001275 9.315e-20 v k 7.3703e-10 0.0010807 0.00071252 0.00090619 v omega 13.754 1.0313e+05 2665.5 498.69 v TempK 288 342.07 294.06 291.01 v Density 1.205 1.205 1.205 1.205 v TurbVisc 8.6411e-15 9.4693e-05 5.6904e-05 7.4288e-05 v CourantNb 2.8605e-09 0.00019767 1.38e-05 8.4903e-06 v FourierNb 0.096077 0.6281 0.187 0.15792 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9539 4.954 0.00054219 -5.5342e-07 v volume_forces[Z] -4.9539 4.954 -0.00054208 6.5798e-07 v ǁvolume_forcesǁ 1.1634e-08 4.955 0.54864 0.27041 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.27 291.15 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015154 5.3584e-05 2.9934e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.096097 0.6281 0.18701 0.15793 INSTANT 0.750177000E+00 TIME STEP NUMBER 779 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.46954E-05 0.22772E-02 Friction velocity uk : 0.46963E-05 0.22771E-02 Dimensionless distance yplus : 0.31275E-04 0.15150E-01 Friction thermal sca. tstar : -0.41306E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.21966E-04 0.10640E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.46954E-05 0.22772E-02 Friction velocity uk : 0.46963E-05 0.22771E-02 Dimensionless distance yplus : 0.31275E-04 0.15150E-01 Friction thermal sca. tstar : -0.41306E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.21966E-04 0.10640E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.36653E-08 3 0.11912E-06 0.21422E-12 0.93066E+00 c Velocity[X] 0.60103E-32 c Velocity[Y] 0.10711E-12 c Velocity[Z] 0.10711E-12 c Pressure 0.81851E-14 16 0.63643E-07 0.63643E-07 0.10183E+01 c k 0.32558E-06 2 0.34819E-07 0.16756E-08 0.13797E+01 c omega 0.13153E+02 1 0.11100E-08 0.19784E+00 0.23156E-02 c TempK 0.94705E+02 1 0.87353E-07 0.19750E-01 0.15555E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.3606e-14 7.8199e-14 -9.7089e-18 -2.5221e-18 v Velocity[Y] -0.0001238 0.00011733 -6.273e-10 -3.4216e-12 v Velocity[Z] -0.00011728 0.0001238 3.5107e-10 -2.0329e-12 v ǁVelocityǁ 3.1463e-10 0.00013275 1.1098e-05 7.8678e-06 v Pressure -0.0013139 0.022472 0.001276 -7.1284e-20 v k 7.3452e-10 0.0010794 0.00071152 0.00090497 v omega 13.739 1.0313e+05 2665.5 498.68 v TempK 288 342.07 294.06 291.01 v Density 1.205 1.205 1.205 1.205 v TurbVisc 8.6117e-15 9.4682e-05 5.6885e-05 7.4266e-05 v CourantNb 2.8634e-09 0.00019757 1.38e-05 8.4938e-06 v FourierNb 0.095993 0.6281 0.18696 0.15788 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.954 4.954 0.0005424 -5.537e-07 v volume_forces[Z] -4.954 4.954 -0.00054229 6.5829e-07 v ǁvolume_forcesǁ 1.1501e-08 4.9551 0.54885 0.27058 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.27 291.16 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.01515 5.357e-05 2.9926e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.096012 0.6281 0.18698 0.15789 INSTANT 0.751140000E+00 TIME STEP NUMBER 780 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.45589E-05 0.22766E-02 Friction velocity uk : 0.45598E-05 0.22766E-02 Dimensionless distance yplus : 0.30366E-04 0.15146E-01 Friction thermal sca. tstar : -0.52794E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.21327E-04 0.10638E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.45589E-05 0.22766E-02 Friction velocity uk : 0.45598E-05 0.22766E-02 Dimensionless distance yplus : 0.30366E-04 0.15146E-01 Friction thermal sca. tstar : -0.52794E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.21327E-04 0.10638E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.36667E-08 3 0.11885E-06 0.21379E-12 0.92961E+00 c Velocity[X] 0.59859E-32 c Velocity[Y] 0.10689E-12 c Velocity[Z] 0.10690E-12 c Pressure 0.81744E-14 16 0.63558E-07 0.63558E-07 0.10169E+01 c k 0.32516E-06 2 0.34759E-07 0.16677E-08 0.13783E+01 c omega 0.13153E+02 1 0.11070E-08 0.19696E+00 0.23104E-02 c TempK 0.94706E+02 1 0.87194E-07 0.19712E-01 0.15540E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.355e-14 7.8154e-14 -9.7035e-18 -2.5208e-18 v Velocity[Y] -0.00012377 0.00011729 -6.2502e-10 -3.4166e-12 v Velocity[Z] -0.00011725 0.00012378 3.4862e-10 -2.0331e-12 v ǁVelocityǁ 3.113e-10 0.00013272 1.1102e-05 7.8739e-06 v Pressure -0.0013156 0.022486 0.001277 -4.432e-20 v k 7.3202e-10 0.0010781 0.00071053 0.00090375 v omega 13.724 1.0313e+05 2665.5 498.67 v TempK 288 342.07 294.06 291.02 v Density 1.205 1.205 1.205 1.205 v TurbVisc 8.5823e-15 9.4672e-05 5.6867e-05 7.4245e-05 v CourantNb 2.8662e-09 0.00019748 1.38e-05 8.4973e-06 v FourierNb 0.095909 0.6281 0.18693 0.15785 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.954 4.9541 0.00054261 -5.5399e-07 v volume_forces[Z] -4.954 4.9541 -0.00054249 6.5861e-07 v ǁvolume_forcesǁ 1.1374e-08 4.9551 0.54905 0.27076 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.27 291.16 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015146 5.3556e-05 2.9917e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.095928 0.6281 0.18694 0.15786 INSTANT 0.752103000E+00 TIME STEP NUMBER 781 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.44178E-05 0.22760E-02 Friction velocity uk : 0.44187E-05 0.22760E-02 Dimensionless distance yplus : 0.29426E-04 0.15142E-01 Friction thermal sca. tstar : -0.87199E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.20667E-04 0.10635E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.44178E-05 0.22760E-02 Friction velocity uk : 0.44187E-05 0.22760E-02 Dimensionless distance yplus : 0.29426E-04 0.15142E-01 Friction thermal sca. tstar : -0.87199E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.20667E-04 0.10635E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.36681E-08 3 0.11858E-06 0.21336E-12 0.92856E+00 c Velocity[X] 0.59618E-32 c Velocity[Y] 0.10668E-12 c Velocity[Z] 0.10668E-12 c Pressure 0.81788E-14 16 0.63592E-07 0.63592E-07 0.10156E+01 c k 0.32473E-06 2 0.34699E-07 0.16598E-08 0.13768E+01 c omega 0.13153E+02 1 0.11041E-08 0.19608E+00 0.23053E-02 c TempK 0.94706E+02 1 0.87035E-07 0.19674E-01 0.15525E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.3494e-14 7.8109e-14 -9.6981e-18 -2.5195e-18 v Velocity[Y] -0.00012374 0.00011726 -6.2273e-10 -3.4116e-12 v Velocity[Z] -0.00011722 0.00012375 3.4617e-10 -2.0332e-12 v ǁVelocityǁ 3.0815e-10 0.00013269 1.1105e-05 7.88e-06 v Pressure -0.0013172 0.0225 0.001278 5.8832e-22 v k 7.2953e-10 0.0010768 0.00070954 0.00090253 v omega 13.709 1.0313e+05 2665.5 498.65 v TempK 288 342.07 294.06 291.02 v Density 1.205 1.205 1.205 1.205 v TurbVisc 8.5532e-15 9.4661e-05 5.6848e-05 7.4223e-05 v CourantNb 2.869e-09 0.00019739 1.38e-05 8.5009e-06 v FourierNb 0.095825 0.6281 0.18689 0.15781 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9541 4.9541 0.00054282 -5.5428e-07 v volume_forces[Z] -4.9541 4.9541 -0.0005427 6.5892e-07 v ǁvolume_forcesǁ 1.1254e-08 4.9552 0.54926 0.27093 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.27 291.16 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015142 5.3542e-05 2.9909e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.095844 0.6281 0.1869 0.15782 INSTANT 0.753066000E+00 TIME STEP NUMBER 782 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.42716E-05 0.22755E-02 Friction velocity uk : 0.42725E-05 0.22754E-02 Dimensionless distance yplus : 0.28453E-04 0.15139E-01 Friction thermal sca. tstar : -0.10222E+05 0.00000E+00 Dim-less thermal sca. tplus : 0.19984E-04 0.10632E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.42716E-05 0.22755E-02 Friction velocity uk : 0.42725E-05 0.22754E-02 Dimensionless distance yplus : 0.28453E-04 0.15139E-01 Friction thermal sca. tstar : -0.10222E+05 0.00000E+00 Dim-less thermal sca. tplus : 0.19984E-04 0.10632E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.36695E-08 3 0.11830E-06 0.21293E-12 0.92751E+00 c Velocity[X] 0.59378E-32 c Velocity[Y] 0.10646E-12 c Velocity[Z] 0.10647E-12 c Pressure 0.81620E-14 16 0.63460E-07 0.63460E-07 0.10142E+01 c k 0.32431E-06 2 0.34640E-07 0.16520E-08 0.13753E+01 c omega 0.13153E+02 1 0.11011E-08 0.19522E+00 0.23002E-02 c TempK 0.94707E+02 1 0.86877E-07 0.19637E-01 0.15510E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.3438e-14 7.8064e-14 -9.6927e-18 -2.5183e-18 v Velocity[Y] -0.00012372 0.00011723 -6.2044e-10 -3.4066e-12 v Velocity[Z] -0.00011718 0.00012372 3.4372e-10 -2.0334e-12 v ǁVelocityǁ 3.052e-10 0.00013266 1.1109e-05 7.8861e-06 v Pressure -0.0013189 0.022514 0.0012789 4.7261e-20 v k 7.2706e-10 0.0010755 0.00070855 0.00090131 v omega 13.694 1.0313e+05 2665.5 498.64 v TempK 288 342.07 294.07 291.02 v Density 1.205 1.205 1.205 1.205 v TurbVisc 8.5241e-15 9.465e-05 5.683e-05 7.4201e-05 v CourantNb 2.8718e-09 0.00019729 1.3801e-05 8.5044e-06 v FourierNb 0.095741 0.6281 0.18685 0.15777 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9541 4.9542 0.00054303 -5.5456e-07 v volume_forces[Z] -4.9541 4.9542 -0.00054291 6.5923e-07 v ǁvolume_forcesǁ 1.114e-08 4.9552 0.54947 0.2711 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.28 291.16 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015139 5.3528e-05 2.99e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.095761 0.6281 0.18687 0.15778 INSTANT 0.754029000E+00 TIME STEP NUMBER 783 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.41199E-05 0.22749E-02 Friction velocity uk : 0.41208E-05 0.22748E-02 Dimensionless distance yplus : 0.27443E-04 0.15135E-01 Friction thermal sca. tstar : -0.88616E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.19274E-04 0.10630E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.41199E-05 0.22749E-02 Friction velocity uk : 0.41208E-05 0.22748E-02 Dimensionless distance yplus : 0.27443E-04 0.15135E-01 Friction thermal sca. tstar : -0.88616E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.19274E-04 0.10630E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.36710E-08 3 0.11800E-06 0.21250E-12 0.92646E+00 c Velocity[X] 0.59138E-32 c Velocity[Y] 0.10625E-12 c Velocity[Z] 0.10625E-12 c Pressure 0.81257E-14 16 0.63178E-07 0.63178E-07 0.10128E+01 c k 0.32389E-06 2 0.34580E-07 0.16442E-08 0.13739E+01 c omega 0.13153E+02 1 0.10982E-08 0.19435E+00 0.22951E-02 c TempK 0.94707E+02 1 0.86720E-07 0.19599E-01 0.15495E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.3382e-14 7.8019e-14 -9.6874e-18 -2.517e-18 v Velocity[Y] -0.00012369 0.0001172 -6.1815e-10 -3.4016e-12 v Velocity[Z] -0.00011715 0.00012369 3.4127e-10 -2.0335e-12 v ǁVelocityǁ 3.0245e-10 0.00013263 1.1113e-05 7.8922e-06 v Pressure -0.0013206 0.022528 0.0012799 1.0815e-19 v k 7.246e-10 0.0010742 0.00070756 0.0009001 v omega 13.679 1.0313e+05 2665.5 498.63 v TempK 288 342.07 294.07 291.02 v Density 1.205 1.205 1.205 1.205 v TurbVisc 8.4952e-15 9.4639e-05 5.6811e-05 7.418e-05 v CourantNb 2.8747e-09 0.0001972 1.3801e-05 8.5079e-06 v FourierNb 0.095658 0.6281 0.18681 0.15773 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9542 4.9542 0.00054324 -5.5484e-07 v volume_forces[Z] -4.9542 4.9542 -0.00054312 6.5955e-07 v ǁvolume_forcesǁ 1.1033e-08 4.9553 0.54968 0.27127 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.28 291.16 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015135 5.3515e-05 2.9892e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.095677 0.6281 0.18683 0.15774 INSTANT 0.754992000E+00 TIME STEP NUMBER 784 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.39619E-05 0.22743E-02 Friction velocity uk : 0.39629E-05 0.22743E-02 Dimensionless distance yplus : 0.26391E-04 0.15131E-01 Friction thermal sca. tstar : -0.53170E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.18535E-04 0.10627E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.39619E-05 0.22743E-02 Friction velocity uk : 0.39629E-05 0.22743E-02 Dimensionless distance yplus : 0.26391E-04 0.15131E-01 Friction thermal sca. tstar : -0.53170E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.18535E-04 0.10627E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.36724E-08 3 0.11774E-06 0.21207E-12 0.92541E+00 c Velocity[X] 0.58901E-32 c Velocity[Y] 0.10604E-12 c Velocity[Z] 0.10604E-12 c Pressure 0.81211E-14 16 0.63141E-07 0.63141E-07 0.10115E+01 c k 0.32347E-06 2 0.34521E-07 0.16364E-08 0.13724E+01 c omega 0.13153E+02 1 0.10952E-08 0.19349E+00 0.22900E-02 c TempK 0.94708E+02 1 0.86563E-07 0.19562E-01 0.15480E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.3327e-14 7.7974e-14 -9.682e-18 -2.5157e-18 v Velocity[Y] -0.00012366 0.00011717 -6.1585e-10 -3.3966e-12 v Velocity[Z] -0.00011712 0.00012367 3.3882e-10 -2.0337e-12 v ǁVelocityǁ 2.999e-10 0.0001326 1.1117e-05 7.8983e-06 v Pressure -0.0013222 0.022542 0.0012809 1.1423e-19 v k 7.2214e-10 0.001073 0.00070657 0.00089889 v omega 13.665 1.0313e+05 2665.5 498.61 v TempK 288 342.07 294.07 291.02 v Density 1.205 1.205 1.205 1.205 v TurbVisc 8.4664e-15 9.4629e-05 5.6793e-05 7.4158e-05 v CourantNb 2.8775e-09 0.0001971 1.3801e-05 8.5115e-06 v FourierNb 0.095574 0.6281 0.18678 0.1577 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9542 4.9543 0.00054345 -5.5513e-07 v volume_forces[Z] -4.9542 4.9543 -0.00054333 6.5986e-07 v ǁvolume_forcesǁ 1.0933e-08 4.9553 0.54988 0.27145 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.28 291.17 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015131 5.3503e-05 2.9885e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.095594 0.6281 0.18679 0.1577 INSTANT 0.755955000E+00 TIME STEP NUMBER 785 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.37970E-05 0.22738E-02 Friction velocity uk : 0.37980E-05 0.22737E-02 Dimensionless distance yplus : 0.25293E-04 0.15127E-01 Friction thermal sca. tstar : -0.41521E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.17764E-04 0.10624E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.37970E-05 0.22738E-02 Friction velocity uk : 0.37980E-05 0.22737E-02 Dimensionless distance yplus : 0.25293E-04 0.15127E-01 Friction thermal sca. tstar : -0.41521E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.17764E-04 0.10624E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.36738E-08 3 0.11900E-06 0.21165E-12 0.92436E+00 c Velocity[X] 0.58664E-32 c Velocity[Y] 0.10582E-12 c Velocity[Z] 0.10582E-12 c Pressure 0.80950E-14 16 0.62937E-07 0.62937E-07 0.10101E+01 c k 0.32305E-06 2 0.34462E-07 0.16287E-08 0.13710E+01 c omega 0.13153E+02 1 0.10923E-08 0.19264E+00 0.22850E-02 c TempK 0.94708E+02 1 0.86406E-07 0.19524E-01 0.15465E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.3271e-14 7.793e-14 -9.6767e-18 -2.5144e-18 v Velocity[Y] -0.00012364 0.00011713 -6.1356e-10 -3.3917e-12 v Velocity[Z] -0.00011709 0.00012364 3.3637e-10 -2.0338e-12 v ǁVelocityǁ 2.9758e-10 0.00013257 1.112e-05 7.9044e-06 v Pressure -0.0013239 0.022556 0.0012819 -6.5107e-20 v k 7.197e-10 0.0010717 0.00070559 0.00089768 v omega 13.65 1.0313e+05 2665.5 498.6 v TempK 288 342.07 294.07 291.03 v Density 1.205 1.205 1.205 1.205 v TurbVisc 8.4377e-15 9.4618e-05 5.6775e-05 7.4137e-05 v CourantNb 2.8803e-09 0.00019701 1.3801e-05 8.515e-06 v FourierNb 0.095491 0.6281 0.18674 0.15766 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9543 4.9543 0.00054365 -5.5541e-07 v volume_forces[Z] -4.9543 4.9543 -0.00054354 6.6017e-07 v ǁvolume_forcesǁ 1.0842e-08 4.9554 0.55009 0.27162 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.28 291.17 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015127 5.349e-05 2.9877e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.095511 0.6281 0.18675 0.15767 INSTANT 0.756918000E+00 TIME STEP NUMBER 786 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.36241E-05 0.22732E-02 Friction velocity uk : 0.36251E-05 0.22731E-02 Dimensionless distance yplus : 0.24142E-04 0.15124E-01 Friction thermal sca. tstar : -0.35217E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.16956E-04 0.10622E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.36241E-05 0.22732E-02 Friction velocity uk : 0.36251E-05 0.22731E-02 Dimensionless distance yplus : 0.24142E-04 0.15124E-01 Friction thermal sca. tstar : -0.35217E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.16956E-04 0.10622E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.36752E-08 3 0.11717E-06 0.21122E-12 0.92331E+00 c Velocity[X] 0.58429E-32 c Velocity[Y] 0.10561E-12 c Velocity[Z] 0.10561E-12 c Pressure 0.80756E-14 16 0.62785E-07 0.62785E-07 0.10088E+01 c k 0.32263E-06 2 0.34403E-07 0.16211E-08 0.13695E+01 c omega 0.13153E+02 1 0.10894E-08 0.19179E+00 0.22799E-02 c TempK 0.94709E+02 1 0.86250E-07 0.19487E-01 0.15450E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.3216e-14 7.7885e-14 -9.6714e-18 -2.5132e-18 v Velocity[Y] -0.00012361 0.0001171 -6.1126e-10 -3.3867e-12 v Velocity[Z] -0.00011706 0.00012361 3.3391e-10 -2.0339e-12 v ǁVelocityǁ 2.9547e-10 0.00013254 1.1124e-05 7.9105e-06 v Pressure -0.0013256 0.02257 0.0012828 -2.8043e-20 v k 7.1727e-10 0.0010704 0.00070461 0.00089648 v omega 13.635 1.0313e+05 2665.4 498.59 v TempK 288 342.07 294.08 291.03 v Density 1.205 1.205 1.205 1.205 v TurbVisc 8.4092e-15 9.4607e-05 5.6756e-05 7.4115e-05 v CourantNb 2.8831e-09 0.00019692 1.3802e-05 8.5185e-06 v FourierNb 0.095409 0.6281 0.1867 0.15762 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9543 4.9544 0.00054386 -5.5569e-07 v volume_forces[Z] -4.9543 4.9544 -0.00054375 6.6048e-07 v ǁvolume_forcesǁ 1.0757e-08 4.9554 0.5503 0.27179 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.28 291.17 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015124 5.3477e-05 2.987e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.095428 0.6281 0.18672 0.15763 INSTANT 0.757881000E+00 TIME STEP NUMBER 787 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.34420E-05 0.22726E-02 Friction velocity uk : 0.34431E-05 0.22726E-02 Dimensionless distance yplus : 0.22930E-04 0.15120E-01 Friction thermal sca. tstar : -0.31122E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.16104E-04 0.10619E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.34420E-05 0.22726E-02 Friction velocity uk : 0.34431E-05 0.22726E-02 Dimensionless distance yplus : 0.22930E-04 0.15120E-01 Friction thermal sca. tstar : -0.31122E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.16104E-04 0.10619E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.36766E-08 3 0.11690E-06 0.21079E-12 0.92226E+00 c Velocity[X] 0.58194E-32 c Velocity[Y] 0.10539E-12 c Velocity[Z] 0.10540E-12 c Pressure 0.80603E-14 16 0.62665E-07 0.62665E-07 0.10075E+01 c k 0.32222E-06 2 0.34345E-07 0.16134E-08 0.13681E+01 c omega 0.13153E+02 1 0.10865E-08 0.19094E+00 0.22749E-02 c TempK 0.94709E+02 1 0.86095E-07 0.19450E-01 0.15435E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.316e-14 7.784e-14 -9.6661e-18 -2.5119e-18 v Velocity[Y] -0.00012358 0.00011707 -6.0895e-10 -3.3818e-12 v Velocity[Z] -0.00011702 0.00012359 3.3145e-10 -2.034e-12 v ǁVelocityǁ 2.936e-10 0.00013252 1.1128e-05 7.9166e-06 v Pressure -0.0013272 0.022584 0.0012838 7.148e-20 v k 7.1485e-10 0.0010692 0.00070363 0.00089528 v omega 13.621 1.0313e+05 2665.4 498.58 v TempK 288 342.07 294.08 291.03 v Density 1.205 1.205 1.205 1.205 v TurbVisc 8.3808e-15 9.4596e-05 5.6738e-05 7.4094e-05 v CourantNb 2.8859e-09 0.00019682 1.3802e-05 8.5221e-06 v FourierNb 0.095326 0.6281 0.18667 0.15758 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9544 4.9544 0.00054407 -5.5597e-07 v volume_forces[Z] -4.9544 4.9544 -0.00054396 6.6079e-07 v ǁvolume_forcesǁ 1.0681e-08 4.9555 0.5505 0.27196 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.29 291.17 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.01512 5.3465e-05 2.9862e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.095346 0.6281 0.18668 0.15759 INSTANT 0.758844000E+00 TIME STEP NUMBER 788 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.32493E-05 0.22721E-02 Friction velocity uk : 0.32505E-05 0.22720E-02 Dimensionless distance yplus : 0.21647E-04 0.15116E-01 Friction thermal sca. tstar : -0.28188E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.15203E-04 0.10617E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.32493E-05 0.22721E-02 Friction velocity uk : 0.32505E-05 0.22720E-02 Dimensionless distance yplus : 0.21647E-04 0.15116E-01 Friction thermal sca. tstar : -0.28188E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.15203E-04 0.10617E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.36780E-08 3 0.11662E-06 0.21036E-12 0.92121E+00 c Velocity[X] 0.57961E-32 c Velocity[Y] 0.10518E-12 c Velocity[Z] 0.10518E-12 c Pressure 0.80450E-14 16 0.62545E-07 0.62545E-07 0.10061E+01 c k 0.32180E-06 2 0.34286E-07 0.16059E-08 0.13666E+01 c omega 0.13153E+02 1 0.10836E-08 0.19010E+00 0.22699E-02 c TempK 0.94710E+02 1 0.85939E-07 0.19413E-01 0.15420E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.3105e-14 7.7796e-14 -9.6607e-18 -2.5107e-18 v Velocity[Y] -0.00012356 0.00011704 -6.0665e-10 -3.3769e-12 v Velocity[Z] -0.00011699 0.00012356 3.2899e-10 -2.0341e-12 v ǁVelocityǁ 2.9196e-10 0.00013249 1.1132e-05 7.9227e-06 v Pressure -0.0013289 0.022598 0.0012848 -1.0041e-19 v k 7.1244e-10 0.0010679 0.00070266 0.00089408 v omega 13.606 1.0313e+05 2665.4 498.56 v TempK 288 342.07 294.08 291.03 v Density 1.205 1.205 1.205 1.205 v TurbVisc 8.3525e-15 9.4586e-05 5.672e-05 7.4072e-05 v CourantNb 2.8887e-09 0.00019673 1.3802e-05 8.5256e-06 v FourierNb 0.095244 0.6281 0.18663 0.15755 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9544 4.9545 0.00054428 -5.5626e-07 v volume_forces[Z] -4.9544 4.9545 -0.00054416 6.611e-07 v ǁvolume_forcesǁ 1.0614e-08 4.9555 0.55071 0.27213 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.29 291.17 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015116 5.3452e-05 2.9854e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.095263 0.6281 0.18664 0.15755 INSTANT 0.759807000E+00 TIME STEP NUMBER 789 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.30439E-05 0.22715E-02 Friction velocity uk : 0.30451E-05 0.22715E-02 Dimensionless distance yplus : 0.20279E-04 0.15112E-01 Friction thermal sca. tstar : -0.25953E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.14243E-04 0.10614E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.30439E-05 0.22715E-02 Friction velocity uk : 0.30451E-05 0.22715E-02 Dimensionless distance yplus : 0.20279E-04 0.15112E-01 Friction thermal sca. tstar : -0.25953E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.14243E-04 0.10614E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.36794E-08 3 0.11634E-06 0.20994E-12 0.92016E+00 c Velocity[X] 0.57729E-32 c Velocity[Y] 0.10497E-12 c Velocity[Z] 0.10497E-12 c Pressure 0.80287E-14 16 0.62418E-07 0.62418E-07 0.10048E+01 c k 0.32138E-06 2 0.34228E-07 0.15983E-08 0.13652E+01 c omega 0.13153E+02 1 0.10807E-08 0.18926E+00 0.22649E-02 c TempK 0.94711E+02 1 0.85785E-07 0.19376E-01 0.15406E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.305e-14 7.7751e-14 -9.6555e-18 -2.5094e-18 v Velocity[Y] -0.00012353 0.00011701 -6.0419e-10 -3.2324e-12 v Velocity[Z] -0.00011696 0.00012353 3.2677e-10 -1.8107e-12 v ǁVelocityǁ 2.905e-10 0.00013246 1.1135e-05 7.9288e-06 v Pressure -0.0013306 0.022612 0.0012857 2.2552e-21 v k 7.1005e-10 0.0010666 0.00070168 0.00089289 v omega 13.592 1.0313e+05 2665.4 498.55 v TempK 288 342.07 294.08 291.03 v Density 1.205 1.205 1.205 1.205 v TurbVisc 8.3244e-15 9.4575e-05 5.6701e-05 7.4051e-05 v CourantNb 2.8914e-09 0.00019664 1.3802e-05 8.5291e-06 v FourierNb 0.095162 0.6281 0.18659 0.15751 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9545 4.9545 0.00054449 -5.5654e-07 v volume_forces[Z] -4.9545 4.9545 -0.00054437 6.6141e-07 v ǁvolume_forcesǁ 1.0554e-08 4.9556 0.55092 0.27231 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.29 291.17 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015112 5.3439e-05 2.9847e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.095181 0.6281 0.18661 0.15752 INSTANT 0.760770000E+00 TIME STEP NUMBER 790 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.28141E-05 0.22709E-02 Friction velocity uk : 0.28154E-05 0.22709E-02 Dimensionless distance yplus : 0.18750E-04 0.15109E-01 Friction thermal sca. tstar : -0.24179E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.13169E-04 0.10611E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.28141E-05 0.22709E-02 Friction velocity uk : 0.28154E-05 0.22709E-02 Dimensionless distance yplus : 0.18750E-04 0.15109E-01 Friction thermal sca. tstar : -0.24179E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.13169E-04 0.10611E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.36809E-08 3 0.11607E-06 0.20951E-12 0.91911E+00 c Velocity[X] 0.57498E-32 c Velocity[Y] 0.10476E-12 c Velocity[Z] 0.10476E-12 c Pressure 0.80141E-14 16 0.62303E-07 0.62303E-07 0.10034E+01 c k 0.32097E-06 2 0.34170E-07 0.15908E-08 0.13638E+01 c omega 0.13153E+02 1 0.10779E-08 0.18843E+00 0.22599E-02 c TempK 0.94711E+02 1 0.85631E-07 0.19339E-01 0.15391E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.2995e-14 7.7707e-14 -9.6502e-18 -2.5082e-18 v Velocity[Y] -0.0001235 0.00011698 -6.0187e-10 -3.2185e-12 v Velocity[Z] -0.00011693 0.00012351 3.243e-10 -1.8152e-12 v ǁVelocityǁ 2.8939e-10 0.00013243 1.1139e-05 7.9349e-06 v Pressure -0.0013322 0.022626 0.0012867 6.4617e-20 v k 7.0766e-10 0.0010654 0.00070071 0.00089169 v omega 13.577 1.0313e+05 2665.4 498.54 v TempK 288 342.07 294.08 291.04 v Density 1.205 1.205 1.205 1.205 v TurbVisc 8.2964e-15 9.4564e-05 5.6683e-05 7.4029e-05 v CourantNb 2.8942e-09 0.00019654 1.3803e-05 8.5326e-06 v FourierNb 0.09508 0.6281 0.18656 0.15747 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9545 4.9546 0.00054469 -5.5681e-07 v volume_forces[Z] -4.9545 4.9546 -0.00054458 6.6172e-07 v ǁvolume_forcesǁ 1.0502e-08 4.9556 0.55112 0.27248 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.29 291.18 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015109 5.3426e-05 2.9839e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.0951 0.6281 0.18657 0.15748 INSTANT 0.761733000E+00 TIME STEP NUMBER 791 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.25758E-05 0.22704E-02 Friction velocity uk : 0.25773E-05 0.22703E-02 Dimensionless distance yplus : 0.17164E-04 0.15105E-01 Friction thermal sca. tstar : -0.22725E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.12055E-04 0.10609E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.25758E-05 0.22704E-02 Friction velocity uk : 0.25773E-05 0.22703E-02 Dimensionless distance yplus : 0.17164E-04 0.15105E-01 Friction thermal sca. tstar : -0.22725E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.12055E-04 0.10609E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.36823E-08 3 0.11580E-06 0.20909E-12 0.91806E+00 c Velocity[X] 0.57269E-32 c Velocity[Y] 0.10454E-12 c Velocity[Z] 0.10455E-12 c Pressure 0.79991E-14 16 0.62186E-07 0.62186E-07 0.10021E+01 c k 0.32056E-06 2 0.34112E-07 0.15834E-08 0.13623E+01 c omega 0.13153E+02 1 0.10750E-08 0.18760E+00 0.22549E-02 c TempK 0.94712E+02 1 0.85477E-07 0.19303E-01 0.15376E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.294e-14 7.7663e-14 -9.6449e-18 -2.5069e-18 v Velocity[Y] -0.00012348 0.00011695 -5.9957e-10 -3.2184e-12 v Velocity[Z] -0.0001169 0.00012348 3.2184e-10 -1.8138e-12 v ǁVelocityǁ 2.885e-10 0.0001324 1.1143e-05 7.941e-06 v Pressure -0.0013339 0.02264 0.0012877 1.3727e-20 v k 7.0528e-10 0.0010641 0.00069974 0.0008905 v omega 13.563 1.0313e+05 2665.4 498.52 v TempK 288 342.07 294.09 291.04 v Density 1.205 1.205 1.205 1.205 v TurbVisc 8.2685e-15 9.4554e-05 5.6665e-05 7.4008e-05 v CourantNb 2.897e-09 0.00019645 1.3803e-05 8.5362e-06 v FourierNb 0.094999 0.6281 0.18652 0.15743 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9546 4.9546 0.0005449 -5.5709e-07 v volume_forces[Z] -4.9546 4.9546 -0.00054478 6.6203e-07 v ǁvolume_forcesǁ 1.0461e-08 4.9557 0.55133 0.27265 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.3 291.18 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015105 5.3413e-05 2.9831e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.095018 0.6281 0.18653 0.15744 INSTANT 0.762696000E+00 TIME STEP NUMBER 792 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.23111E-05 0.22698E-02 Friction velocity uk : 0.23128E-05 0.22698E-02 Dimensionless distance yplus : 0.15402E-04 0.15101E-01 Friction thermal sca. tstar : -0.21506E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.10818E-04 0.10606E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.23111E-05 0.22698E-02 Friction velocity uk : 0.23128E-05 0.22698E-02 Dimensionless distance yplus : 0.15402E-04 0.15101E-01 Friction thermal sca. tstar : -0.21506E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.10818E-04 0.10606E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.36837E-08 3 0.11554E-06 0.20866E-12 0.91701E+00 c Velocity[X] 0.57042E-32 c Velocity[Y] 0.10433E-12 c Velocity[Z] 0.10433E-12 c Pressure 0.80518E-14 16 0.62595E-07 0.62595E-07 0.10008E+01 c k 0.32014E-06 2 0.34054E-07 0.15760E-08 0.13609E+01 c omega 0.13153E+02 1 0.10722E-08 0.18678E+00 0.22500E-02 c TempK 0.94712E+02 1 0.85324E-07 0.19266E-01 0.15362E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.2885e-14 7.7619e-14 -9.6396e-18 -2.5057e-18 v Velocity[Y] -0.00012345 0.00011691 -5.9725e-10 -3.2136e-12 v Velocity[Z] -0.00011687 0.00012345 3.1937e-10 -1.8136e-12 v ǁVelocityǁ 2.8787e-10 0.00013237 1.1146e-05 7.9471e-06 v Pressure -0.0013356 0.022654 0.0012886 -5.0497e-20 v k 7.0292e-10 0.0010629 0.00069878 0.00088932 v omega 13.548 1.0313e+05 2665.4 498.51 v TempK 288 342.07 294.09 291.04 v Density 1.205 1.205 1.205 1.205 v TurbVisc 8.2407e-15 9.4543e-05 5.6646e-05 7.3987e-05 v CourantNb 2.8998e-09 0.00019636 1.3803e-05 8.5397e-06 v FourierNb 0.094917 0.6281 0.18648 0.1574 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9546 4.9547 0.00054511 -5.5737e-07 v volume_forces[Z] -4.9546 4.9547 -0.00054499 6.6233e-07 v ǁvolume_forcesǁ 1.0429e-08 4.9557 0.55153 0.27282 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.3 291.18 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015101 5.3401e-05 2.9823e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.094937 0.6281 0.1865 0.15741 INSTANT 0.763659000E+00 TIME STEP NUMBER 793 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.20100E-05 0.22692E-02 Friction velocity uk : 0.20120E-05 0.22692E-02 Dimensionless distance yplus : 0.13399E-04 0.15097E-01 Friction thermal sca. tstar : -0.20464E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.94104E-05 0.10603E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.20100E-05 0.22692E-02 Friction velocity uk : 0.20120E-05 0.22692E-02 Dimensionless distance yplus : 0.13399E-04 0.15097E-01 Friction thermal sca. tstar : -0.20464E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.94104E-05 0.10603E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.36851E-08 3 0.11526E-06 0.20824E-12 0.91596E+00 c Velocity[X] 0.56815E-32 c Velocity[Y] 0.10412E-12 c Velocity[Z] 0.10412E-12 c Pressure 0.79696E-14 16 0.61955E-07 0.61955E-07 0.99947E+00 c k 0.31973E-06 2 0.33996E-07 0.15686E-08 0.13595E+01 c omega 0.13153E+02 1 0.10693E-08 0.18596E+00 0.22450E-02 c TempK 0.94713E+02 1 0.85171E-07 0.19230E-01 0.15347E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.283e-14 7.7575e-14 -9.6344e-18 -2.5044e-18 v Velocity[Y] -0.00012342 0.00011688 -5.9493e-10 -3.2089e-12 v Velocity[Z] -0.00011684 0.00012343 3.169e-10 -1.814e-12 v ǁVelocityǁ 2.8749e-10 0.00013234 1.115e-05 7.9532e-06 v Pressure -0.0013372 0.022668 0.0012896 -6.5695e-21 v k 7.0056e-10 0.0010616 0.00069782 0.00088813 v omega 13.534 1.0313e+05 2665.4 498.5 v TempK 288 342.08 294.09 291.04 v Density 1.205 1.205 1.205 1.205 v TurbVisc 8.2131e-15 9.4533e-05 5.6628e-05 7.3965e-05 v CourantNb 2.9025e-09 0.00019627 1.3804e-05 8.5432e-06 v FourierNb 0.094836 0.6281 0.18645 0.15736 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9547 4.9547 0.00054531 -5.5765e-07 v volume_forces[Z] -4.9547 4.9547 -0.0005452 6.6264e-07 v ǁvolume_forcesǁ 1.0406e-08 4.9558 0.55174 0.27299 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.3 291.18 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015097 5.3388e-05 2.9816e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.094856 0.6281 0.18646 0.15737 INSTANT 0.764622000E+00 TIME STEP NUMBER 794 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.16536E-05 0.22687E-02 Friction velocity uk : 0.16559E-05 0.22686E-02 Dimensionless distance yplus : 0.11028E-04 0.15094E-01 Friction thermal sca. tstar : -0.19561E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.77452E-05 0.10601E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.16536E-05 0.22687E-02 Friction velocity uk : 0.16559E-05 0.22686E-02 Dimensionless distance yplus : 0.11028E-04 0.15094E-01 Friction thermal sca. tstar : -0.19561E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.77452E-05 0.10601E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.36866E-08 3 0.11498E-06 0.20782E-12 0.91491E+00 c Velocity[X] 0.56591E-32 c Velocity[Y] 0.10391E-12 c Velocity[Z] 0.10391E-12 c Pressure 0.79539E-14 16 0.61832E-07 0.61832E-07 0.99815E+00 c k 0.31932E-06 2 0.33939E-07 0.15613E-08 0.13581E+01 c omega 0.13153E+02 1 0.10665E-08 0.18515E+00 0.22401E-02 c TempK 0.94713E+02 1 0.85019E-07 0.19194E-01 0.15332E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.2776e-14 7.7531e-14 -9.6291e-18 -2.5032e-18 v Velocity[Y] -0.0001234 0.00011685 -5.9261e-10 -3.2042e-12 v Velocity[Z] -0.0001168 0.0001234 3.1443e-10 -1.8142e-12 v ǁVelocityǁ 2.8738e-10 0.00013231 1.1154e-05 7.9593e-06 v Pressure -0.0013389 0.022682 0.0012906 8.3933e-20 v k 6.9822e-10 0.0010604 0.00069685 0.00088695 v omega 13.519 1.0313e+05 2665.4 498.49 v TempK 288 342.08 294.09 291.04 v Density 1.205 1.205 1.205 1.205 v TurbVisc 8.1856e-15 9.4522e-05 5.661e-05 7.3944e-05 v CourantNb 2.9053e-09 0.00019617 1.3804e-05 8.5468e-06 v FourierNb 0.094755 0.6281 0.18641 0.15732 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9547 4.9548 0.00054552 -5.5793e-07 v volume_forces[Z] -4.9547 4.9548 -0.00054541 6.6295e-07 v ǁvolume_forcesǁ 1.0393e-08 4.9558 0.55194 0.27316 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.3 291.18 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015094 5.3375e-05 2.9808e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.094775 0.6281 0.18643 0.15733 INSTANT 0.765585000E+00 TIME STEP NUMBER 795 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11934E-05 0.22681E-02 Friction velocity uk : 0.11966E-05 0.22681E-02 Dimensionless distance yplus : 0.79690E-05 0.15090E-01 Friction thermal sca. tstar : -0.18768E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.55969E-05 0.10598E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11934E-05 0.22681E-02 Friction velocity uk : 0.11966E-05 0.22681E-02 Dimensionless distance yplus : 0.79690E-05 0.15090E-01 Friction thermal sca. tstar : -0.18768E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.55969E-05 0.10598E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.36880E-08 3 0.11474E-06 0.20739E-12 0.91386E+00 c Velocity[X] 0.56367E-32 c Velocity[Y] 0.10370E-12 c Velocity[Z] 0.10370E-12 c Pressure 0.79406E-14 16 0.61728E-07 0.61728E-07 0.99683E+00 c k 0.31891E-06 2 0.33881E-07 0.15540E-08 0.13566E+01 c omega 0.13153E+02 1 0.10637E-08 0.18434E+00 0.22352E-02 c TempK 0.94714E+02 1 0.84867E-07 0.19157E-01 0.15318E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.2721e-14 7.7487e-14 -9.6239e-18 -2.5019e-18 v Velocity[Y] -0.00012337 0.00011682 -5.9028e-10 -3.1995e-12 v Velocity[Z] -0.00011677 0.00012338 3.1196e-10 -1.8145e-12 v ǁVelocityǁ 2.8753e-10 0.00013228 1.1158e-05 7.9654e-06 v Pressure -0.0013405 0.022696 0.0012915 -5.5106e-20 v k 6.9589e-10 0.0010591 0.0006959 0.00088577 v omega 13.505 1.0313e+05 2665.4 498.47 v TempK 288 342.08 294.1 291.05 v Density 1.205 1.205 1.205 1.205 v TurbVisc 8.1582e-15 9.4511e-05 5.6592e-05 7.3923e-05 v CourantNb 2.908e-09 0.00019608 1.3804e-05 8.5503e-06 v FourierNb 0.094675 0.6281 0.18638 0.15729 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9548 4.9548 0.00054573 -5.5821e-07 v volume_forces[Z] -4.9548 4.9548 -0.00054561 6.6326e-07 v ǁvolume_forcesǁ 1.0389e-08 4.9559 0.55215 0.27333 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.31 291.19 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.01509 5.3362e-05 2.98e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.094694 0.6281 0.18639 0.15729 INSTANT 0.766548000E+00 TIME STEP NUMBER 796 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.38259E-06 0.22676E-02 Friction velocity uk : 0.39249E-06 0.22675E-02 Dimensionless distance yplus : 0.26138E-05 0.15086E-01 Friction thermal sca. tstar : -0.18065E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.18358E-05 0.10596E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.38259E-06 0.22676E-02 Friction velocity uk : 0.39249E-06 0.22675E-02 Dimensionless distance yplus : 0.26138E-05 0.15086E-01 Friction thermal sca. tstar : -0.18065E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.18358E-05 0.10596E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.36894E-08 3 0.11447E-06 0.20697E-12 0.91281E+00 c Velocity[X] 0.56146E-32 c Velocity[Y] 0.10348E-12 c Velocity[Z] 0.10349E-12 c Pressure 0.79258E-14 16 0.61612E-07 0.61612E-07 0.99552E+00 c k 0.31850E-06 2 0.33824E-07 0.15468E-08 0.13552E+01 c omega 0.13153E+02 1 0.10609E-08 0.18354E+00 0.22303E-02 c TempK 0.94714E+02 1 0.84715E-07 0.19121E-01 0.15303E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.2667e-14 7.7443e-14 -9.6187e-18 -2.5007e-18 v Velocity[Y] -0.00012334 0.00011679 -5.8796e-10 -3.1949e-12 v Velocity[Z] -0.00011674 0.00012335 3.0948e-10 -1.8148e-12 v ǁVelocityǁ 2.8794e-10 0.00013225 1.1161e-05 7.9714e-06 v Pressure -0.0013422 0.02271 0.0012925 8.0796e-20 v k 6.9357e-10 0.0010579 0.00069494 0.0008846 v omega 13.491 1.0313e+05 2665.3 498.46 v TempK 288 342.08 294.1 291.05 v Density 1.205 1.205 1.205 1.205 v TurbVisc 8.131e-15 9.4501e-05 5.6574e-05 7.3901e-05 v CourantNb 2.9108e-09 0.00019599 1.3804e-05 8.5538e-06 v FourierNb 0.094594 0.6281 0.18634 0.15725 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9548 4.9549 0.00054593 -5.5848e-07 v volume_forces[Z] -4.9548 4.9549 -0.00054582 6.6356e-07 v ǁvolume_forcesǁ 1.0394e-08 4.9559 0.55235 0.2735 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.31 291.19 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015086 5.3349e-05 2.9792e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.094614 0.6281 0.18635 0.15726 INSTANT 0.767511000E+00 TIME STEP NUMBER 797 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10954E-05 0.22670E-02 Friction velocity uk : 0.10989E-05 0.22670E-02 Dimensionless distance yplus : 0.73180E-05 0.15083E-01 Friction thermal sca. tstar : -0.17435E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.51397E-05 0.10593E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10954E-05 0.22670E-02 Friction velocity uk : 0.10989E-05 0.22670E-02 Dimensionless distance yplus : 0.73180E-05 0.15083E-01 Friction thermal sca. tstar : -0.17435E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.51397E-05 0.10593E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.36908E-08 3 0.11418E-06 0.20655E-12 0.91176E+00 c Velocity[X] 0.55924E-32 c Velocity[Y] 0.10327E-12 c Velocity[Z] 0.10328E-12 c Pressure 0.79091E-14 16 0.61481E-07 0.61481E-07 0.99421E+00 c k 0.31810E-06 2 0.33767E-07 0.15396E-08 0.13538E+01 c omega 0.13153E+02 1 0.10581E-08 0.18274E+00 0.22255E-02 c TempK 0.94715E+02 1 0.84564E-07 0.19085E-01 0.15289E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.2612e-14 7.7399e-14 -9.6135e-18 -2.4995e-18 v Velocity[Y] -0.00012332 0.00011676 -5.8563e-10 -3.1902e-12 v Velocity[Z] -0.00011671 0.00012332 3.0701e-10 -1.815e-12 v ǁVelocityǁ 2.8863e-10 0.00013223 1.1165e-05 7.9775e-06 v Pressure -0.0013439 0.022724 0.0012935 -2.9906e-20 v k 6.9125e-10 0.0010566 0.00069398 0.00088342 v omega 13.476 1.0313e+05 2665.3 498.45 v TempK 288 342.08 294.1 291.05 v Density 1.205 1.205 1.205 1.205 v TurbVisc 8.1038e-15 9.449e-05 5.6556e-05 7.388e-05 v CourantNb 2.9135e-09 0.0001959 1.3805e-05 8.5573e-06 v FourierNb 0.094514 0.6281 0.1863 0.15721 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9549 4.9549 0.00054614 -5.5876e-07 v volume_forces[Z] -4.9549 4.9549 -0.00054602 6.6387e-07 v ǁvolume_forcesǁ 1.0409e-08 4.956 0.55255 0.27368 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.31 291.19 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015083 5.3336e-05 2.9785e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.094534 0.6281 0.18632 0.15722 INSTANT 0.768474000E+00 TIME STEP NUMBER 798 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15878E-05 0.22665E-02 Friction velocity uk : 0.15902E-05 0.22664E-02 Dimensionless distance yplus : 0.10590E-04 0.15079E-01 Friction thermal sca. tstar : -0.16867E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.74377E-05 0.10590E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15878E-05 0.22665E-02 Friction velocity uk : 0.15902E-05 0.22664E-02 Dimensionless distance yplus : 0.10590E-04 0.15079E-01 Friction thermal sca. tstar : -0.16867E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.74377E-05 0.10590E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.36923E-08 3 0.11391E-06 0.20613E-12 0.91071E+00 c Velocity[X] 0.55702E-32 c Velocity[Y] 0.10306E-12 c Velocity[Z] 0.10307E-12 c Pressure 0.78940E-14 16 0.61364E-07 0.61364E-07 0.99291E+00 c k 0.31769E-06 2 0.33710E-07 0.15325E-08 0.13524E+01 c omega 0.13153E+02 1 0.10553E-08 0.18194E+00 0.22206E-02 c TempK 0.94716E+02 1 0.84414E-07 0.19050E-01 0.15274E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.2558e-14 7.7356e-14 -9.6083e-18 -2.4982e-18 v Velocity[Y] -0.00012329 0.00011673 -5.8329e-10 -3.1856e-12 v Velocity[Z] -0.00011668 0.0001233 3.0453e-10 -1.8153e-12 v ǁVelocityǁ 2.8958e-10 0.0001322 1.1169e-05 7.9836e-06 v Pressure -0.0013455 0.022738 0.0012944 2.1572e-20 v k 6.8895e-10 0.0010554 0.00069303 0.00088225 v omega 13.462 1.0313e+05 2665.3 498.44 v TempK 288 342.08 294.1 291.05 v Density 1.205 1.205 1.205 1.205 v TurbVisc 8.0768e-15 9.448e-05 5.6538e-05 7.3859e-05 v CourantNb 2.9163e-09 0.00019581 1.3805e-05 8.5609e-06 v FourierNb 0.094434 0.6281 0.18627 0.15718 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9549 4.955 0.00054634 -5.5904e-07 v volume_forces[Z] -4.9549 4.955 -0.00054623 6.6417e-07 v ǁvolume_forcesǁ 1.0434e-08 4.956 0.55276 0.27385 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.31 291.19 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015079 5.3324e-05 2.9777e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.094454 0.6281 0.18628 0.15718 INSTANT 0.769437000E+00 TIME STEP NUMBER 799 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19611E-05 0.22659E-02 Friction velocity uk : 0.19630E-05 0.22659E-02 Dimensionless distance yplus : 0.13073E-04 0.15075E-01 Friction thermal sca. tstar : -0.16352E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.91813E-05 0.10588E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19611E-05 0.22659E-02 Friction velocity uk : 0.19630E-05 0.22659E-02 Dimensionless distance yplus : 0.13073E-04 0.15075E-01 Friction thermal sca. tstar : -0.16352E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.91813E-05 0.10588E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.36937E-08 3 0.11364E-06 0.20571E-12 0.90966E+00 c Velocity[X] 0.55481E-32 c Velocity[Y] 0.10285E-12 c Velocity[Z] 0.10286E-12 c Pressure 0.78796E-14 16 0.61251E-07 0.61251E-07 0.99160E+00 c k 0.31728E-06 2 0.33654E-07 0.15254E-08 0.13510E+01 c omega 0.13153E+02 1 0.10525E-08 0.18115E+00 0.22158E-02 c TempK 0.94716E+02 1 0.84264E-07 0.19014E-01 0.15260E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.2504e-14 7.7312e-14 -9.6031e-18 -2.497e-18 v Velocity[Y] -0.00012327 0.0001167 -5.8096e-10 -3.181e-12 v Velocity[Z] -0.00011665 0.00012327 3.0205e-10 -1.8154e-12 v ǁVelocityǁ 2.908e-10 0.00013217 1.1173e-05 7.9897e-06 v Pressure -0.0013472 0.022751 0.0012954 -1.863e-20 v k 6.8666e-10 0.0010541 0.00069208 0.00088109 v omega 13.448 1.0313e+05 2665.3 498.42 v TempK 288 342.08 294.11 291.05 v Density 1.205 1.205 1.205 1.205 v TurbVisc 8.0499e-15 9.4469e-05 5.652e-05 7.3838e-05 v CourantNb 2.919e-09 0.00019571 1.3805e-05 8.5644e-06 v FourierNb 0.094355 0.6281 0.18623 0.15714 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.955 4.955 0.00054655 -5.5932e-07 v volume_forces[Z] -4.955 4.955 -0.00054643 6.6448e-07 v ǁvolume_forcesǁ 1.0468e-08 4.9561 0.55296 0.27402 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.31 291.19 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015075 5.3311e-05 2.9769e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.094374 0.6281 0.18624 0.15715 INSTANT 0.770400000E+00 TIME STEP NUMBER 800 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.22746E-05 0.22653E-02 Friction velocity uk : 0.22762E-05 0.22653E-02 Dimensionless distance yplus : 0.15159E-04 0.15071E-01 Friction thermal sca. tstar : -0.15881E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.10646E-04 0.10585E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.22746E-05 0.22653E-02 Friction velocity uk : 0.22762E-05 0.22653E-02 Dimensionless distance yplus : 0.15159E-04 0.15071E-01 Friction thermal sca. tstar : -0.15881E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.10646E-04 0.10585E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.36951E-08 3 0.11338E-06 0.20529E-12 0.90861E+00 c Velocity[X] 0.55263E-32 c Velocity[Y] 0.10264E-12 c Velocity[Z] 0.10265E-12 c Pressure 0.78651E-14 16 0.61137E-07 0.61137E-07 0.99030E+00 c k 0.31688E-06 2 0.33597E-07 0.15183E-08 0.13496E+01 c omega 0.13153E+02 1 0.10498E-08 0.18036E+00 0.22109E-02 c TempK 0.94717E+02 1 0.84114E-07 0.18978E-01 0.15245E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.245e-14 7.7269e-14 -9.5979e-18 -2.4958e-18 v Velocity[Y] -0.00012324 0.00011667 -5.7862e-10 -3.1763e-12 v Velocity[Z] -0.00011662 0.00012325 2.9957e-10 -1.8157e-12 v ǁVelocityǁ 2.9229e-10 0.00013214 1.1176e-05 7.9957e-06 v Pressure -0.0013489 0.022765 0.0012963 -2.1768e-20 v k 6.8438e-10 0.0010529 0.00069114 0.00087992 v omega 13.433 1.0313e+05 2665.3 498.41 v TempK 288 342.08 294.11 291.05 v Density 1.205 1.205 1.205 1.205 v TurbVisc 8.0232e-15 9.4459e-05 5.6502e-05 7.3816e-05 v CourantNb 2.9218e-09 0.00019562 1.3806e-05 8.5679e-06 v FourierNb 0.094275 0.6281 0.18619 0.1571 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.955 4.9551 0.00054675 -5.5959e-07 v volume_forces[Z] -4.955 4.9551 -0.00054664 6.6478e-07 v ǁvolume_forcesǁ 1.0512e-08 4.9561 0.55317 0.27419 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.32 291.2 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015071 5.3298e-05 2.9762e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.094294 0.6281 0.18621 0.15711 INSTANT 0.771363000E+00 TIME STEP NUMBER 801 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.25505E-05 0.22648E-02 Friction velocity uk : 0.25520E-05 0.22647E-02 Dimensionless distance yplus : 0.16995E-04 0.15068E-01 Friction thermal sca. tstar : -0.15449E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.11936E-04 0.10583E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.25505E-05 0.22648E-02 Friction velocity uk : 0.25520E-05 0.22647E-02 Dimensionless distance yplus : 0.16995E-04 0.15068E-01 Friction thermal sca. tstar : -0.15449E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.11936E-04 0.10583E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.36966E-08 3 0.11312E-06 0.20487E-12 0.90757E+00 c Velocity[X] 0.55046E-32 c Velocity[Y] 0.10243E-12 c Velocity[Z] 0.10244E-12 c Pressure 0.78506E-14 16 0.61024E-07 0.61024E-07 0.98901E+00 c k 0.31647E-06 2 0.33541E-07 0.15113E-08 0.13482E+01 c omega 0.13153E+02 1 0.10470E-08 0.17958E+00 0.22061E-02 c TempK 0.94717E+02 1 0.83965E-07 0.18943E-01 0.15231E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.2396e-14 7.7226e-14 -9.5927e-18 -2.4945e-18 v Velocity[Y] -0.00012322 0.00011664 -5.7628e-10 -3.1718e-12 v Velocity[Z] -0.00011659 0.00012322 2.9709e-10 -1.8159e-12 v ǁVelocityǁ 2.9404e-10 0.00013211 1.118e-05 8.0018e-06 v Pressure -0.0013505 0.022779 0.0012973 -1.2766e-19 v k 6.8211e-10 0.0010517 0.00069019 0.00087876 v omega 13.419 1.0313e+05 2665.3 498.4 v TempK 288 342.08 294.11 291.06 v Density 1.205 1.205 1.205 1.205 v TurbVisc 7.9965e-15 9.4448e-05 5.6483e-05 7.3795e-05 v CourantNb 2.9245e-09 0.00019553 1.3806e-05 8.5714e-06 v FourierNb 0.094196 0.6281 0.18616 0.15706 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9551 4.9551 0.00054696 -5.5987e-07 v volume_forces[Z] -4.9551 4.9551 -0.00054685 6.6508e-07 v ǁvolume_forcesǁ 1.0566e-08 4.9562 0.55337 0.27436 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.32 291.2 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015068 5.3285e-05 2.9754e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.094215 0.6281 0.18617 0.15707 INSTANT 0.772326000E+00 TIME STEP NUMBER 802 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.28000E-05 0.22642E-02 Friction velocity uk : 0.28013E-05 0.22642E-02 Dimensionless distance yplus : 0.18655E-04 0.15064E-01 Friction thermal sca. tstar : -0.15051E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.13102E-04 0.10580E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.28000E-05 0.22642E-02 Friction velocity uk : 0.28013E-05 0.22642E-02 Dimensionless distance yplus : 0.18655E-04 0.15064E-01 Friction thermal sca. tstar : -0.15051E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.13102E-04 0.10580E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.36980E-08 3 0.11286E-06 0.20445E-12 0.90652E+00 c Velocity[X] 0.54830E-32 c Velocity[Y] 0.10222E-12 c Velocity[Z] 0.10223E-12 c Pressure 0.78372E-14 16 0.60919E-07 0.60919E-07 0.98772E+00 c k 0.31607E-06 2 0.33485E-07 0.15043E-08 0.13468E+01 c omega 0.13153E+02 1 0.10443E-08 0.17880E+00 0.22013E-02 c TempK 0.94718E+02 1 0.83817E-07 0.18907E-01 0.15217E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.2342e-14 7.7182e-14 -9.5876e-18 -2.4933e-18 v Velocity[Y] -0.00012319 0.00011661 -5.7394e-10 -3.1672e-12 v Velocity[Z] -0.00011656 0.00012319 2.9461e-10 -1.8161e-12 v ǁVelocityǁ 2.9605e-10 0.00013208 1.1184e-05 8.0079e-06 v Pressure -0.0013522 0.022793 0.0012983 8.5796e-20 v k 6.7985e-10 0.0010505 0.00068925 0.0008776 v omega 13.405 1.0313e+05 2665.3 498.39 v TempK 288 342.08 294.11 291.06 v Density 1.205 1.205 1.205 1.205 v TurbVisc 7.97e-15 9.4437e-05 5.6465e-05 7.3774e-05 v CourantNb 2.9272e-09 0.00019544 1.3806e-05 8.575e-06 v FourierNb 0.094117 0.6281 0.18612 0.15703 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9551 4.9552 0.00054716 -5.6014e-07 v volume_forces[Z] -4.9551 4.9552 -0.00054705 6.6539e-07 v ǁvolume_forcesǁ 1.0629e-08 4.9562 0.55357 0.27453 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.32 291.2 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015064 5.3273e-05 2.9746e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.094136 0.6281 0.18614 0.15704 INSTANT 0.773289000E+00 TIME STEP NUMBER 803 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.30295E-05 0.22637E-02 Friction velocity uk : 0.30307E-05 0.22636E-02 Dimensionless distance yplus : 0.20183E-04 0.15060E-01 Friction thermal sca. tstar : -0.14682E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.14175E-04 0.10577E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.30295E-05 0.22637E-02 Friction velocity uk : 0.30307E-05 0.22636E-02 Dimensionless distance yplus : 0.20183E-04 0.15060E-01 Friction thermal sca. tstar : -0.14682E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.14175E-04 0.10577E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.36994E-08 3 0.11260E-06 0.20403E-12 0.90547E+00 c Velocity[X] 0.54615E-32 c Velocity[Y] 0.10201E-12 c Velocity[Z] 0.10202E-12 c Pressure 0.78227E-14 16 0.60805E-07 0.60805E-07 0.98643E+00 c k 0.31567E-06 2 0.33429E-07 0.14973E-08 0.13454E+01 c omega 0.13153E+02 1 0.10415E-08 0.17802E+00 0.21966E-02 c TempK 0.94718E+02 1 0.83668E-07 0.18872E-01 0.15202E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.2288e-14 7.7139e-14 -9.5824e-18 -2.4921e-18 v Velocity[Y] -0.00012316 0.00011658 -5.7159e-10 -3.1626e-12 v Velocity[Z] -0.00011653 0.00012317 2.9212e-10 -1.8163e-12 v ǁVelocityǁ 2.9831e-10 0.00013206 1.1188e-05 8.0139e-06 v Pressure -0.0013538 0.022807 0.0012992 -4.53e-20 v k 6.776e-10 0.0010492 0.00068831 0.00087644 v omega 13.391 1.0313e+05 2665.3 498.37 v TempK 288 342.08 294.11 291.06 v Density 1.205 1.205 1.205 1.205 v TurbVisc 7.9436e-15 9.4427e-05 5.6448e-05 7.3753e-05 v CourantNb 2.9299e-09 0.00019535 1.3807e-05 8.5785e-06 v FourierNb 0.094038 0.6281 0.18609 0.15699 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9552 4.9552 0.00054737 -5.6042e-07 v volume_forces[Z] -4.9552 4.9552 -0.00054726 6.6569e-07 v ǁvolume_forcesǁ 1.0702e-08 4.9563 0.55378 0.2747 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.32 291.2 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.01506 5.326e-05 2.9738e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.094057 0.6281 0.1861 0.157 INSTANT 0.774252000E+00 TIME STEP NUMBER 804 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.32434E-05 0.22631E-02 Friction velocity uk : 0.32445E-05 0.22631E-02 Dimensionless distance yplus : 0.21607E-04 0.15057E-01 Friction thermal sca. tstar : -0.14339E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.15175E-04 0.10575E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.32434E-05 0.22631E-02 Friction velocity uk : 0.32445E-05 0.22631E-02 Dimensionless distance yplus : 0.21607E-04 0.15057E-01 Friction thermal sca. tstar : -0.14339E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.15175E-04 0.10575E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.37009E-08 3 0.11233E-06 0.20362E-12 0.90442E+00 c Velocity[X] 0.54401E-32 c Velocity[Y] 0.10181E-12 c Velocity[Z] 0.10181E-12 c Pressure 0.78072E-14 16 0.60684E-07 0.60684E-07 0.98514E+00 c k 0.31527E-06 2 0.33373E-07 0.14904E-08 0.13440E+01 c omega 0.13153E+02 1 0.10388E-08 0.17725E+00 0.21918E-02 c TempK 0.94719E+02 1 0.83521E-07 0.18837E-01 0.15188E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.2235e-14 7.7096e-14 -9.5773e-18 -2.4909e-18 v Velocity[Y] -0.00012314 0.00011655 -5.6924e-10 -3.1581e-12 v Velocity[Z] -0.0001165 0.00012314 2.8964e-10 -1.8165e-12 v ǁVelocityǁ 3.0083e-10 0.00013203 1.1191e-05 8.02e-06 v Pressure -0.0013555 0.022821 0.0013002 1.0197e-20 v k 6.7536e-10 0.001048 0.00068737 0.00087529 v omega 13.377 1.0313e+05 2665.3 498.36 v TempK 288 342.08 294.12 291.06 v Density 1.205 1.205 1.205 1.205 v TurbVisc 7.9173e-15 9.4416e-05 5.643e-05 7.3732e-05 v CourantNb 2.9326e-09 0.00019526 1.3807e-05 8.582e-06 v FourierNb 0.093959 0.6281 0.18605 0.15695 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9552 4.9552 0.00054757 -5.6069e-07 v volume_forces[Z] -4.9552 4.9552 -0.00054746 6.6599e-07 v ǁvolume_forcesǁ 1.0784e-08 4.9563 0.55398 0.27487 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.33 291.2 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015057 5.3247e-05 2.9731e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.093979 0.6281 0.18607 0.15696 INSTANT 0.775215000E+00 TIME STEP NUMBER 805 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.34444E-05 0.22626E-02 Friction velocity uk : 0.34454E-05 0.22625E-02 Dimensionless distance yplus : 0.22945E-04 0.15053E-01 Friction thermal sca. tstar : -0.14019E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.16115E-04 0.10572E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.34444E-05 0.22626E-02 Friction velocity uk : 0.34454E-05 0.22625E-02 Dimensionless distance yplus : 0.22945E-04 0.15053E-01 Friction thermal sca. tstar : -0.14019E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.16115E-04 0.10572E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.37023E-08 3 0.11207E-06 0.20320E-12 0.90337E+00 c Velocity[X] 0.54189E-32 c Velocity[Y] 0.10160E-12 c Velocity[Z] 0.10160E-12 c Pressure 0.77927E-14 16 0.60570E-07 0.60570E-07 0.98386E+00 c k 0.31487E-06 2 0.33317E-07 0.14835E-08 0.13426E+01 c omega 0.13153E+02 1 0.10361E-08 0.17648E+00 0.21871E-02 c TempK 0.94719E+02 1 0.83373E-07 0.18802E-01 0.15174E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.2181e-14 7.7053e-14 -9.5721e-18 -2.4897e-18 v Velocity[Y] -0.00012311 0.00011652 -5.6689e-10 -3.1536e-12 v Velocity[Z] -0.00011647 0.00012312 2.8715e-10 -1.8167e-12 v ǁVelocityǁ 3.0361e-10 0.000132 1.1195e-05 8.026e-06 v Pressure -0.0013572 0.022835 0.0013011 -2.5102e-20 v k 6.7313e-10 0.0010468 0.00068643 0.00087414 v omega 13.363 1.0313e+05 2665.3 498.35 v TempK 288 342.08 294.12 291.06 v Density 1.205 1.205 1.205 1.205 v TurbVisc 7.8911e-15 9.4406e-05 5.6412e-05 7.3711e-05 v CourantNb 2.9354e-09 0.00019517 1.3807e-05 8.5855e-06 v FourierNb 0.093881 0.6281 0.18602 0.15692 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9553 4.9553 0.00054778 -5.6097e-07 v volume_forces[Z] -4.9553 4.9553 -0.00054766 6.6629e-07 v ǁvolume_forcesǁ 1.0875e-08 4.9564 0.55418 0.27504 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.33 291.21 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015053 5.3234e-05 2.9723e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.0939 0.6281 0.18603 0.15693 INSTANT 0.776178000E+00 TIME STEP NUMBER 806 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.36348E-05 0.22620E-02 Friction velocity uk : 0.36358E-05 0.22620E-02 Dimensionless distance yplus : 0.24213E-04 0.15049E-01 Friction thermal sca. tstar : -0.13720E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.17005E-04 0.10570E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.36348E-05 0.22620E-02 Friction velocity uk : 0.36358E-05 0.22620E-02 Dimensionless distance yplus : 0.24213E-04 0.15049E-01 Friction thermal sca. tstar : -0.13720E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.17005E-04 0.10570E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.37038E-08 3 0.11181E-06 0.20278E-12 0.90232E+00 c Velocity[X] 0.53978E-32 c Velocity[Y] 0.10139E-12 c Velocity[Z] 0.10139E-12 c Pressure 0.77791E-14 16 0.60464E-07 0.60464E-07 0.98258E+00 c k 0.31447E-06 2 0.33261E-07 0.14767E-08 0.13412E+01 c omega 0.13153E+02 1 0.10334E-08 0.17572E+00 0.21823E-02 c TempK 0.94720E+02 1 0.83226E-07 0.18767E-01 0.15160E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.2128e-14 7.701e-14 -9.567e-18 -2.4884e-18 v Velocity[Y] -0.00012309 0.00011649 -5.6454e-10 -3.149e-12 v Velocity[Z] -0.00011644 0.00012309 2.8466e-10 -1.8169e-12 v ǁVelocityǁ 3.0662e-10 0.00013197 1.1199e-05 8.0321e-06 v Pressure -0.0013588 0.022848 0.0013021 -1.2649e-20 v k 6.7091e-10 0.0010456 0.0006855 0.00087299 v omega 13.349 1.0313e+05 2665.2 498.34 v TempK 288 342.08 294.12 291.07 v Density 1.205 1.205 1.205 1.205 v TurbVisc 7.865e-15 9.4395e-05 5.6394e-05 7.369e-05 v CourantNb 2.9381e-09 0.00019508 1.3808e-05 8.589e-06 v FourierNb 0.093803 0.6281 0.18598 0.15688 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9553 4.9553 0.00054798 -5.6124e-07 v volume_forces[Z] -4.9553 4.9553 -0.00054787 6.6659e-07 v ǁvolume_forcesǁ 1.0975e-08 4.9564 0.55438 0.27521 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.33 291.21 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015049 5.3222e-05 2.9715e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.093822 0.6281 0.18599 0.15689 INSTANT 0.777141000E+00 TIME STEP NUMBER 807 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.38162E-05 0.22615E-02 Friction velocity uk : 0.38171E-05 0.22614E-02 Dimensionless distance yplus : 0.25420E-04 0.15046E-01 Friction thermal sca. tstar : -0.13439E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.17853E-04 0.10567E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.38162E-05 0.22615E-02 Friction velocity uk : 0.38171E-05 0.22614E-02 Dimensionless distance yplus : 0.25420E-04 0.15046E-01 Friction thermal sca. tstar : -0.13439E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.17853E-04 0.10567E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.37052E-08 3 0.11156E-06 0.20236E-12 0.90127E+00 c Velocity[X] 0.53767E-32 c Velocity[Y] 0.10118E-12 c Velocity[Z] 0.10118E-12 c Pressure 0.77647E-14 16 0.60351E-07 0.60351E-07 0.98130E+00 c k 0.31407E-06 2 0.33206E-07 0.14699E-08 0.13399E+01 c omega 0.13153E+02 1 0.10307E-08 0.17496E+00 0.21776E-02 c TempK 0.94721E+02 1 0.83080E-07 0.18732E-01 0.15145E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.2074e-14 7.6967e-14 -9.5619e-18 -2.4872e-18 v Velocity[Y] -0.00012306 0.00011646 -5.6219e-10 -3.1445e-12 v Velocity[Z] -0.00011641 0.00012307 2.8217e-10 -1.8171e-12 v ǁVelocityǁ 3.0988e-10 0.00013194 1.1203e-05 8.0381e-06 v Pressure -0.0013605 0.022862 0.001303 -6.0695e-20 v k 6.687e-10 0.0010444 0.00068457 0.00087184 v omega 13.335 1.0313e+05 2665.2 498.32 v TempK 288 342.08 294.12 291.07 v Density 1.205 1.205 1.205 1.205 v TurbVisc 7.8391e-15 9.4385e-05 5.6376e-05 7.3669e-05 v CourantNb 2.9408e-09 0.00019499 1.3808e-05 8.5926e-06 v FourierNb 0.093725 0.6281 0.18594 0.15685 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9554 4.9554 0.00054818 -5.6151e-07 v volume_forces[Z] -4.9554 4.9554 -0.00054807 6.6689e-07 v ǁvolume_forcesǁ 1.1084e-08 4.9565 0.55459 0.27538 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.33 291.21 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015046 5.3209e-05 2.9708e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.093744 0.6281 0.18596 0.15685 INSTANT 0.778104000E+00 TIME STEP NUMBER 808 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.39897E-05 0.22609E-02 Friction velocity uk : 0.39906E-05 0.22609E-02 Dimensionless distance yplus : 0.26575E-04 0.15042E-01 Friction thermal sca. tstar : -0.13176E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.18665E-04 0.10565E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.39897E-05 0.22609E-02 Friction velocity uk : 0.39906E-05 0.22609E-02 Dimensionless distance yplus : 0.26575E-04 0.15042E-01 Friction thermal sca. tstar : -0.13176E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.18665E-04 0.10565E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.37066E-08 3 0.16162E-06 0.20195E-12 0.90022E+00 c Velocity[X] 0.53558E-32 c Velocity[Y] 0.10097E-12 c Velocity[Z] 0.10098E-12 c Pressure 0.77570E-14 16 0.60291E-07 0.60291E-07 0.98003E+00 c k 0.31367E-06 2 0.33151E-07 0.14632E-08 0.13385E+01 c omega 0.13153E+02 1 0.10280E-08 0.17421E+00 0.21729E-02 c TempK 0.94721E+02 1 0.82934E-07 0.18697E-01 0.15131E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.2021e-14 7.6924e-14 -9.5568e-18 -2.486e-18 v Velocity[Y] -0.00012304 0.00011643 -5.5983e-10 -3.1401e-12 v Velocity[Z] -0.00011638 0.00012304 2.7968e-10 -1.8173e-12 v ǁVelocityǁ 3.1336e-10 0.00013192 1.1206e-05 8.0442e-06 v Pressure -0.0013622 0.022876 0.001304 5.5792e-20 v k 6.665e-10 0.0010431 0.00068364 0.0008707 v omega 13.321 1.0313e+05 2665.2 498.31 v TempK 288 342.08 294.13 291.07 v Density 1.205 1.205 1.205 1.205 v TurbVisc 7.8133e-15 9.4375e-05 5.6358e-05 7.3648e-05 v CourantNb 2.9434e-09 0.0001949 1.3808e-05 8.5961e-06 v FourierNb 0.093647 0.6281 0.18591 0.15681 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9554 4.9554 0.00054839 -5.6178e-07 v volume_forces[Z] -4.9554 4.9554 -0.00054828 6.6719e-07 v ǁvolume_forcesǁ 1.1202e-08 4.9565 0.55479 0.27555 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.33 291.21 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015042 5.3196e-05 2.97e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.093666 0.6281 0.18592 0.15682 INSTANT 0.779067000E+00 TIME STEP NUMBER 809 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.41564E-05 0.22604E-02 Friction velocity uk : 0.41572E-05 0.22603E-02 Dimensionless distance yplus : 0.27685E-04 0.15038E-01 Friction thermal sca. tstar : -0.12927E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.19444E-04 0.10562E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.41564E-05 0.22604E-02 Friction velocity uk : 0.41572E-05 0.22603E-02 Dimensionless distance yplus : 0.27685E-04 0.15038E-01 Friction thermal sca. tstar : -0.12927E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.19444E-04 0.10562E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.37081E-08 3 0.11105E-06 0.20153E-12 0.89918E+00 c Velocity[X] 0.53350E-32 c Velocity[Y] 0.10076E-12 c Velocity[Z] 0.10077E-12 c Pressure 0.77438E-14 16 0.60187E-07 0.60187E-07 0.97876E+00 c k 0.31328E-06 2 0.33096E-07 0.14565E-08 0.13371E+01 c omega 0.13153E+02 1 0.10253E-08 0.17346E+00 0.21682E-02 c TempK 0.94722E+02 1 0.82788E-07 0.18663E-01 0.15117E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.1968e-14 7.6882e-14 -9.5517e-18 -2.4848e-18 v Velocity[Y] -0.00012301 0.0001164 -5.5747e-10 -3.1356e-12 v Velocity[Z] -0.00011635 0.00012302 2.7718e-10 -1.8175e-12 v ǁVelocityǁ 3.1708e-10 0.00013189 1.121e-05 8.0502e-06 v Pressure -0.0013638 0.02289 0.0013049 -3.726e-21 v k 6.6431e-10 0.0010419 0.00068271 0.00086956 v omega 13.307 1.0313e+05 2665.2 498.3 v TempK 288 342.08 294.13 291.07 v Density 1.205 1.205 1.205 1.205 v TurbVisc 7.7876e-15 9.4364e-05 5.634e-05 7.3627e-05 v CourantNb 2.9461e-09 0.00019481 1.3809e-05 8.5996e-06 v FourierNb 0.09357 0.6281 0.18587 0.15677 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9555 4.9555 0.00054859 -5.6206e-07 v volume_forces[Z] -4.9555 4.9555 -0.00054848 6.6749e-07 v ǁvolume_forcesǁ 1.1328e-08 4.9565 0.55499 0.27572 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.34 291.21 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015038 5.3184e-05 2.9693e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.093589 0.6281 0.18589 0.15678 INSTANT 0.780030000E+00 TIME STEP NUMBER 810 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.43170E-05 0.22598E-02 Friction velocity uk : 0.43178E-05 0.22598E-02 Dimensionless distance yplus : 0.28755E-04 0.15035E-01 Friction thermal sca. tstar : -0.12692E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.20195E-04 0.10559E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.43170E-05 0.22598E-02 Friction velocity uk : 0.43178E-05 0.22598E-02 Dimensionless distance yplus : 0.28755E-04 0.15035E-01 Friction thermal sca. tstar : -0.12692E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.20195E-04 0.10559E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.37095E-08 3 0.22896E-06 0.20112E-12 0.89813E+00 c Velocity[X] 0.53142E-32 c Velocity[Y] 0.10056E-12 c Velocity[Z] 0.10056E-12 c Pressure 0.77641E-14 16 0.60344E-07 0.60344E-07 0.97749E+00 c k 0.31288E-06 2 0.33041E-07 0.14498E-08 0.13357E+01 c omega 0.13153E+02 1 0.10226E-08 0.17271E+00 0.21636E-02 c TempK 0.94722E+02 1 0.82643E-07 0.18628E-01 0.15103E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.1915e-14 7.6839e-14 -9.5466e-18 -2.4836e-18 v Velocity[Y] -0.00012299 0.00011637 -5.5511e-10 -3.1311e-12 v Velocity[Z] -0.00011632 0.00012299 2.7469e-10 -1.8176e-12 v ǁVelocityǁ 3.2102e-10 0.00013186 1.1214e-05 8.0563e-06 v Pressure -0.0013655 0.022904 0.0013059 -8.5502e-20 v k 6.6213e-10 0.0010407 0.00068179 0.00086842 v omega 13.293 1.0313e+05 2665.2 498.29 v TempK 288 342.08 294.13 291.07 v Density 1.205 1.205 1.205 1.205 v TurbVisc 7.762e-15 9.4354e-05 5.6322e-05 7.3606e-05 v CourantNb 2.9488e-09 0.00019472 1.3809e-05 8.6031e-06 v FourierNb 0.093492 0.6281 0.18584 0.15674 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9555 4.9555 0.00054879 -5.6233e-07 v volume_forces[Z] -4.9555 4.9555 -0.00054868 6.6779e-07 v ǁvolume_forcesǁ 1.1462e-08 4.9566 0.55519 0.27589 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.34 291.22 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015035 5.3171e-05 2.9685e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.093511 0.6281 0.18585 0.15674 INSTANT 0.780993000E+00 TIME STEP NUMBER 811 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.44722E-05 0.22593E-02 Friction velocity uk : 0.44730E-05 0.22592E-02 Dimensionless distance yplus : 0.29788E-04 0.15031E-01 Friction thermal sca. tstar : -0.12469E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.20921E-04 0.10557E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.44722E-05 0.22593E-02 Friction velocity uk : 0.44730E-05 0.22592E-02 Dimensionless distance yplus : 0.29788E-04 0.15031E-01 Friction thermal sca. tstar : -0.12469E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.20921E-04 0.10557E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.37110E-08 3 0.11054E-06 0.20070E-12 0.89708E+00 c Velocity[X] 0.52936E-32 c Velocity[Y] 0.10035E-12 c Velocity[Z] 0.10035E-12 c Pressure 0.77459E-14 16 0.60202E-07 0.60202E-07 0.97623E+00 c k 0.31249E-06 2 0.32986E-07 0.14431E-08 0.13344E+01 c omega 0.13153E+02 1 0.10200E-08 0.17197E+00 0.21589E-02 c TempK 0.94723E+02 1 0.82498E-07 0.18594E-01 0.15089E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.1862e-14 7.6797e-14 -9.5416e-18 -2.4824e-18 v Velocity[Y] -0.00012296 0.00011634 -5.5274e-10 -3.1267e-12 v Velocity[Z] -0.00011629 0.00012297 2.722e-10 -1.8178e-12 v ǁVelocityǁ 3.2517e-10 0.00013183 1.1218e-05 8.0623e-06 v Pressure -0.0013671 0.022917 0.0013068 3.9123e-20 v k 6.5996e-10 0.0010395 0.00068086 0.00086729 v omega 13.279 1.0313e+05 2665.2 498.27 v TempK 288 342.08 294.13 291.08 v Density 1.205 1.205 1.205 1.205 v TurbVisc 7.7365e-15 9.4343e-05 5.6304e-05 7.3585e-05 v CourantNb 2.9515e-09 0.00019464 1.3809e-05 8.6066e-06 v FourierNb 0.093415 0.6281 0.1858 0.1567 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9556 4.9556 0.000549 -5.626e-07 v volume_forces[Z] -4.9556 4.9556 -0.00054889 6.6809e-07 v ǁvolume_forcesǁ 1.1605e-08 4.9566 0.55539 0.27606 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.34 291.22 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015031 5.3158e-05 2.9677e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.093434 0.6281 0.18582 0.15671 INSTANT 0.781956000E+00 TIME STEP NUMBER 812 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.46226E-05 0.22587E-02 Friction velocity uk : 0.46233E-05 0.22587E-02 Dimensionless distance yplus : 0.30789E-04 0.15027E-01 Friction thermal sca. tstar : -0.12258E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.21624E-04 0.10554E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.46226E-05 0.22587E-02 Friction velocity uk : 0.46233E-05 0.22587E-02 Dimensionless distance yplus : 0.30789E-04 0.15027E-01 Friction thermal sca. tstar : -0.12258E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.21624E-04 0.10554E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.37124E-08 3 0.11028E-06 0.20029E-12 0.89603E+00 c Velocity[X] 0.52731E-32 c Velocity[Y] 0.10014E-12 c Velocity[Z] 0.10015E-12 c Pressure 0.76935E-14 16 0.59794E-07 0.59794E-07 0.97497E+00 c k 0.31209E-06 2 0.32931E-07 0.14365E-08 0.13330E+01 c omega 0.13153E+02 1 0.10173E-08 0.17123E+00 0.21543E-02 c TempK 0.94723E+02 1 0.82354E-07 0.18559E-01 0.15075E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.1809e-14 7.6754e-14 -9.5365e-18 -2.4812e-18 v Velocity[Y] -0.00012294 0.00011631 -5.5038e-10 -3.1223e-12 v Velocity[Z] -0.00011626 0.00012294 2.697e-10 -1.818e-12 v ǁVelocityǁ 3.236e-10 0.00013181 1.1221e-05 8.0684e-06 v Pressure -0.0013688 0.022931 0.0013078 -7.452e-20 v k 6.578e-10 0.0010383 0.00067994 0.00086615 v omega 13.265 1.0313e+05 2665.2 498.26 v TempK 288 342.09 294.13 291.08 v Density 1.205 1.205 1.205 1.205 v TurbVisc 7.7111e-15 9.4333e-05 5.6287e-05 7.3564e-05 v CourantNb 2.9542e-09 0.00019457 1.381e-05 8.6101e-06 v FourierNb 0.093338 0.6281 0.18577 0.15666 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9556 4.9556 0.0005492 -5.6287e-07 v volume_forces[Z] -4.9556 4.9556 -0.00054909 6.6839e-07 v ǁvolume_forcesǁ 1.1755e-08 4.9567 0.55559 0.27622 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.34 291.22 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015027 5.3146e-05 2.967e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.093358 0.6281 0.18578 0.15667 INSTANT 0.782919000E+00 TIME STEP NUMBER 813 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.47473E-05 0.22582E-02 Friction velocity uk : 0.47480E-05 0.22582E-02 Dimensionless distance yplus : 0.31620E-04 0.15024E-01 Friction thermal sca. tstar : -0.12057E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.22208E-04 0.10552E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.47473E-05 0.22582E-02 Friction velocity uk : 0.47480E-05 0.22582E-02 Dimensionless distance yplus : 0.31620E-04 0.15024E-01 Friction thermal sca. tstar : -0.12057E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.22208E-04 0.10552E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.37139E-08 3 0.11002E-06 0.19988E-12 0.89498E+00 c Velocity[X] 0.52528E-32 c Velocity[Y] 0.99937E-13 c Velocity[Z] 0.99940E-13 c Pressure 0.76791E-14 16 0.59681E-07 0.59681E-07 0.97371E+00 c k 0.31170E-06 2 0.32877E-07 0.14300E-08 0.13316E+01 c omega 0.13153E+02 1 0.10147E-08 0.17050E+00 0.21496E-02 c TempK 0.94724E+02 1 0.82210E-07 0.18525E-01 0.15061E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.1756e-14 7.6712e-14 -9.5315e-18 -2.48e-18 v Velocity[Y] -0.00012291 0.00011628 -5.4801e-10 -3.118e-12 v Velocity[Z] -0.00011623 0.00012292 2.672e-10 -1.8182e-12 v ǁVelocityǁ 3.2059e-10 0.00013178 1.1225e-05 8.0744e-06 v Pressure -0.0013705 0.022945 0.0013088 -2.7357e-20 v k 6.5564e-10 0.0010371 0.00067903 0.00086502 v omega 13.251 1.0313e+05 2665.2 498.25 v TempK 288 342.09 294.14 291.08 v Density 1.205 1.205 1.205 1.205 v TurbVisc 7.6859e-15 9.4322e-05 5.6269e-05 7.3543e-05 v CourantNb 2.9568e-09 0.0001945 1.381e-05 8.6136e-06 v FourierNb 0.093262 0.6281 0.18573 0.15663 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9557 4.9557 0.0005494 -5.6314e-07 v volume_forces[Z] -4.9557 4.9557 -0.00054929 6.6868e-07 v ǁvolume_forcesǁ 1.1698e-08 4.9567 0.5558 0.27639 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.35 291.22 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015024 5.3133e-05 2.9662e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.093281 0.6281 0.18575 0.15664 INSTANT 0.783882000E+00 TIME STEP NUMBER 814 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.46331E-05 0.22576E-02 Friction velocity uk : 0.46338E-05 0.22576E-02 Dimensionless distance yplus : 0.30859E-04 0.15020E-01 Friction thermal sca. tstar : -0.11866E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.21673E-04 0.10549E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.46331E-05 0.22576E-02 Friction velocity uk : 0.46338E-05 0.22576E-02 Dimensionless distance yplus : 0.30859E-04 0.15020E-01 Friction thermal sca. tstar : -0.11866E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.21673E-04 0.10549E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.37153E-08 3 0.10977E-06 0.19946E-12 0.89393E+00 c Velocity[X] 0.52325E-32 c Velocity[Y] 0.99730E-13 c Velocity[Z] 0.99734E-13 c Pressure 0.76733E-14 16 0.59636E-07 0.59636E-07 0.97246E+00 c k 0.31131E-06 2 0.32823E-07 0.14234E-08 0.13303E+01 c omega 0.13153E+02 1 0.10121E-08 0.16977E+00 0.21450E-02 c TempK 0.94724E+02 1 0.82067E-07 0.18491E-01 0.15047E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.1703e-14 7.667e-14 -9.5264e-18 -2.4788e-18 v Velocity[Y] -0.00012289 0.00011625 -5.4564e-10 -3.1136e-12 v Velocity[Z] -0.0001162 0.00012289 2.647e-10 -1.8184e-12 v ǁVelocityǁ 3.177e-10 0.00013175 1.1229e-05 8.0804e-06 v Pressure -0.0013721 0.022959 0.0013097 3.7848e-20 v k 6.535e-10 0.0010359 0.00067811 0.0008639 v omega 13.237 1.0313e+05 2665.2 498.24 v TempK 288 342.09 294.14 291.08 v Density 1.205 1.205 1.205 1.205 v TurbVisc 7.6607e-15 9.4312e-05 5.6251e-05 7.3522e-05 v CourantNb 2.9595e-09 0.00019442 1.3811e-05 8.6171e-06 v FourierNb 0.093185 0.6281 0.1857 0.15659 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9557 4.9557 0.0005496 -5.6341e-07 v volume_forces[Z] -4.9557 4.9557 -0.00054949 6.6898e-07 v ǁvolume_forcesǁ 1.1589e-08 4.9568 0.556 0.27656 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.35 291.22 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.01502 5.312e-05 2.9654e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.093204 0.6281 0.18571 0.1566 INSTANT 0.784845000E+00 TIME STEP NUMBER 815 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.45157E-05 0.22571E-02 Friction velocity uk : 0.45164E-05 0.22571E-02 Dimensionless distance yplus : 0.30077E-04 0.15017E-01 Friction thermal sca. tstar : -0.11684E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.21124E-04 0.10547E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.45157E-05 0.22571E-02 Friction velocity uk : 0.45164E-05 0.22571E-02 Dimensionless distance yplus : 0.30077E-04 0.15017E-01 Friction thermal sca. tstar : -0.11684E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.21124E-04 0.10547E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.37168E-08 3 0.10952E-06 0.19905E-12 0.89288E+00 c Velocity[X] 0.52123E-32 c Velocity[Y] 0.99524E-13 c Velocity[Z] 0.99527E-13 c Pressure 0.76543E-14 16 0.59487E-07 0.59487E-07 0.97121E+00 c k 0.31092E-06 2 0.32768E-07 0.14169E-08 0.13289E+01 c omega 0.13153E+02 1 0.10094E-08 0.16904E+00 0.21404E-02 c TempK 0.94725E+02 1 0.81924E-07 0.18457E-01 0.15033E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.1651e-14 7.6627e-14 -9.5214e-18 -2.4776e-18 v Velocity[Y] -0.00012286 0.00011622 -5.4326e-10 -3.1092e-12 v Velocity[Z] -0.00011617 0.00012287 2.622e-10 -1.8185e-12 v ǁVelocityǁ 3.1494e-10 0.00013172 1.1233e-05 8.0864e-06 v Pressure -0.0013738 0.022972 0.0013106 -2.9416e-22 v k 6.5137e-10 0.0010347 0.0006772 0.00086277 v omega 13.224 1.0313e+05 2665.2 498.23 v TempK 288 342.09 294.14 291.08 v Density 1.205 1.205 1.205 1.205 v TurbVisc 7.6357e-15 9.4302e-05 5.6233e-05 7.3501e-05 v CourantNb 2.9622e-09 0.00019435 1.3811e-05 8.6206e-06 v FourierNb 0.093109 0.6281 0.18566 0.15656 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9558 4.9558 0.00054981 -5.6368e-07 v volume_forces[Z] -4.9558 4.9558 -0.0005497 6.6928e-07 v ǁvolume_forcesǁ 1.1485e-08 4.9568 0.5562 0.27673 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.35 291.22 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015017 5.3108e-05 2.9647e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.093128 0.6281 0.18568 0.15656 INSTANT 0.785808000E+00 TIME STEP NUMBER 816 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.43948E-05 0.22566E-02 Friction velocity uk : 0.43955E-05 0.22565E-02 Dimensionless distance yplus : 0.29272E-04 0.15013E-01 Friction thermal sca. tstar : -0.11511E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.20559E-04 0.10544E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.43948E-05 0.22566E-02 Friction velocity uk : 0.43955E-05 0.22565E-02 Dimensionless distance yplus : 0.29272E-04 0.15013E-01 Friction thermal sca. tstar : -0.11511E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.20559E-04 0.10544E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.37182E-08 3 0.10927E-06 0.19864E-12 0.89184E+00 c Velocity[X] 0.51922E-32 c Velocity[Y] 0.99318E-13 c Velocity[Z] 0.99321E-13 c Pressure 0.76377E-14 16 0.59357E-07 0.59357E-07 0.96996E+00 c k 0.31053E-06 2 0.32714E-07 0.14105E-08 0.13275E+01 c omega 0.13153E+02 1 0.10068E-08 0.16832E+00 0.21358E-02 c TempK 0.94725E+02 1 0.81781E-07 0.18423E-01 0.15019E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.1598e-14 7.6585e-14 -9.5164e-18 -2.4764e-18 v Velocity[Y] -0.00012284 0.00011619 -5.4089e-10 -3.1048e-12 v Velocity[Z] -0.00011614 0.00012284 2.597e-10 -1.8187e-12 v ǁVelocityǁ 3.1232e-10 0.0001317 1.1236e-05 8.0925e-06 v Pressure -0.0013754 0.022986 0.0013116 6.7656e-21 v k 6.4925e-10 0.0010336 0.00067628 0.00086165 v omega 13.21 1.0313e+05 2665.1 498.21 v TempK 288 342.09 294.14 291.09 v Density 1.205 1.205 1.205 1.205 v TurbVisc 7.6108e-15 9.4291e-05 5.6216e-05 7.348e-05 v CourantNb 2.9648e-09 0.00019428 1.3811e-05 8.6242e-06 v FourierNb 0.093033 0.6281 0.18563 0.15652 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9558 4.9558 0.00055001 -5.6395e-07 v volume_forces[Z] -4.9558 4.9558 -0.0005499 6.6957e-07 v ǁvolume_forcesǁ 1.1385e-08 4.9569 0.5564 0.2769 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.35 291.23 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015013 5.3095e-05 2.9639e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.093052 0.6281 0.18564 0.15653 INSTANT 0.786771000E+00 TIME STEP NUMBER 817 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.42702E-05 0.22560E-02 Friction velocity uk : 0.42709E-05 0.22560E-02 Dimensionless distance yplus : 0.28443E-04 0.15009E-01 Friction thermal sca. tstar : -0.11344E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.19976E-04 0.10542E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.42702E-05 0.22560E-02 Friction velocity uk : 0.42709E-05 0.22560E-02 Dimensionless distance yplus : 0.28443E-04 0.15009E-01 Friction thermal sca. tstar : -0.11344E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.19976E-04 0.10542E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.37197E-08 3 0.11397E-06 0.19823E-12 0.89079E+00 c Velocity[X] 0.51723E-32 c Velocity[Y] 0.99112E-13 c Velocity[Z] 0.99116E-13 c Pressure 0.76247E-14 16 0.59256E-07 0.59256E-07 0.96872E+00 c k 0.31014E-06 2 0.32661E-07 0.14041E-08 0.13262E+01 c omega 0.13153E+02 1 0.10042E-08 0.16760E+00 0.21313E-02 c TempK 0.94726E+02 1 0.81639E-07 0.18389E-01 0.15005E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.1546e-14 7.6543e-14 -9.5114e-18 -2.4753e-18 v Velocity[Y] -0.00012281 0.00011616 -5.3851e-10 -3.1005e-12 v Velocity[Z] -0.00011611 0.00012282 2.572e-10 -1.8188e-12 v ǁVelocityǁ 3.0983e-10 0.00013167 1.124e-05 8.0985e-06 v Pressure -0.0013771 0.023 0.0013125 -1.06e-19 v k 6.4713e-10 0.0010324 0.00067538 0.00086053 v omega 13.196 1.0313e+05 2665.1 498.2 v TempK 288 342.09 294.15 291.09 v Density 1.205 1.205 1.205 1.205 v TurbVisc 7.586e-15 9.4281e-05 5.6198e-05 7.3459e-05 v CourantNb 2.9675e-09 0.00019421 1.3812e-05 8.6277e-06 v FourierNb 0.092957 0.6281 0.18559 0.15648 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9558 4.9559 0.00055021 -5.6422e-07 v volume_forces[Z] -4.9558 4.9559 -0.0005501 6.6987e-07 v ǁvolume_forcesǁ 1.129e-08 4.9569 0.5566 0.27707 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.35 291.23 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015009 5.3083e-05 2.9632e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.092976 0.6281 0.18561 0.15649 INSTANT 0.787734000E+00 TIME STEP NUMBER 818 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.41415E-05 0.22555E-02 Friction velocity uk : 0.41423E-05 0.22554E-02 Dimensionless distance yplus : 0.27586E-04 0.15006E-01 Friction thermal sca. tstar : -0.11185E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.19374E-04 0.10539E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.41415E-05 0.22555E-02 Friction velocity uk : 0.41423E-05 0.22554E-02 Dimensionless distance yplus : 0.27586E-04 0.15006E-01 Friction thermal sca. tstar : -0.11185E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.19374E-04 0.10539E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.37211E-08 3 0.10877E-06 0.19782E-12 0.88974E+00 c Velocity[X] 0.51525E-32 c Velocity[Y] 0.98906E-13 c Velocity[Z] 0.98910E-13 c Pressure 0.76156E-14 16 0.59183E-07 0.59183E-07 0.96748E+00 c k 0.30975E-06 2 0.32607E-07 0.13977E-08 0.13248E+01 c omega 0.13153E+02 1 0.10016E-08 0.16688E+00 0.21267E-02 c TempK 0.94727E+02 1 0.81497E-07 0.18356E-01 0.14991E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.1493e-14 7.6501e-14 -9.5064e-18 -2.4741e-18 v Velocity[Y] -0.00012279 0.00011614 -5.3613e-10 -3.0962e-12 v Velocity[Z] -0.00011608 0.00012279 2.5469e-10 -1.8189e-12 v ǁVelocityǁ 3.0748e-10 0.00013164 1.1244e-05 8.1045e-06 v Pressure -0.0013788 0.023013 0.0013135 -8.5208e-20 v k 6.4503e-10 0.0010312 0.00067447 0.00085941 v omega 13.182 1.0313e+05 2665.1 498.19 v TempK 288 342.09 294.15 291.09 v Density 1.205 1.205 1.205 1.205 v TurbVisc 7.5613e-15 9.4271e-05 5.618e-05 7.3439e-05 v CourantNb 2.9701e-09 0.00019414 1.3812e-05 8.6312e-06 v FourierNb 0.092882 0.6281 0.18556 0.15645 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9559 4.9559 0.00055041 -5.6449e-07 v volume_forces[Z] -4.9559 4.9559 -0.0005503 6.7016e-07 v ǁvolume_forcesǁ 1.12e-08 4.957 0.5568 0.27724 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.36 291.23 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015006 5.307e-05 2.9624e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.092901 0.6281 0.18557 0.15646 INSTANT 0.788697000E+00 TIME STEP NUMBER 819 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.40083E-05 0.22549E-02 Friction velocity uk : 0.40091E-05 0.22549E-02 Dimensionless distance yplus : 0.26699E-04 0.15002E-01 Friction thermal sca. tstar : -0.11093E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.18752E-04 0.10537E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.40083E-05 0.22549E-02 Friction velocity uk : 0.40091E-05 0.22549E-02 Dimensionless distance yplus : 0.26699E-04 0.15002E-01 Friction thermal sca. tstar : -0.11093E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.18752E-04 0.10537E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.37226E-08 3 0.10853E-06 0.19741E-12 0.88869E+00 c Velocity[X] 0.51327E-32 c Velocity[Y] 0.98701E-13 c Velocity[Z] 0.98705E-13 c Pressure 0.76039E-14 16 0.59092E-07 0.59092E-07 0.96624E+00 c k 0.30936E-06 2 0.32553E-07 0.13913E-08 0.13235E+01 c omega 0.13153E+02 1 0.99905E-09 0.16617E+00 0.21222E-02 c TempK 0.94727E+02 1 0.81356E-07 0.18322E-01 0.14978E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.1441e-14 7.646e-14 -9.5014e-18 -2.4729e-18 v Velocity[Y] -0.00012276 0.00011611 -5.3375e-10 -3.0919e-12 v Velocity[Z] -0.00011605 0.00012277 2.5219e-10 -1.8191e-12 v ǁVelocityǁ 3.0528e-10 0.00013162 1.1248e-05 8.1105e-06 v Pressure -0.0013804 0.023027 0.0013144 4.079e-20 v k 6.4293e-10 0.00103 0.00067356 0.0008583 v omega 13.169 1.0313e+05 2665.1 498.18 v TempK 288 342.09 294.15 291.09 v Density 1.205 1.205 1.205 1.205 v TurbVisc 7.5367e-15 9.426e-05 5.6163e-05 7.3418e-05 v CourantNb 2.9728e-09 0.00019406 1.3813e-05 8.6347e-06 v FourierNb 0.092807 0.6281 0.18552 0.15641 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9559 4.956 0.00055061 -5.6475e-07 v volume_forces[Z] -4.9559 4.956 -0.0005505 6.7046e-07 v ǁvolume_forcesǁ 1.1116e-08 4.957 0.557 0.27741 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.36 291.23 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.015002 5.3058e-05 2.9617e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.092825 0.6281 0.18554 0.15642 INSTANT 0.789660000E+00 TIME STEP NUMBER 820 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.38702E-05 0.22544E-02 Friction velocity uk : 0.38710E-05 0.22544E-02 Dimensionless distance yplus : 0.25779E-04 0.14999E-01 Friction thermal sca. tstar : -0.11205E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.18106E-04 0.10534E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.38702E-05 0.22544E-02 Friction velocity uk : 0.38710E-05 0.22544E-02 Dimensionless distance yplus : 0.25779E-04 0.14999E-01 Friction thermal sca. tstar : -0.11205E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.18106E-04 0.10534E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.37240E-08 3 0.10828E-06 0.19700E-12 0.88764E+00 c Velocity[X] 0.51130E-32 c Velocity[Y] 0.98496E-13 c Velocity[Z] 0.98500E-13 c Pressure 0.75823E-14 16 0.58923E-07 0.58923E-07 0.96500E+00 c k 0.30897E-06 2 0.32500E-07 0.13850E-08 0.13221E+01 c omega 0.13153E+02 1 0.99648E-09 0.16546E+00 0.21177E-02 c TempK 0.94728E+02 1 0.81215E-07 0.18288E-01 0.14964E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.1389e-14 7.6418e-14 -9.4964e-18 -2.4717e-18 v Velocity[Y] -0.00012274 0.00011608 -5.3136e-10 -3.0876e-12 v Velocity[Z] -0.00011603 0.00012274 2.4968e-10 -1.8192e-12 v ǁVelocityǁ 3.0324e-10 0.00013159 1.1251e-05 8.1165e-06 v Pressure -0.0013821 0.023041 0.0013154 1.3041e-19 v k 6.4085e-10 0.0010288 0.00067266 0.00085719 v omega 13.155 1.0313e+05 2665.1 498.17 v TempK 288 342.09 294.15 291.09 v Density 1.205 1.205 1.205 1.205 v TurbVisc 7.5122e-15 9.425e-05 5.6145e-05 7.3397e-05 v CourantNb 2.9754e-09 0.00019399 1.3813e-05 8.6382e-06 v FourierNb 0.092731 0.6281 0.18549 0.15638 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.956 4.956 0.00055082 -5.6502e-07 v volume_forces[Z] -4.956 4.956 -0.00055071 6.7075e-07 v ǁvolume_forcesǁ 1.1036e-08 4.9571 0.5572 0.27757 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.36 291.23 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014999 5.3045e-05 2.9609e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.09275 0.6281 0.1855 0.15638 INSTANT 0.790623000E+00 TIME STEP NUMBER 821 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.37266E-05 0.22539E-02 Friction velocity uk : 0.37274E-05 0.22538E-02 Dimensionless distance yplus : 0.24823E-04 0.14995E-01 Friction thermal sca. tstar : -0.11321E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.17434E-04 0.10532E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.37266E-05 0.22539E-02 Friction velocity uk : 0.37274E-05 0.22538E-02 Dimensionless distance yplus : 0.24823E-04 0.14995E-01 Friction thermal sca. tstar : -0.11321E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.17434E-04 0.10532E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.37255E-08 3 0.10803E-06 0.19659E-12 0.88659E+00 c Velocity[X] 0.50935E-32 c Velocity[Y] 0.98291E-13 c Velocity[Z] 0.98295E-13 c Pressure 0.75683E-14 16 0.58814E-07 0.58814E-07 0.96377E+00 c k 0.30859E-06 2 0.32447E-07 0.13787E-08 0.13208E+01 c omega 0.13153E+02 1 0.99391E-09 0.16476E+00 0.21132E-02 c TempK 0.94728E+02 1 0.81074E-07 0.18255E-01 0.14950E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.1337e-14 7.6376e-14 -9.4914e-18 -2.4705e-18 v Velocity[Y] -0.00012271 0.00011605 -5.2898e-10 -3.0833e-12 v Velocity[Z] -0.000116 0.00012272 2.4717e-10 -1.8194e-12 v ǁVelocityǁ 3.0134e-10 0.00013156 1.1255e-05 8.1225e-06 v Pressure -0.0013837 0.023054 0.0013163 5.5106e-20 v k 6.3877e-10 0.0010276 0.00067176 0.00085608 v omega 13.142 1.0313e+05 2665.1 498.15 v TempK 288 342.09 294.16 291.1 v Density 1.205 1.205 1.205 1.205 v TurbVisc 7.4878e-15 9.424e-05 5.6128e-05 7.3376e-05 v CourantNb 2.978e-09 0.00019392 1.3813e-05 8.6417e-06 v FourierNb 0.092656 0.6281 0.18545 0.15634 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.956 4.9561 0.00055102 -5.6529e-07 v volume_forces[Z] -4.956 4.9561 -0.00055091 6.7104e-07 v ǁvolume_forcesǁ 1.0962e-08 4.9571 0.5574 0.27774 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.36 291.24 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014995 5.3033e-05 2.9602e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.092675 0.6281 0.18547 0.15635 INSTANT 0.791586000E+00 TIME STEP NUMBER 822 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.35768E-05 0.22533E-02 Friction velocity uk : 0.35777E-05 0.22533E-02 Dimensionless distance yplus : 0.23826E-04 0.14991E-01 Friction thermal sca. tstar : -0.11439E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.16734E-04 0.10529E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.35768E-05 0.22533E-02 Friction velocity uk : 0.35777E-05 0.22533E-02 Dimensionless distance yplus : 0.23826E-04 0.14991E-01 Friction thermal sca. tstar : -0.11439E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.16734E-04 0.10529E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.37269E-08 3 0.10778E-06 0.19618E-12 0.88554E+00 c Velocity[X] 0.50741E-32 c Velocity[Y] 0.98086E-13 c Velocity[Z] 0.98090E-13 c Pressure 0.75557E-14 16 0.58715E-07 0.58715E-07 0.96254E+00 c k 0.30820E-06 2 0.32393E-07 0.13725E-08 0.13195E+01 c omega 0.13153E+02 1 0.99136E-09 0.16406E+00 0.21087E-02 c TempK 0.94729E+02 1 0.80934E-07 0.18222E-01 0.14936E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.1285e-14 7.6335e-14 -9.4864e-18 -2.4694e-18 v Velocity[Y] -0.00012269 0.00011602 -5.2659e-10 -3.079e-12 v Velocity[Z] -0.00011597 0.00012269 2.4467e-10 -1.8195e-12 v ǁVelocityǁ 2.9961e-10 0.00013154 1.1259e-05 8.1285e-06 v Pressure -0.0013854 0.023068 0.0013173 1.9905e-20 v k 6.367e-10 0.0010265 0.00067086 0.00085497 v omega 13.128 1.0313e+05 2665.1 498.14 v TempK 288 342.09 294.16 291.1 v Density 1.205 1.205 1.205 1.205 v TurbVisc 7.4635e-15 9.4229e-05 5.611e-05 7.3356e-05 v CourantNb 2.9806e-09 0.00019385 1.3814e-05 8.6452e-06 v FourierNb 0.092582 0.6281 0.18542 0.1563 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9561 4.9561 0.00055122 -5.6555e-07 v volume_forces[Z] -4.9561 4.9561 -0.00055111 6.7133e-07 v ǁvolume_forcesǁ 1.0894e-08 4.9572 0.5576 0.27791 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.37 291.24 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014991 5.302e-05 2.9594e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.092601 0.6281 0.18543 0.15631 INSTANT 0.792549000E+00 TIME STEP NUMBER 823 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.34201E-05 0.22528E-02 Friction velocity uk : 0.34210E-05 0.22527E-02 Dimensionless distance yplus : 0.22782E-04 0.14988E-01 Friction thermal sca. tstar : -0.11561E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.16001E-04 0.10526E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.34201E-05 0.22528E-02 Friction velocity uk : 0.34210E-05 0.22527E-02 Dimensionless distance yplus : 0.22782E-04 0.14988E-01 Friction thermal sca. tstar : -0.11561E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.16001E-04 0.10526E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.37284E-08 3 0.10754E-06 0.19577E-12 0.88450E+00 c Velocity[X] 0.50547E-32 c Velocity[Y] 0.97882E-13 c Velocity[Z] 0.97886E-13 c Pressure 0.75437E-14 16 0.58621E-07 0.58621E-07 0.96132E+00 c k 0.30782E-06 2 0.32340E-07 0.13663E-08 0.13181E+01 c omega 0.13153E+02 1 0.98881E-09 0.16336E+00 0.21042E-02 c TempK 0.94729E+02 1 0.80794E-07 0.18189E-01 0.14923E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.1233e-14 7.6293e-14 -9.4815e-18 -2.4682e-18 v Velocity[Y] -0.00012266 0.00011599 -5.242e-10 -3.0748e-12 v Velocity[Z] -0.00011594 0.00012267 2.4216e-10 -1.8196e-12 v ǁVelocityǁ 2.9804e-10 0.00013151 1.1263e-05 8.1345e-06 v Pressure -0.0013871 0.023082 0.0013182 -6.0401e-20 v k 6.3464e-10 0.0010253 0.00066996 0.00085386 v omega 13.114 1.0313e+05 2665.1 498.13 v TempK 288 342.09 294.16 291.1 v Density 1.205 1.205 1.205 1.205 v TurbVisc 7.4394e-15 9.4219e-05 5.6092e-05 7.3335e-05 v CourantNb 2.9833e-09 0.00019378 1.3814e-05 8.6487e-06 v FourierNb 0.092507 0.6281 0.18538 0.15627 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9561 4.9561 0.00055142 -5.6582e-07 v volume_forces[Z] -4.9561 4.9561 -0.00055131 6.7163e-07 v ǁvolume_forcesǁ 1.0831e-08 4.9572 0.55779 0.27808 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.37 291.24 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014988 5.3008e-05 2.9587e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.092526 0.6281 0.1854 0.15628 INSTANT 0.793512000E+00 TIME STEP NUMBER 824 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.32554E-05 0.22522E-02 Friction velocity uk : 0.32564E-05 0.22522E-02 Dimensionless distance yplus : 0.21686E-04 0.14984E-01 Friction thermal sca. tstar : -0.11686E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.15231E-04 0.10524E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.32554E-05 0.22522E-02 Friction velocity uk : 0.32564E-05 0.22522E-02 Dimensionless distance yplus : 0.21686E-04 0.14984E-01 Friction thermal sca. tstar : -0.11686E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.15231E-04 0.10524E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.37298E-08 3 0.10730E-06 0.19536E-12 0.88345E+00 c Velocity[X] 0.50355E-32 c Velocity[Y] 0.97678E-13 c Velocity[Z] 0.97682E-13 c Pressure 0.75277E-14 16 0.58496E-07 0.58496E-07 0.96009E+00 c k 0.30743E-06 2 0.32288E-07 0.13601E-08 0.13168E+01 c omega 0.13153E+02 1 0.98627E-09 0.16267E+00 0.20997E-02 c TempK 0.94730E+02 1 0.80655E-07 0.18155E-01 0.14909E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.1182e-14 7.6252e-14 -9.4765e-18 -2.467e-18 v Velocity[Y] -0.00012264 0.00011596 -5.218e-10 -3.0705e-12 v Velocity[Z] -0.00011591 0.00012264 2.3965e-10 -1.8197e-12 v ǁVelocityǁ 2.9664e-10 0.00013148 1.1266e-05 8.1405e-06 v Pressure -0.0013887 0.023095 0.0013192 -4.2163e-20 v k 6.3259e-10 0.0010241 0.00066907 0.00085276 v omega 13.101 1.0313e+05 2665.1 498.12 v TempK 288 342.09 294.16 291.1 v Density 1.205 1.205 1.205 1.205 v TurbVisc 7.4153e-15 9.4209e-05 5.6075e-05 7.3314e-05 v CourantNb 2.9859e-09 0.00019371 1.3815e-05 8.6522e-06 v FourierNb 0.092433 0.6281 0.18535 0.15623 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9562 4.9562 0.00055162 -5.6609e-07 v volume_forces[Z] -4.9562 4.9562 -0.00055151 6.7192e-07 v ǁvolume_forcesǁ 1.0774e-08 4.9572 0.55799 0.27825 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.37 291.24 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014984 5.2995e-05 2.9579e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.092452 0.6281 0.18536 0.15624 INSTANT 0.794475000E+00 TIME STEP NUMBER 825 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.30815E-05 0.22517E-02 Friction velocity uk : 0.30825E-05 0.22517E-02 Dimensionless distance yplus : 0.20528E-04 0.14981E-01 Friction thermal sca. tstar : -0.11815E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.14418E-04 0.10521E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.30815E-05 0.22517E-02 Friction velocity uk : 0.30825E-05 0.22517E-02 Dimensionless distance yplus : 0.20528E-04 0.14981E-01 Friction thermal sca. tstar : -0.11815E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.14418E-04 0.10521E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.37313E-08 3 0.10705E-06 0.19495E-12 0.88240E+00 c Velocity[X] 0.50164E-32 c Velocity[Y] 0.97474E-13 c Velocity[Z] 0.97478E-13 c Pressure 0.75145E-14 16 0.58393E-07 0.58393E-07 0.95887E+00 c k 0.30705E-06 2 0.32235E-07 0.13540E-08 0.13155E+01 c omega 0.13153E+02 1 0.98374E-09 0.16198E+00 0.20953E-02 c TempK 0.94730E+02 1 0.80516E-07 0.18122E-01 0.14895E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.113e-14 7.621e-14 -9.4716e-18 -2.4659e-18 v Velocity[Y] -0.00012262 0.00011594 -5.1941e-10 -3.0663e-12 v Velocity[Z] -0.00011588 0.00012262 2.3713e-10 -1.8198e-12 v ǁVelocityǁ 2.9542e-10 0.00013146 1.127e-05 8.1465e-06 v Pressure -0.0013904 0.023109 0.0013201 7.6089e-20 v k 6.3055e-10 0.001023 0.00066818 0.00085166 v omega 13.087 1.0313e+05 2665.1 498.11 v TempK 288 342.09 294.16 291.1 v Density 1.205 1.205 1.205 1.205 v TurbVisc 7.3914e-15 9.4198e-05 5.6057e-05 7.3294e-05 v CourantNb 2.9885e-09 0.00019364 1.3815e-05 8.6557e-06 v FourierNb 0.092359 0.6281 0.18531 0.1562 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9562 4.9562 0.00055182 -5.6635e-07 v volume_forces[Z] -4.9562 4.9562 -0.00055171 6.7221e-07 v ǁvolume_forcesǁ 1.0724e-08 4.9573 0.55819 0.27841 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.37 291.24 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014981 5.2983e-05 2.9572e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.092378 0.6281 0.18533 0.15621 INSTANT 0.795438000E+00 TIME STEP NUMBER 826 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.28966E-05 0.22512E-02 Friction velocity uk : 0.28977E-05 0.22511E-02 Dimensionless distance yplus : 0.19298E-04 0.14977E-01 Friction thermal sca. tstar : -0.11948E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.13553E-04 0.10519E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.28966E-05 0.22512E-02 Friction velocity uk : 0.28977E-05 0.22511E-02 Dimensionless distance yplus : 0.19298E-04 0.14977E-01 Friction thermal sca. tstar : -0.11948E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.13553E-04 0.10519E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.37328E-08 3 0.10681E-06 0.19454E-12 0.88135E+00 c Velocity[X] 0.49973E-32 c Velocity[Y] 0.97270E-13 c Velocity[Z] 0.97274E-13 c Pressure 0.75014E-14 16 0.58290E-07 0.58290E-07 0.95766E+00 c k 0.30667E-06 2 0.32182E-07 0.13479E-08 0.13141E+01 c omega 0.13153E+02 1 0.98122E-09 0.16129E+00 0.20908E-02 c TempK 0.94731E+02 1 0.80378E-07 0.18090E-01 0.14882E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.1078e-14 7.6169e-14 -9.4667e-18 -2.4647e-18 v Velocity[Y] -0.00012259 0.00011591 -5.1701e-10 -3.0621e-12 v Velocity[Z] -0.00011585 0.0001226 2.3462e-10 -1.82e-12 v ǁVelocityǁ 2.9436e-10 0.00013143 1.1274e-05 8.1525e-06 v Pressure -0.001392 0.023123 0.001321 -7.5207e-20 v k 6.2852e-10 0.0010218 0.00066729 0.00085057 v omega 13.074 1.0313e+05 2665.1 498.09 v TempK 288 342.09 294.17 291.1 v Density 1.205 1.205 1.205 1.205 v TurbVisc 7.3675e-15 9.4188e-05 5.604e-05 7.3273e-05 v CourantNb 2.9911e-09 0.00019357 1.3815e-05 8.6592e-06 v FourierNb 0.092285 0.6281 0.18528 0.15616 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9563 4.9563 0.00055202 -5.6662e-07 v volume_forces[Z] -4.9563 4.9563 -0.00055191 6.725e-07 v ǁvolume_forcesǁ 1.0679e-08 4.9573 0.55839 0.27858 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.37 291.25 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014977 5.297e-05 2.9564e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.092304 0.6281 0.18529 0.15617 INSTANT 0.796401000E+00 TIME STEP NUMBER 827 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.26987E-05 0.22506E-02 Friction velocity uk : 0.26999E-05 0.22506E-02 Dimensionless distance yplus : 0.17980E-04 0.14974E-01 Friction thermal sca. tstar : -0.12084E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.12628E-04 0.10516E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.26987E-05 0.22506E-02 Friction velocity uk : 0.26999E-05 0.22506E-02 Dimensionless distance yplus : 0.17980E-04 0.14974E-01 Friction thermal sca. tstar : -0.12084E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.12628E-04 0.10516E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.37342E-08 3 0.10657E-06 0.19414E-12 0.88030E+00 c Velocity[X] 0.49784E-32 c Velocity[Y] 0.97066E-13 c Velocity[Z] 0.97070E-13 c Pressure 0.74946E-14 16 0.58237E-07 0.58237E-07 0.95644E+00 c k 0.30629E-06 2 0.32130E-07 0.13418E-08 0.13128E+01 c omega 0.13153E+02 1 0.97871E-09 0.16061E+00 0.20864E-02 c TempK 0.94732E+02 1 0.80240E-07 0.18057E-01 0.14868E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.1027e-14 7.6128e-14 -9.4618e-18 -2.4635e-18 v Velocity[Y] -0.00012257 0.00011588 -5.1461e-10 -3.0579e-12 v Velocity[Z] -0.00011582 0.00012257 2.3211e-10 -1.8201e-12 v ǁVelocityǁ 2.9349e-10 0.0001314 1.1278e-05 8.1585e-06 v Pressure -0.0013937 0.023136 0.001322 9.8053e-21 v k 6.2649e-10 0.0010206 0.0006664 0.00084947 v omega 13.06 1.0313e+05 2665 498.08 v TempK 288 342.09 294.17 291.11 v Density 1.205 1.205 1.205 1.205 v TurbVisc 7.3438e-15 9.4178e-05 5.6023e-05 7.3252e-05 v CourantNb 2.9937e-09 0.0001935 1.3816e-05 8.6627e-06 v FourierNb 0.092211 0.6281 0.18524 0.15613 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9563 4.9563 0.00055222 -5.6688e-07 v volume_forces[Z] -4.9563 4.9563 -0.00055211 6.7279e-07 v ǁvolume_forcesǁ 1.0641e-08 4.9574 0.55859 0.27875 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.38 291.25 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014974 5.2958e-05 2.9557e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.09223 0.6281 0.18526 0.15613 INSTANT 0.797364000E+00 TIME STEP NUMBER 828 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.24844E-05 0.22501E-02 Friction velocity uk : 0.24857E-05 0.22501E-02 Dimensionless distance yplus : 0.16554E-04 0.14970E-01 Friction thermal sca. tstar : -0.12225E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.11626E-04 0.10514E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.24844E-05 0.22501E-02 Friction velocity uk : 0.24857E-05 0.22501E-02 Dimensionless distance yplus : 0.16554E-04 0.14970E-01 Friction thermal sca. tstar : -0.12225E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.11626E-04 0.10514E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.37357E-08 3 0.10634E-06 0.19373E-12 0.87926E+00 c Velocity[X] 0.49594E-32 c Velocity[Y] 0.96863E-13 c Velocity[Z] 0.96867E-13 c Pressure 0.74774E-14 16 0.58102E-07 0.58102E-07 0.95523E+00 c k 0.30591E-06 2 0.32078E-07 0.13358E-08 0.13115E+01 c omega 0.13153E+02 1 0.97621E-09 0.15993E+00 0.20820E-02 c TempK 0.94732E+02 1 0.80102E-07 0.18024E-01 0.14854E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.0975e-14 7.6087e-14 -9.4569e-18 -2.4624e-18 v Velocity[Y] -0.00012254 0.00011585 -5.1221e-10 -3.0537e-12 v Velocity[Z] -0.0001158 0.00012255 2.2959e-10 -1.8202e-12 v ǁVelocityǁ 2.928e-10 0.00013138 1.1281e-05 8.1645e-06 v Pressure -0.0013954 0.02315 0.0013229 -3.3436e-20 v k 6.2448e-10 0.0010195 0.00066551 0.00084838 v omega 13.047 1.0313e+05 2665 498.07 v TempK 288 342.09 294.17 291.11 v Density 1.205 1.205 1.205 1.205 v TurbVisc 7.3201e-15 9.4167e-05 5.6005e-05 7.3232e-05 v CourantNb 2.9963e-09 0.00019343 1.3816e-05 8.6662e-06 v FourierNb 0.092138 0.6281 0.18521 0.15609 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9564 4.9564 0.00055242 -5.6714e-07 v volume_forces[Z] -4.9564 4.9564 -0.00055231 6.7308e-07 v ǁvolume_forcesǁ 1.061e-08 4.9574 0.55879 0.27892 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.38 291.25 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.01497 5.2945e-05 2.9549e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.092157 0.6281 0.18522 0.1561 INSTANT 0.798327000E+00 TIME STEP NUMBER 829 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.22492E-05 0.22496E-02 Friction velocity uk : 0.22506E-05 0.22495E-02 Dimensionless distance yplus : 0.14988E-04 0.14966E-01 Friction thermal sca. tstar : -0.12370E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.10527E-04 0.10511E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.22492E-05 0.22496E-02 Friction velocity uk : 0.22506E-05 0.22495E-02 Dimensionless distance yplus : 0.14988E-04 0.14966E-01 Friction thermal sca. tstar : -0.12370E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.10527E-04 0.10511E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.37371E-08 3 0.10610E-06 0.19332E-12 0.87821E+00 c Velocity[X] 0.49409E-32 c Velocity[Y] 0.96660E-13 c Velocity[Z] 0.96664E-13 c Pressure 0.74615E-14 16 0.57978E-07 0.57978E-07 0.95402E+00 c k 0.30553E-06 2 0.32026E-07 0.13298E-08 0.13102E+01 c omega 0.13153E+02 1 0.97372E-09 0.15926E+00 0.20776E-02 c TempK 0.94733E+02 1 0.79965E-07 0.17991E-01 0.14841E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.0924e-14 7.6045e-14 -9.452e-18 -2.4612e-18 v Velocity[Y] -0.00012252 0.00011582 -5.0981e-10 -3.0497e-12 v Velocity[Z] -0.00011577 0.00012252 2.2708e-10 -1.8202e-12 v ǁVelocityǁ 2.9229e-10 0.00013135 1.1285e-05 8.1704e-06 v Pressure -0.001397 0.023164 0.0013239 -1.06e-19 v k 6.2247e-10 0.0010183 0.00066463 0.00084729 v omega 13.034 1.0313e+05 2665 498.06 v TempK 288 342.09 294.17 291.11 v Density 1.205 1.205 1.205 1.205 v TurbVisc 7.2966e-15 9.4157e-05 5.5988e-05 7.3211e-05 v CourantNb 2.9989e-09 0.00019336 1.3817e-05 8.6697e-06 v FourierNb 0.092064 0.6281 0.18518 0.15605 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9564 4.9564 0.00055262 -5.6741e-07 v volume_forces[Z] -4.9564 4.9564 -0.00055251 6.7337e-07 v ǁvolume_forcesǁ 1.0585e-08 4.9575 0.55898 0.27908 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.38 291.25 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014966 5.2933e-05 2.9542e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.092083 0.6281 0.18519 0.15606 INSTANT 0.799290000E+00 TIME STEP NUMBER 830 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19857E-05 0.22490E-02 Friction velocity uk : 0.19873E-05 0.22490E-02 Dimensionless distance yplus : 0.13234E-04 0.14963E-01 Friction thermal sca. tstar : -0.12520E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.92950E-05 0.10509E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19857E-05 0.22490E-02 Friction velocity uk : 0.19873E-05 0.22490E-02 Dimensionless distance yplus : 0.13234E-04 0.14963E-01 Friction thermal sca. tstar : -0.12520E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.92950E-05 0.10509E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.37386E-08 3 0.10586E-06 0.19292E-12 0.87716E+00 c Velocity[X] 0.49222E-32 c Velocity[Y] 0.96457E-13 c Velocity[Z] 0.96461E-13 c Pressure 0.74671E-14 16 0.58021E-07 0.58021E-07 0.95282E+00 c k 0.30515E-06 2 0.31974E-07 0.13238E-08 0.13089E+01 c omega 0.13153E+02 1 0.97123E-09 0.15859E+00 0.20732E-02 c TempK 0.94733E+02 1 0.79828E-07 0.17959E-01 0.14827E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.0873e-14 7.6004e-14 -9.4471e-18 -2.4601e-18 v Velocity[Y] -0.0001225 0.00011579 -5.074e-10 -3.0456e-12 v Velocity[Z] -0.00011574 0.0001225 2.2456e-10 -1.8203e-12 v ǁVelocityǁ 2.9197e-10 0.00013132 1.1289e-05 8.1764e-06 v Pressure -0.0013987 0.023177 0.0013248 3.4417e-20 v k 6.2048e-10 0.0010172 0.00066375 0.0008462 v omega 13.02 1.0313e+05 2665 498.05 v TempK 288 342.09 294.18 291.11 v Density 1.205 1.205 1.205 1.205 v TurbVisc 7.2732e-15 9.4147e-05 5.597e-05 7.3191e-05 v CourantNb 3.0015e-09 0.00019329 1.3817e-05 8.6732e-06 v FourierNb 0.091991 0.6281 0.18514 0.15602 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9565 4.9565 0.00055282 -5.6767e-07 v volume_forces[Z] -4.9565 4.9565 -0.00055271 6.7366e-07 v ǁvolume_forcesǁ 1.0566e-08 4.9575 0.55918 0.27925 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.38 291.25 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014963 5.292e-05 2.9534e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.09201 0.6281 0.18515 0.15603 INSTANT 0.800253000E+00 TIME STEP NUMBER 831 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.16805E-05 0.22485E-02 Friction velocity uk : 0.16824E-05 0.22485E-02 Dimensionless distance yplus : 0.11204E-04 0.14959E-01 Friction thermal sca. tstar : -0.12674E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.78690E-05 0.10506E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.16805E-05 0.22485E-02 Friction velocity uk : 0.16824E-05 0.22485E-02 Dimensionless distance yplus : 0.11204E-04 0.14959E-01 Friction thermal sca. tstar : -0.12674E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.78690E-05 0.10506E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.37401E-08 3 0.10562E-06 0.19251E-12 0.87611E+00 c Velocity[X] 0.49036E-32 c Velocity[Y] 0.96254E-13 c Velocity[Z] 0.96259E-13 c Pressure 0.74542E-14 16 0.57920E-07 0.57920E-07 0.95162E+00 c k 0.30477E-06 2 0.31922E-07 0.13179E-08 0.13075E+01 c omega 0.13153E+02 1 0.96875E-09 0.15792E+00 0.20688E-02 c TempK 0.94734E+02 1 0.79691E-07 0.17927E-01 0.14814E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.0822e-14 7.5964e-14 -9.4422e-18 -2.4589e-18 v Velocity[Y] -0.00012247 0.00011577 -5.0499e-10 -3.0416e-12 v Velocity[Z] -0.00011571 0.00012248 2.2204e-10 -1.8203e-12 v ǁVelocityǁ 2.9184e-10 0.0001313 1.1292e-05 8.1824e-06 v Pressure -0.0014003 0.023191 0.0013257 1.765e-20 v k 6.1849e-10 0.001016 0.00066287 0.00084512 v omega 13.007 1.0313e+05 2665 498.04 v TempK 288 342.09 294.18 291.11 v Density 1.205 1.205 1.205 1.205 v TurbVisc 7.2498e-15 9.4137e-05 5.5953e-05 7.317e-05 v CourantNb 3.004e-09 0.00019322 1.3818e-05 8.6767e-06 v FourierNb 0.091918 0.6281 0.18511 0.15598 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9565 4.9565 0.00055302 -5.6793e-07 v volume_forces[Z] -4.9565 4.9565 -0.00055291 6.7395e-07 v ǁvolume_forcesǁ 1.0555e-08 4.9576 0.55938 0.27942 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.39 291.26 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014959 5.2908e-05 2.9527e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.091937 0.6281 0.18512 0.15599 INSTANT 0.801216000E+00 TIME STEP NUMBER 832 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.13048E-05 0.22480E-02 Friction velocity uk : 0.13072E-05 0.22479E-02 Dimensionless distance yplus : 0.87057E-05 0.14956E-01 Friction thermal sca. tstar : -0.12834E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.61143E-05 0.10504E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.13048E-05 0.22480E-02 Friction velocity uk : 0.13072E-05 0.22479E-02 Dimensionless distance yplus : 0.87057E-05 0.14956E-01 Friction thermal sca. tstar : -0.12834E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.61143E-05 0.10504E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.37415E-08 3 0.10538E-06 0.19211E-12 0.87506E+00 c Velocity[X] 0.48851E-32 c Velocity[Y] 0.96052E-13 c Velocity[Z] 0.96056E-13 c Pressure 0.74398E-14 16 0.57808E-07 0.57808E-07 0.95042E+00 c k 0.30440E-06 2 0.31870E-07 0.13120E-08 0.13062E+01 c omega 0.13153E+02 1 0.96629E-09 0.15725E+00 0.20645E-02 c TempK 0.94734E+02 1 0.79555E-07 0.17894E-01 0.14800E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.0771e-14 7.5923e-14 -9.4373e-18 -2.4578e-18 v Velocity[Y] -0.00012245 0.00011574 -5.0258e-10 -3.0376e-12 v Velocity[Z] -0.00011568 0.00012245 2.1952e-10 -1.8206e-12 v ǁVelocityǁ 2.919e-10 0.00013127 1.1296e-05 8.1884e-06 v Pressure -0.001402 0.023204 0.0013267 -4.2163e-21 v k 6.1651e-10 0.0010149 0.00066199 0.00084404 v omega 12.994 1.0313e+05 2665 498.02 v TempK 288 342.1 294.18 291.12 v Density 1.205 1.205 1.205 1.205 v TurbVisc 7.2266e-15 9.4127e-05 5.5935e-05 7.315e-05 v CourantNb 3.0066e-09 0.00019315 1.3818e-05 8.6802e-06 v FourierNb 0.091846 0.6281 0.18507 0.15595 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9565 4.9566 0.00055322 -5.6819e-07 v volume_forces[Z] -4.9565 4.9566 -0.00055311 6.7423e-07 v ǁvolume_forcesǁ 1.055e-08 4.9576 0.55958 0.27959 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.39 291.26 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014956 5.2896e-05 2.9519e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.091865 0.6281 0.18509 0.15596 INSTANT 0.802179000E+00 TIME STEP NUMBER 833 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.76027E-06 0.22474E-02 Friction velocity uk : 0.76451E-06 0.22474E-02 Dimensionless distance yplus : 0.50913E-05 0.14952E-01 Friction thermal sca. tstar : -0.12999E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.35758E-05 0.10502E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.76027E-06 0.22474E-02 Friction velocity uk : 0.76451E-06 0.22474E-02 Dimensionless distance yplus : 0.50913E-05 0.14952E-01 Friction thermal sca. tstar : -0.12999E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.35758E-05 0.10502E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.37430E-08 3 0.10519E-06 0.19170E-12 0.87402E+00 c Velocity[X] 0.48667E-32 c Velocity[Y] 0.95850E-13 c Velocity[Z] 0.95854E-13 c Pressure 0.75438E-14 16 0.58614E-07 0.58614E-07 0.94922E+00 c k 0.30402E-06 2 0.31819E-07 0.13061E-08 0.13049E+01 c omega 0.13153E+02 1 0.96383E-09 0.15659E+00 0.20601E-02 c TempK 0.94735E+02 1 0.79419E-07 0.17862E-01 0.14787E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.072e-14 7.5882e-14 -9.4325e-18 -2.4566e-18 v Velocity[Y] -0.00012242 0.00011571 -5.0017e-10 -3.0335e-12 v Velocity[Z] -0.00011566 0.00012243 2.1701e-10 -1.8207e-12 v ǁVelocityǁ 2.9215e-10 0.00013124 1.13e-05 8.1943e-06 v Pressure -0.0014036 0.023218 0.0013276 1.4512e-20 v k 6.1454e-10 0.0010137 0.00066111 0.00084296 v omega 12.98 1.0313e+05 2665 498.01 v TempK 288 342.1 294.18 291.12 v Density 1.205 1.205 1.205 1.205 v TurbVisc 7.2035e-15 9.4116e-05 5.5918e-05 7.3129e-05 v CourantNb 3.0092e-09 0.00019308 1.3818e-05 8.6837e-06 v FourierNb 0.091773 0.6281 0.18504 0.15591 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9566 4.9566 0.00055341 -5.6846e-07 v volume_forces[Z] -4.9566 4.9566 -0.00055331 6.7452e-07 v ǁvolume_forcesǁ 1.0552e-08 4.9577 0.55977 0.27975 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.39 291.26 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014952 5.2883e-05 2.9512e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.091792 0.6281 0.18505 0.15592 INSTANT 0.803142000E+00 TIME STEP NUMBER 834 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.73672E-06 0.22469E-02 Friction velocity uk : 0.74107E-06 0.22469E-02 Dimensionless distance yplus : 0.49352E-05 0.14949E-01 Friction thermal sca. tstar : -0.13170E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.34662E-05 0.10499E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.73672E-06 0.22469E-02 Friction velocity uk : 0.74107E-06 0.22469E-02 Dimensionless distance yplus : 0.49352E-05 0.14949E-01 Friction thermal sca. tstar : -0.13170E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.34662E-05 0.10499E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.37444E-08 3 0.10491E-06 0.19130E-12 0.87297E+00 c Velocity[X] 0.48484E-32 c Velocity[Y] 0.95648E-13 c Velocity[Z] 0.95652E-13 c Pressure 0.73993E-14 16 0.57491E-07 0.57491E-07 0.94803E+00 c k 0.30365E-06 2 0.31767E-07 0.13002E-08 0.13036E+01 c omega 0.13153E+02 1 0.96138E-09 0.15593E+00 0.20558E-02 c TempK 0.94735E+02 1 0.79284E-07 0.17830E-01 0.14774E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.0669e-14 7.5841e-14 -9.4276e-18 -2.4555e-18 v Velocity[Y] -0.0001224 0.00011568 -4.9776e-10 -3.0295e-12 v Velocity[Z] -0.00011563 0.0001224 2.1449e-10 -1.8208e-12 v ǁVelocityǁ 2.9259e-10 0.00013122 1.1304e-05 8.2003e-06 v Pressure -0.0014053 0.023231 0.0013285 9.5209e-20 v k 6.1258e-10 0.0010126 0.00066024 0.00084188 v omega 12.967 1.0313e+05 2665 498 v TempK 288 342.1 294.18 291.12 v Density 1.205 1.205 1.205 1.205 v TurbVisc 7.1804e-15 9.4106e-05 5.5901e-05 7.3109e-05 v CourantNb 3.0117e-09 0.00019301 1.3819e-05 8.6871e-06 v FourierNb 0.091701 0.6281 0.185 0.15588 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9566 4.9567 0.00055361 -5.6872e-07 v volume_forces[Z] -4.9566 4.9567 -0.00055351 6.7481e-07 v ǁvolume_forcesǁ 1.0561e-08 4.9577 0.55997 0.27992 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.39 291.26 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014949 5.2871e-05 2.9504e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.09172 0.6281 0.18502 0.15589 INSTANT 0.804105000E+00 TIME STEP NUMBER 835 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12934E-05 0.22464E-02 Friction velocity uk : 0.12958E-05 0.22463E-02 Dimensionless distance yplus : 0.86296E-05 0.14945E-01 Friction thermal sca. tstar : -0.13347E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.60609E-05 0.10497E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12934E-05 0.22464E-02 Friction velocity uk : 0.12958E-05 0.22463E-02 Dimensionless distance yplus : 0.86296E-05 0.14945E-01 Friction thermal sca. tstar : -0.13347E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.60609E-05 0.10497E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.37459E-08 3 0.16841E-06 0.19090E-12 0.87192E+00 c Velocity[X] 0.48303E-32 c Velocity[Y] 0.95446E-13 c Velocity[Z] 0.95451E-13 c Pressure 0.73878E-14 16 0.57401E-07 0.57401E-07 0.94684E+00 c k 0.30327E-06 2 0.31716E-07 0.12944E-08 0.13023E+01 c omega 0.13153E+02 1 0.95894E-09 0.15528E+00 0.20515E-02 c TempK 0.94736E+02 1 0.79149E-07 0.17798E-01 0.14760E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.0618e-14 7.5801e-14 -9.4228e-18 -2.4543e-18 v Velocity[Y] -0.00012238 0.00011566 -4.9534e-10 -3.0255e-12 v Velocity[Z] -0.0001156 0.00012238 2.1196e-10 -1.821e-12 v ǁVelocityǁ 2.9323e-10 0.00013119 1.1307e-05 8.2062e-06 v Pressure -0.001407 0.023245 0.0013295 3.5103e-20 v k 6.1062e-10 0.0010114 0.00065937 0.00084081 v omega 12.954 1.0313e+05 2665 497.99 v TempK 288 342.1 294.19 291.12 v Density 1.205 1.205 1.205 1.205 v TurbVisc 7.1575e-15 9.4096e-05 5.5884e-05 7.3088e-05 v CourantNb 3.0143e-09 0.00019294 1.3819e-05 8.6906e-06 v FourierNb 0.091629 0.6281 0.18497 0.15584 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9567 4.9567 0.00055381 -5.6898e-07 v volume_forces[Z] -4.9567 4.9567 -0.0005537 6.7509e-07 v ǁvolume_forcesǁ 1.0577e-08 4.9577 0.56017 0.28009 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.39 291.26 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014945 5.2859e-05 2.9497e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.091648 0.6281 0.18498 0.15585 INSTANT 0.805068000E+00 TIME STEP NUMBER 836 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10023E-05 0.22458E-02 Friction velocity uk : 0.10055E-05 0.22458E-02 Dimensionless distance yplus : 0.66962E-05 0.14942E-01 Friction thermal sca. tstar : -0.13530E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.47030E-05 0.10494E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10023E-05 0.22458E-02 Friction velocity uk : 0.10055E-05 0.22458E-02 Dimensionless distance yplus : 0.66962E-05 0.14942E-01 Friction thermal sca. tstar : -0.13530E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.47030E-05 0.10494E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.37474E-08 3 0.16810E-06 0.19049E-12 0.87087E+00 c Velocity[X] 0.48124E-32 c Velocity[Y] 0.95245E-13 c Velocity[Z] 0.95249E-13 c Pressure 0.73803E-14 16 0.57342E-07 0.57342E-07 0.94565E+00 c k 0.30290E-06 2 0.31665E-07 0.12887E-08 0.13010E+01 c omega 0.13153E+02 1 0.95650E-09 0.15463E+00 0.20472E-02 c TempK 0.94736E+02 1 0.79015E-07 0.17766E-01 0.14747E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.0568e-14 7.576e-14 -9.4179e-18 -2.4532e-18 v Velocity[Y] -0.00012235 0.00011563 -4.9293e-10 -3.0215e-12 v Velocity[Z] -0.00011557 0.00012236 2.0944e-10 -1.821e-12 v ǁVelocityǁ 2.9406e-10 0.00013117 1.1311e-05 8.2122e-06 v Pressure -0.0014086 0.023258 0.0013304 -7.5991e-20 v k 6.0868e-10 0.0010103 0.0006585 0.00083973 v omega 12.941 1.0313e+05 2665 497.98 v TempK 288 342.1 294.19 291.12 v Density 1.205 1.205 1.205 1.205 v TurbVisc 7.1347e-15 9.4086e-05 5.5866e-05 7.3068e-05 v CourantNb 3.0169e-09 0.00019288 1.382e-05 8.6941e-06 v FourierNb 0.091557 0.6281 0.18494 0.15581 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9567 4.9567 0.00055401 -5.6924e-07 v volume_forces[Z] -4.9567 4.9567 -0.0005539 6.7538e-07 v ǁvolume_forcesǁ 1.06e-08 4.9578 0.56036 0.28025 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.4 291.26 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014942 5.2846e-05 2.949e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.091576 0.6281 0.18495 0.15582 INSTANT 0.806031000E+00 TIME STEP NUMBER 837 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.38345E-06 0.22453E-02 Friction velocity uk : 0.39160E-06 0.22453E-02 Dimensionless distance yplus : 0.26079E-05 0.14938E-01 Friction thermal sca. tstar : -0.13720E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.18316E-05 0.10492E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.38345E-06 0.22453E-02 Friction velocity uk : 0.39160E-06 0.22453E-02 Dimensionless distance yplus : 0.26079E-05 0.14938E-01 Friction thermal sca. tstar : -0.13720E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.18316E-05 0.10492E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.37488E-08 3 0.22405E-06 0.19009E-12 0.86982E+00 c Velocity[X] 0.47944E-32 c Velocity[Y] 0.95043E-13 c Velocity[Z] 0.95047E-13 c Pressure 0.73863E-14 16 0.57388E-07 0.57388E-07 0.94447E+00 c k 0.30253E-06 2 0.31614E-07 0.12829E-08 0.12997E+01 c omega 0.13153E+02 1 0.95408E-09 0.15398E+00 0.20429E-02 c TempK 0.94737E+02 1 0.78881E-07 0.17734E-01 0.14734E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.0517e-14 7.572e-14 -9.4131e-18 -2.452e-18 v Velocity[Y] -0.00012233 0.0001156 -4.9051e-10 -3.0175e-12 v Velocity[Z] -0.00011554 0.00012233 2.0692e-10 -1.8211e-12 v ǁVelocityǁ 2.9508e-10 0.00013114 1.1315e-05 8.2181e-06 v Pressure -0.0014103 0.023272 0.0013313 6.3342e-20 v k 6.0674e-10 0.0010092 0.00065763 0.00083866 v omega 12.928 1.0313e+05 2665 497.97 v TempK 288 342.1 294.19 291.13 v Density 1.205 1.205 1.205 1.205 v TurbVisc 7.112e-15 9.4076e-05 5.5849e-05 7.3047e-05 v CourantNb 3.0194e-09 0.00019281 1.382e-05 8.6976e-06 v FourierNb 0.091485 0.6281 0.1849 0.15577 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9568 4.9568 0.00055421 -5.695e-07 v volume_forces[Z] -4.9568 4.9568 -0.0005541 6.7566e-07 v ǁvolume_forcesǁ 1.063e-08 4.9578 0.56056 0.28042 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.4 291.27 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014938 5.2834e-05 2.9482e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.091504 0.6281 0.18492 0.15578 INSTANT 0.806994000E+00 TIME STEP NUMBER 838 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11370E-05 0.22448E-02 Friction velocity uk : 0.11397E-05 0.22447E-02 Dimensionless distance yplus : 0.75901E-05 0.14935E-01 Friction thermal sca. tstar : -0.13917E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.53308E-05 0.10489E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11370E-05 0.22448E-02 Friction velocity uk : 0.11397E-05 0.22447E-02 Dimensionless distance yplus : 0.75901E-05 0.14935E-01 Friction thermal sca. tstar : -0.13917E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.53308E-05 0.10489E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.37503E-08 3 0.16756E-06 0.18969E-12 0.86878E+00 c Velocity[X] 0.47764E-32 c Velocity[Y] 0.94842E-13 c Velocity[Z] 0.94847E-13 c Pressure 0.73537E-14 16 0.57134E-07 0.57134E-07 0.94328E+00 c k 0.30216E-06 2 0.31563E-07 0.12772E-08 0.12984E+01 c omega 0.13153E+02 1 0.95166E-09 0.15334E+00 0.20386E-02 c TempK 0.94738E+02 1 0.78747E-07 0.17702E-01 0.14720E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.0467e-14 7.5679e-14 -9.4083e-18 -2.4509e-18 v Velocity[Y] -0.00012231 0.00011557 -4.8809e-10 -3.0139e-12 v Velocity[Z] -0.00011552 0.00012231 2.044e-10 -1.8199e-12 v ǁVelocityǁ 2.9629e-10 0.00013111 1.1319e-05 8.2241e-06 v Pressure -0.0014119 0.023286 0.0013323 3.2063e-20 v k 6.0481e-10 0.001008 0.00065676 0.0008376 v omega 12.914 1.0313e+05 2664.9 497.95 v TempK 288 342.1 294.19 291.13 v Density 1.205 1.205 1.205 1.205 v TurbVisc 7.0893e-15 9.4065e-05 5.5832e-05 7.3027e-05 v CourantNb 3.022e-09 0.00019274 1.3821e-05 8.7011e-06 v FourierNb 0.091414 0.6281 0.18487 0.15574 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9568 4.9568 0.00055441 -5.6976e-07 v volume_forces[Z] -4.9568 4.9568 -0.0005543 6.7595e-07 v ǁvolume_forcesǁ 1.0667e-08 4.9579 0.56076 0.28058 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.4 291.27 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014935 5.2822e-05 2.9475e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.091433 0.6281 0.18488 0.15575 INSTANT 0.807957000E+00 TIME STEP NUMBER 839 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15641E-05 0.22443E-02 Friction velocity uk : 0.15661E-05 0.22442E-02 Dimensionless distance yplus : 0.10429E-04 0.14931E-01 Friction thermal sca. tstar : -0.14123E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.73249E-05 0.10487E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15641E-05 0.22443E-02 Friction velocity uk : 0.15661E-05 0.22442E-02 Dimensionless distance yplus : 0.10429E-04 0.14931E-01 Friction thermal sca. tstar : -0.14123E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.73249E-05 0.10487E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.37518E-08 3 0.22338E-06 0.18929E-12 0.86773E+00 c Velocity[X] 0.47585E-32 c Velocity[Y] 0.94641E-13 c Velocity[Z] 0.94646E-13 c Pressure 0.73560E-14 16 0.57151E-07 0.57151E-07 0.94211E+00 c k 0.30179E-06 2 0.31512E-07 0.12715E-08 0.12971E+01 c omega 0.13153E+02 1 0.94925E-09 0.15270E+00 0.20343E-02 c TempK 0.94738E+02 1 0.78613E-07 0.17671E-01 0.14707E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.0416e-14 7.5639e-14 -9.4035e-18 -2.4498e-18 v Velocity[Y] -0.00012228 0.00011555 -4.8567e-10 -3.0099e-12 v Velocity[Z] -0.00011549 0.00012229 2.0187e-10 -1.82e-12 v ǁVelocityǁ 2.977e-10 0.00013109 1.1322e-05 8.23e-06 v Pressure -0.0014136 0.023299 0.0013332 -1.158e-19 v k 6.0289e-10 0.0010069 0.0006559 0.00083653 v omega 12.901 1.0313e+05 2664.9 497.94 v TempK 288 342.1 294.2 291.13 v Density 1.205 1.205 1.205 1.205 v TurbVisc 7.0668e-15 9.4055e-05 5.5815e-05 7.3007e-05 v CourantNb 3.0245e-09 0.00019267 1.3821e-05 8.7046e-06 v FourierNb 0.091343 0.6281 0.18483 0.1557 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9569 4.9569 0.0005546 -5.7002e-07 v volume_forces[Z] -4.9569 4.9569 -0.0005545 6.7623e-07 v ǁvolume_forcesǁ 1.0711e-08 4.9579 0.56095 0.28075 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.4 291.27 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014931 5.2809e-05 2.9468e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.091361 0.6281 0.18485 0.15571 INSTANT 0.808920000E+00 TIME STEP NUMBER 840 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.18989E-05 0.22437E-02 Friction velocity uk : 0.19006E-05 0.22437E-02 Dimensionless distance yplus : 0.12657E-04 0.14928E-01 Friction thermal sca. tstar : -0.14336E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.88894E-05 0.10484E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.18989E-05 0.22437E-02 Friction velocity uk : 0.19006E-05 0.22437E-02 Dimensionless distance yplus : 0.12657E-04 0.14928E-01 Friction thermal sca. tstar : -0.14336E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.88894E-05 0.10484E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.37532E-08 3 0.18050E-06 0.18888E-12 0.86668E+00 c Velocity[X] 0.47407E-32 c Velocity[Y] 0.94440E-13 c Velocity[Z] 0.94445E-13 c Pressure 0.73312E-14 16 0.56957E-07 0.56957E-07 0.94093E+00 c k 0.30142E-06 2 0.31462E-07 0.12659E-08 0.12958E+01 c omega 0.13153E+02 1 0.94685E-09 0.15206E+00 0.20301E-02 c TempK 0.94739E+02 1 0.78480E-07 0.17639E-01 0.14694E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.0366e-14 7.5599e-14 -9.3987e-18 -2.4486e-18 v Velocity[Y] -0.00012226 0.00011552 -4.8324e-10 -3.0059e-12 v Velocity[Z] -0.00011546 0.00012226 1.9935e-10 -1.8201e-12 v ǁVelocityǁ 2.9909e-10 0.00013106 1.1326e-05 8.2359e-06 v Pressure -0.0014152 0.023313 0.0013341 -3.8143e-20 v k 6.0098e-10 0.0010058 0.00065504 0.00083547 v omega 12.888 1.0313e+05 2664.9 497.93 v TempK 288 342.1 294.2 291.13 v Density 1.205 1.205 1.205 1.205 v TurbVisc 7.0443e-15 9.4045e-05 5.5797e-05 7.2986e-05 v CourantNb 3.027e-09 0.0001926 1.3822e-05 8.708e-06 v FourierNb 0.091272 0.6281 0.1848 0.15567 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9569 4.9569 0.0005548 -5.7028e-07 v volume_forces[Z] -4.9569 4.9569 -0.00055469 6.7651e-07 v ǁvolume_forcesǁ 1.0762e-08 4.958 0.56115 0.28092 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.41 291.27 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014928 5.2797e-05 2.946e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.09129 0.6281 0.18481 0.15568 INSTANT 0.809883000E+00 TIME STEP NUMBER 841 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.21836E-05 0.22432E-02 Friction velocity uk : 0.21850E-05 0.22432E-02 Dimensionless distance yplus : 0.14551E-04 0.14924E-01 Friction thermal sca. tstar : -0.14558E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.10220E-04 0.10482E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.21836E-05 0.22432E-02 Friction velocity uk : 0.21850E-05 0.22432E-02 Dimensionless distance yplus : 0.14551E-04 0.14924E-01 Friction thermal sca. tstar : -0.14558E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.10220E-04 0.10482E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.37547E-08 3 0.18022E-06 0.18848E-12 0.86563E+00 c Velocity[X] 0.47234E-32 c Velocity[Y] 0.94239E-13 c Velocity[Z] 0.94244E-13 c Pressure 0.73166E-14 16 0.56843E-07 0.56843E-07 0.93976E+00 c k 0.30105E-06 2 0.31411E-07 0.12602E-08 0.12946E+01 c omega 0.13153E+02 1 0.94446E-09 0.15143E+00 0.20259E-02 c TempK 0.94739E+02 1 0.78348E-07 0.17608E-01 0.14681E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.0316e-14 7.5559e-14 -9.3939e-18 -2.4475e-18 v Velocity[Y] -0.00012223 0.00011549 -4.8082e-10 -3.0019e-12 v Velocity[Z] -0.00011543 0.00012224 1.9682e-10 -1.8201e-12 v ǁVelocityǁ 2.9792e-10 0.00013104 1.133e-05 8.2419e-06 v Pressure -0.0014169 0.023326 0.0013351 -4.1182e-21 v k 5.9907e-10 0.0010046 0.00065418 0.00083441 v omega 12.875 1.0313e+05 2664.9 497.92 v TempK 288 342.1 294.2 291.13 v Density 1.205 1.205 1.205 1.205 v TurbVisc 7.022e-15 9.4035e-05 5.578e-05 7.2966e-05 v CourantNb 3.0295e-09 0.00019253 1.3822e-05 8.7115e-06 v FourierNb 0.091201 0.6281 0.18477 0.15563 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.957 4.957 0.000555 -5.7054e-07 v volume_forces[Z] -4.957 4.957 -0.00055489 6.768e-07 v ǁvolume_forcesǁ 1.0812e-08 4.958 0.56134 0.28108 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.41 291.27 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014924 5.2785e-05 2.9453e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.091219 0.6281 0.18478 0.15564 INSTANT 0.810846000E+00 TIME STEP NUMBER 842 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.24357E-05 0.22427E-02 Friction velocity uk : 0.24370E-05 0.22426E-02 Dimensionless distance yplus : 0.16229E-04 0.14921E-01 Friction thermal sca. tstar : -0.14790E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.11398E-04 0.10479E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.24357E-05 0.22427E-02 Friction velocity uk : 0.24370E-05 0.22426E-02 Dimensionless distance yplus : 0.16229E-04 0.14921E-01 Friction thermal sca. tstar : -0.14790E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.11398E-04 0.10479E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.37562E-08 3 0.10306E-06 0.18808E-12 0.86458E+00 c Velocity[X] 0.47057E-32 c Velocity[Y] 0.94039E-13 c Velocity[Z] 0.94044E-13 c Pressure 0.73090E-14 16 0.56784E-07 0.56784E-07 0.93859E+00 c k 0.30068E-06 2 0.31361E-07 0.12547E-08 0.12933E+01 c omega 0.13153E+02 1 0.94208E-09 0.15080E+00 0.20216E-02 c TempK 0.94740E+02 1 0.78216E-07 0.17576E-01 0.14667E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.0266e-14 7.5519e-14 -9.3891e-18 -2.4464e-18 v Velocity[Y] -0.00012221 0.00011546 -4.7839e-10 -2.9979e-12 v Velocity[Z] -0.00011541 0.00012222 1.943e-10 -1.8202e-12 v ǁVelocityǁ 2.963e-10 0.00013101 1.1334e-05 8.2478e-06 v Pressure -0.0014186 0.023339 0.001336 -1.005e-19 v k 5.9718e-10 0.0010035 0.00065332 0.00083335 v omega 12.862 1.0313e+05 2664.9 497.91 v TempK 288 342.1 294.2 291.14 v Density 1.205 1.205 1.205 1.205 v TurbVisc 6.9997e-15 9.4025e-05 5.5763e-05 7.2946e-05 v CourantNb 3.0321e-09 0.00019247 1.3823e-05 8.715e-06 v FourierNb 0.09113 0.6281 0.18473 0.1556 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.957 4.957 0.0005552 -5.7079e-07 v volume_forces[Z] -4.957 4.957 -0.00055509 6.7708e-07 v ǁvolume_forcesǁ 1.077e-08 4.9581 0.56154 0.28125 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.41 291.28 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014921 5.2773e-05 2.9445e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.091149 0.6281 0.18475 0.15561 INSTANT 0.811809000E+00 TIME STEP NUMBER 843 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.26647E-05 0.22421E-02 Friction velocity uk : 0.26658E-05 0.22421E-02 Dimensionless distance yplus : 0.17753E-04 0.14917E-01 Friction thermal sca. tstar : -0.15032E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.12468E-04 0.10477E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.26647E-05 0.22421E-02 Friction velocity uk : 0.26658E-05 0.22421E-02 Dimensionless distance yplus : 0.17753E-04 0.14917E-01 Friction thermal sca. tstar : -0.15032E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.12468E-04 0.10477E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.37576E-08 3 0.17963E-06 0.18768E-12 0.86354E+00 c Velocity[X] 0.46883E-32 c Velocity[Y] 0.93839E-13 c Velocity[Z] 0.93844E-13 c Pressure 0.72844E-14 16 0.56592E-07 0.56592E-07 0.93742E+00 c k 0.30031E-06 2 0.31311E-07 0.12491E-08 0.12920E+01 c omega 0.13153E+02 1 0.93970E-09 0.15017E+00 0.20174E-02 c TempK 0.94740E+02 1 0.78084E-07 0.17545E-01 0.14654E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.0215e-14 7.5479e-14 -9.3843e-18 -2.4452e-18 v Velocity[Y] -0.00012219 0.00011544 -4.7596e-10 -2.9939e-12 v Velocity[Z] -0.00011538 0.00012219 1.9177e-10 -1.8203e-12 v ǁVelocityǁ 2.9492e-10 0.00013099 1.1337e-05 8.2537e-06 v Pressure -0.0014202 0.023353 0.0013369 1.5031e-19 v k 5.9529e-10 0.0010024 0.00065247 0.0008323 v omega 12.849 1.0313e+05 2664.9 497.9 v TempK 288 342.1 294.2 291.14 v Density 1.205 1.205 1.205 1.205 v TurbVisc 6.9776e-15 9.4015e-05 5.5746e-05 7.2926e-05 v CourantNb 3.0346e-09 0.0001924 1.3823e-05 8.7185e-06 v FourierNb 0.091059 0.6281 0.1847 0.15556 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.957 4.9571 0.00055539 -5.7105e-07 v volume_forces[Z] -4.957 4.9571 -0.00055529 6.7736e-07 v ǁvolume_forcesǁ 1.0711e-08 4.9581 0.56174 0.28141 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.41 291.28 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014917 5.2761e-05 2.9438e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.091078 0.6281 0.18471 0.15557 INSTANT 0.812772000E+00 TIME STEP NUMBER 844 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.27511E-05 0.22416E-02 Friction velocity uk : 0.27522E-05 0.22416E-02 Dimensionless distance yplus : 0.18328E-04 0.14914E-01 Friction thermal sca. tstar : -0.15285E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.12872E-04 0.10474E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.27511E-05 0.22416E-02 Friction velocity uk : 0.27522E-05 0.22416E-02 Dimensionless distance yplus : 0.18328E-04 0.14914E-01 Friction thermal sca. tstar : -0.15285E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.12872E-04 0.10474E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.37591E-08 3 0.17955E-06 0.18728E-12 0.86249E+00 c Velocity[X] 0.46710E-32 c Velocity[Y] 0.93639E-13 c Velocity[Z] 0.93644E-13 c Pressure 0.72709E-14 16 0.56487E-07 0.56487E-07 0.93626E+00 c k 0.29994E-06 2 0.31261E-07 0.12436E-08 0.12907E+01 c omega 0.13153E+02 1 0.93734E-09 0.14954E+00 0.20132E-02 c TempK 0.94741E+02 1 0.77952E-07 0.17514E-01 0.14641E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.0165e-14 7.5439e-14 -9.3796e-18 -2.4441e-18 v Velocity[Y] -0.00012216 0.00011541 -4.7353e-10 -2.99e-12 v Velocity[Z] -0.00011535 0.00012217 1.8925e-10 -1.8203e-12 v ǁVelocityǁ 2.9381e-10 0.00013096 1.1341e-05 8.2596e-06 v Pressure -0.0014219 0.023366 0.0013379 -5.187e-20 v k 5.9341e-10 0.0010013 0.00065161 0.00083124 v omega 12.836 1.0313e+05 2664.9 497.89 v TempK 288 342.1 294.21 291.14 v Density 1.205 1.205 1.205 1.205 v TurbVisc 6.9555e-15 9.4005e-05 5.5729e-05 7.2905e-05 v CourantNb 3.0371e-09 0.00019233 1.3824e-05 8.7219e-06 v FourierNb 0.090989 0.6281 0.18466 0.15553 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9571 4.9571 0.00055559 -5.7131e-07 v volume_forces[Z] -4.9571 4.9571 -0.00055548 6.7764e-07 v ǁvolume_forcesǁ 1.0662e-08 4.9581 0.56193 0.28158 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.41 291.28 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014914 5.2748e-05 2.9431e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.091008 0.6281 0.18468 0.15554 INSTANT 0.813735000E+00 TIME STEP NUMBER 845 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.24989E-05 0.22411E-02 Friction velocity uk : 0.25001E-05 0.22411E-02 Dimensionless distance yplus : 0.16650E-04 0.14910E-01 Friction thermal sca. tstar : -0.15549E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.11694E-04 0.10472E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.24989E-05 0.22411E-02 Friction velocity uk : 0.25001E-05 0.22411E-02 Dimensionless distance yplus : 0.16650E-04 0.14910E-01 Friction thermal sca. tstar : -0.15549E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.11694E-04 0.10472E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.37606E-08 3 0.17906E-06 0.18688E-12 0.86144E+00 c Velocity[X] 0.46537E-32 c Velocity[Y] 0.93439E-13 c Velocity[Z] 0.93444E-13 c Pressure 0.72590E-14 16 0.56393E-07 0.56393E-07 0.93509E+00 c k 0.29958E-06 2 0.31211E-07 0.12381E-08 0.12894E+01 c omega 0.13153E+02 1 0.93498E-09 0.14892E+00 0.20090E-02 c TempK 0.94741E+02 1 0.77821E-07 0.17483E-01 0.14628E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.0116e-14 7.5399e-14 -9.3748e-18 -2.443e-18 v Velocity[Y] -0.00012214 0.00011538 -4.711e-10 -2.986e-12 v Velocity[Z] -0.00011532 0.00012215 1.8672e-10 -1.8203e-12 v ǁVelocityǁ 2.9294e-10 0.00013093 1.1345e-05 8.2656e-06 v Pressure -0.0014235 0.02338 0.0013388 1.9414e-20 v k 5.9154e-10 0.0010001 0.00065076 0.00083019 v omega 12.823 1.0313e+05 2664.9 497.87 v TempK 288 342.1 294.21 291.14 v Density 1.205 1.205 1.205 1.205 v TurbVisc 6.9336e-15 9.3995e-05 5.5712e-05 7.2885e-05 v CourantNb 3.0396e-09 0.00019226 1.3824e-05 8.7254e-06 v FourierNb 0.090919 0.6281 0.18463 0.15549 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9571 4.9572 0.00055579 -5.7156e-07 v volume_forces[Z] -4.9571 4.9572 -0.00055568 6.7793e-07 v ǁvolume_forcesǁ 1.0621e-08 4.9582 0.56213 0.28175 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.42 291.28 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.01491 5.2736e-05 2.9424e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.090938 0.6281 0.18465 0.1555 INSTANT 0.814698000E+00 TIME STEP NUMBER 846 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.22176E-05 0.22406E-02 Friction velocity uk : 0.22190E-05 0.22405E-02 Dimensionless distance yplus : 0.14777E-04 0.14907E-01 Friction thermal sca. tstar : -0.15827E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.10379E-04 0.10470E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.22176E-05 0.22406E-02 Friction velocity uk : 0.22190E-05 0.22405E-02 Dimensionless distance yplus : 0.14777E-04 0.14907E-01 Friction thermal sca. tstar : -0.15827E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.10379E-04 0.10470E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.37620E-08 3 0.21011E-06 0.18648E-12 0.86039E+00 c Velocity[X] 0.46365E-32 c Velocity[Y] 0.93239E-13 c Velocity[Z] 0.93245E-13 c Pressure 0.72937E-14 16 0.56662E-07 0.56662E-07 0.93393E+00 c k 0.29921E-06 2 0.31161E-07 0.12326E-08 0.12882E+01 c omega 0.13153E+02 1 0.93263E-09 0.14830E+00 0.20049E-02 c TempK 0.94742E+02 1 0.77690E-07 0.17452E-01 0.14615E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.0066e-14 7.5359e-14 -9.3701e-18 -2.4419e-18 v Velocity[Y] -0.00012212 0.00011536 -4.6866e-10 -2.9821e-12 v Velocity[Z] -0.0001153 0.00012212 1.8419e-10 -1.8204e-12 v ǁVelocityǁ 2.9235e-10 0.00013091 1.1348e-05 8.2715e-06 v Pressure -0.0014252 0.023393 0.0013397 7.9423e-20 v k 5.8967e-10 0.00099903 0.00064991 0.00082914 v omega 12.81 1.0313e+05 2664.9 497.86 v TempK 288 342.1 294.21 291.14 v Density 1.205 1.205 1.205 1.205 v TurbVisc 6.9117e-15 9.3985e-05 5.5695e-05 7.2865e-05 v CourantNb 3.0421e-09 0.0001922 1.3824e-05 8.7289e-06 v FourierNb 0.090849 0.6281 0.1846 0.15546 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9572 4.9572 0.00055598 -5.7182e-07 v volume_forces[Z] -4.9572 4.9572 -0.00055588 6.7821e-07 v ǁvolume_forcesǁ 1.059e-08 4.9582 0.56232 0.28191 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.42 291.28 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014907 5.2724e-05 2.9416e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.090868 0.6281 0.18461 0.15547 INSTANT 0.815661000E+00 TIME STEP NUMBER 847 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.18942E-05 0.22401E-02 Friction velocity uk : 0.18958E-05 0.22400E-02 Dimensionless distance yplus : 0.12625E-04 0.14903E-01 Friction thermal sca. tstar : -0.16118E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.88671E-05 0.10467E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.18942E-05 0.22401E-02 Friction velocity uk : 0.18958E-05 0.22400E-02 Dimensionless distance yplus : 0.12625E-04 0.14903E-01 Friction thermal sca. tstar : -0.16118E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.88671E-05 0.10467E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.37635E-08 3 0.10192E-06 0.18609E-12 0.85934E+00 c Velocity[X] 0.46193E-32 c Velocity[Y] 0.93040E-13 c Velocity[Z] 0.93045E-13 c Pressure 0.72549E-14 16 0.56360E-07 0.56360E-07 0.93278E+00 c k 0.29885E-06 2 0.31111E-07 0.12272E-08 0.12869E+01 c omega 0.13153E+02 1 0.93029E-09 0.14769E+00 0.20007E-02 c TempK 0.94742E+02 1 0.77560E-07 0.17421E-01 0.14602E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.0016e-14 7.532e-14 -9.3653e-18 -2.4408e-18 v Velocity[Y] -0.00012209 0.00011533 -4.6623e-10 -2.9781e-12 v Velocity[Z] -0.00011527 0.0001221 1.8166e-10 -1.8203e-12 v ǁVelocityǁ 2.9201e-10 0.00013088 1.1352e-05 8.2774e-06 v Pressure -0.0014268 0.023407 0.0013406 1.0109e-19 v k 5.8782e-10 0.00099792 0.00064906 0.0008281 v omega 12.797 1.0313e+05 2664.9 497.85 v TempK 288 342.1 294.21 291.14 v Density 1.205 1.205 1.205 1.205 v TurbVisc 6.8899e-15 9.3974e-05 5.5677e-05 7.2845e-05 v CourantNb 3.0446e-09 0.00019213 1.3825e-05 8.7323e-06 v FourierNb 0.090779 0.6281 0.18456 0.15542 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9572 4.9572 0.00055618 -5.7208e-07 v volume_forces[Z] -4.9572 4.9572 -0.00055607 6.7849e-07 v ǁvolume_forcesǁ 1.0568e-08 4.9583 0.56251 0.28208 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.42 291.29 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014903 5.2712e-05 2.9409e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.090798 0.6281 0.18458 0.15543 INSTANT 0.816624000E+00 TIME STEP NUMBER 848 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15017E-05 0.22395E-02 Friction velocity uk : 0.15037E-05 0.22395E-02 Dimensionless distance yplus : 0.10014E-04 0.14900E-01 Friction thermal sca. tstar : -0.16425E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.70331E-05 0.10465E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15017E-05 0.22395E-02 Friction velocity uk : 0.15037E-05 0.22395E-02 Dimensionless distance yplus : 0.10014E-04 0.14900E-01 Friction thermal sca. tstar : -0.16425E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.70331E-05 0.10465E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.37650E-08 3 0.10168E-06 0.18569E-12 0.85830E+00 c Velocity[X] 0.46023E-32 c Velocity[Y] 0.92841E-13 c Velocity[Z] 0.92846E-13 c Pressure 0.72173E-14 16 0.56067E-07 0.56067E-07 0.93163E+00 c k 0.29848E-06 2 0.31062E-07 0.12218E-08 0.12856E+01 c omega 0.13153E+02 1 0.92795E-09 0.14708E+00 0.19966E-02 c TempK 0.94743E+02 1 0.77430E-07 0.17390E-01 0.14589E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.9967e-14 7.528e-14 -9.3606e-18 -2.4396e-18 v Velocity[Y] -0.00012207 0.0001153 -4.6379e-10 -2.9742e-12 v Velocity[Z] -0.00011524 0.00012208 1.7913e-10 -1.8204e-12 v ǁVelocityǁ 2.9195e-10 0.00013086 1.1356e-05 8.2833e-06 v Pressure -0.0014285 0.02342 0.0013416 1.4816e-19 v k 5.8597e-10 0.00099681 0.00064822 0.00082705 v omega 12.784 1.0313e+05 2664.9 497.84 v TempK 288 342.1 294.21 291.15 v Density 1.205 1.205 1.205 1.205 v TurbVisc 6.8682e-15 9.3964e-05 5.566e-05 7.2824e-05 v CourantNb 3.0471e-09 0.00019206 1.3825e-05 8.7358e-06 v FourierNb 0.09071 0.6281 0.18453 0.15539 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9573 4.9573 0.00055637 -5.7233e-07 v volume_forces[Z] -4.9573 4.9573 -0.00055627 6.7877e-07 v ǁvolume_forcesǁ 1.0556e-08 4.9583 0.56271 0.28224 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.42 291.29 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.0149 5.27e-05 2.9402e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.090728 0.6281 0.18454 0.1554 INSTANT 0.817587000E+00 TIME STEP NUMBER 849 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.95872E-06 0.22390E-02 Friction velocity uk : 0.96184E-06 0.22390E-02 Dimensionless distance yplus : 0.64054E-05 0.14896E-01 Friction thermal sca. tstar : -0.16748E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.44988E-05 0.10462E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.95872E-06 0.22390E-02 Friction velocity uk : 0.96184E-06 0.22390E-02 Dimensionless distance yplus : 0.64054E-05 0.14896E-01 Friction thermal sca. tstar : -0.16748E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.44988E-05 0.10462E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.37664E-08 3 0.10146E-06 0.18529E-12 0.85725E+00 c Velocity[X] 0.45854E-32 c Velocity[Y] 0.92642E-13 c Velocity[Z] 0.92647E-13 c Pressure 0.72049E-14 16 0.55970E-07 0.55970E-07 0.93048E+00 c k 0.29812E-06 2 0.31012E-07 0.12164E-08 0.12844E+01 c omega 0.13153E+02 1 0.92563E-09 0.14647E+00 0.19924E-02 c TempK 0.94744E+02 1 0.77300E-07 0.17359E-01 0.14576E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.9917e-14 7.524e-14 -9.3559e-18 -2.4385e-18 v Velocity[Y] -0.00012205 0.00011527 -4.6135e-10 -2.9703e-12 v Velocity[Z] -0.00011522 0.00012205 1.766e-10 -1.8204e-12 v ǁVelocityǁ 2.9216e-10 0.00013083 1.136e-05 8.2892e-06 v Pressure -0.0014302 0.023434 0.0013425 1.1962e-20 v k 5.8413e-10 0.0009957 0.00064737 0.00082601 v omega 12.772 1.0313e+05 2664.8 497.83 v TempK 288 342.1 294.22 291.15 v Density 1.205 1.205 1.205 1.205 v TurbVisc 6.8467e-15 9.3954e-05 5.5643e-05 7.2804e-05 v CourantNb 3.0496e-09 0.00019199 1.3826e-05 8.7393e-06 v FourierNb 0.090641 0.6281 0.1845 0.15535 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9573 4.9573 0.00055657 -5.7259e-07 v volume_forces[Z] -4.9573 4.9573 -0.00055647 6.7905e-07 v ǁvolume_forcesǁ 1.0554e-08 4.9584 0.5629 0.28241 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.43 291.29 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014896 5.2688e-05 2.9394e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.090659 0.6281 0.18451 0.15536 INSTANT 0.818550000E+00 TIME STEP NUMBER 850 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.64335E-06 0.22385E-02 Friction velocity uk : 0.64798E-06 0.22385E-02 Dimensionless distance yplus : 0.43153E-05 0.14893E-01 Friction thermal sca. tstar : -0.17088E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.30308E-05 0.10460E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.64335E-06 0.22385E-02 Friction velocity uk : 0.64798E-06 0.22385E-02 Dimensionless distance yplus : 0.43153E-05 0.14893E-01 Friction thermal sca. tstar : -0.17088E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.30308E-05 0.10460E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.37679E-08 3 0.10125E-06 0.18489E-12 0.85620E+00 c Velocity[X] 0.45685E-32 c Velocity[Y] 0.92443E-13 c Velocity[Z] 0.92448E-13 c Pressure 0.72010E-14 16 0.55939E-07 0.55939E-07 0.92933E+00 c k 0.29776E-06 2 0.30963E-07 0.12110E-08 0.12831E+01 c omega 0.13153E+02 1 0.92331E-09 0.14586E+00 0.19883E-02 c TempK 0.94744E+02 1 0.77171E-07 0.17329E-01 0.14563E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.9868e-14 7.5201e-14 -9.3512e-18 -2.4374e-18 v Velocity[Y] -0.00012203 0.00011525 -4.5891e-10 -2.9664e-12 v Velocity[Z] -0.00011519 0.00012203 1.7407e-10 -1.8204e-12 v ǁVelocityǁ 2.9264e-10 0.00013081 1.1363e-05 8.2951e-06 v Pressure -0.0014318 0.023447 0.0013434 3.7946e-20 v k 5.823e-10 0.00099459 0.00064653 0.00082497 v omega 12.759 1.0313e+05 2664.8 497.82 v TempK 288 342.1 294.22 291.15 v Density 1.205 1.205 1.205 1.205 v TurbVisc 6.8252e-15 9.3944e-05 5.5626e-05 7.2784e-05 v CourantNb 3.052e-09 0.00019193 1.3826e-05 8.7427e-06 v FourierNb 0.090571 0.6281 0.18446 0.15532 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9574 4.9574 0.00055677 -5.7284e-07 v volume_forces[Z] -4.9574 4.9574 -0.00055666 6.7932e-07 v ǁvolume_forcesǁ 1.0562e-08 4.9584 0.5631 0.28257 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.43 291.29 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014893 5.2675e-05 2.9387e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.09059 0.6281 0.18448 0.15533 INSTANT 0.819513000E+00 TIME STEP NUMBER 851 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.13251E-05 0.22380E-02 Friction velocity uk : 0.13274E-05 0.22379E-02 Dimensionless distance yplus : 0.88397E-05 0.14889E-01 Friction thermal sca. tstar : -0.17449E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.62084E-05 0.10457E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.13251E-05 0.22380E-02 Friction velocity uk : 0.13274E-05 0.22379E-02 Dimensionless distance yplus : 0.88397E-05 0.14889E-01 Friction thermal sca. tstar : -0.17449E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.62084E-05 0.10457E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.37694E-08 3 0.10102E-06 0.18449E-12 0.85515E+00 c Velocity[X] 0.45516E-32 c Velocity[Y] 0.92244E-13 c Velocity[Z] 0.92250E-13 c Pressure 0.71828E-14 16 0.55797E-07 0.55797E-07 0.92818E+00 c k 0.29740E-06 2 0.30914E-07 0.12057E-08 0.12818E+01 c omega 0.13153E+02 1 0.92100E-09 0.14526E+00 0.19842E-02 c TempK 0.94745E+02 1 0.77042E-07 0.17298E-01 0.14550E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.9818e-14 7.5162e-14 -9.3465e-18 -2.4363e-18 v Velocity[Y] -0.000122 0.00011522 -4.5647e-10 -2.9626e-12 v Velocity[Z] -0.00011516 0.00012201 1.7154e-10 -1.8204e-12 v ǁVelocityǁ 2.9339e-10 0.00013078 1.1367e-05 8.301e-06 v Pressure -0.0014335 0.02346 0.0013443 6.0793e-21 v k 5.8047e-10 0.00099349 0.00064569 0.00082394 v omega 12.746 1.0313e+05 2664.8 497.81 v TempK 288 342.1 294.22 291.15 v Density 1.205 1.205 1.205 1.205 v TurbVisc 6.8037e-15 9.3934e-05 5.5609e-05 7.2764e-05 v CourantNb 3.0545e-09 0.00019186 1.3827e-05 8.7462e-06 v FourierNb 0.090502 0.6281 0.18443 0.15529 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9574 4.9574 0.00055696 -5.731e-07 v volume_forces[Z] -4.9574 4.9574 -0.00055686 6.796e-07 v ǁvolume_forcesǁ 1.0579e-08 4.9585 0.56329 0.28274 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.43 291.29 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014889 5.2663e-05 2.938e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.090521 0.6281 0.18444 0.15529 INSTANT 0.820476000E+00 TIME STEP NUMBER 852 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.17610E-05 0.22375E-02 Friction velocity uk : 0.17627E-05 0.22374E-02 Dimensionless distance yplus : 0.11738E-04 0.14886E-01 Friction thermal sca. tstar : -0.17831E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.82443E-05 0.10455E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.17610E-05 0.22375E-02 Friction velocity uk : 0.17627E-05 0.22374E-02 Dimensionless distance yplus : 0.11738E-04 0.14886E-01 Friction thermal sca. tstar : -0.17831E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.82443E-05 0.10455E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.37709E-08 3 0.10080E-06 0.18410E-12 0.85411E+00 c Velocity[X] 0.45352E-32 c Velocity[Y] 0.92046E-13 c Velocity[Z] 0.92051E-13 c Pressure 0.71662E-14 16 0.55667E-07 0.55667E-07 0.92704E+00 c k 0.29704E-06 2 0.30865E-07 0.12004E-08 0.12806E+01 c omega 0.13153E+02 1 0.91870E-09 0.14466E+00 0.19801E-02 c TempK 0.94745E+02 1 0.76914E-07 0.17268E-01 0.14537E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.9769e-14 7.5122e-14 -9.3418e-18 -2.4352e-18 v Velocity[Y] -0.00012198 0.00011519 -4.5403e-10 -2.9587e-12 v Velocity[Z] -0.00011513 0.00012198 1.6901e-10 -1.8204e-12 v ǁVelocityǁ 2.9442e-10 0.00013076 1.1371e-05 8.3068e-06 v Pressure -0.0014351 0.023474 0.0013453 1.2335e-19 v k 5.7866e-10 0.00099239 0.00064485 0.0008229 v omega 12.733 1.0313e+05 2664.8 497.8 v TempK 288 342.11 294.22 291.15 v Density 1.205 1.205 1.205 1.205 v TurbVisc 6.7824e-15 9.3924e-05 5.5592e-05 7.2744e-05 v CourantNb 3.057e-09 0.00019179 1.3827e-05 8.7497e-06 v FourierNb 0.090434 0.6281 0.1844 0.15525 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9574 4.9575 0.00055716 -5.7335e-07 v volume_forces[Z] -4.9574 4.9575 -0.00055705 6.7988e-07 v ǁvolume_forcesǁ 1.0606e-08 4.9585 0.56348 0.2829 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.43 291.29 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014886 5.2651e-05 2.9373e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.090452 0.6281 0.18441 0.15526 INSTANT 0.821439000E+00 TIME STEP NUMBER 853 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.21093E-05 0.22369E-02 Friction velocity uk : 0.21107E-05 0.22369E-02 Dimensionless distance yplus : 0.14056E-04 0.14882E-01 Friction thermal sca. tstar : -0.18237E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.98723E-05 0.10452E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.21093E-05 0.22369E-02 Friction velocity uk : 0.21107E-05 0.22369E-02 Dimensionless distance yplus : 0.14056E-04 0.14882E-01 Friction thermal sca. tstar : -0.18237E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.98723E-05 0.10452E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.37723E-08 3 0.10059E-06 0.18370E-12 0.85306E+00 c Velocity[X] 0.45186E-32 c Velocity[Y] 0.91848E-13 c Velocity[Z] 0.91853E-13 c Pressure 0.71745E-14 16 0.55732E-07 0.55732E-07 0.92590E+00 c k 0.29668E-06 2 0.30816E-07 0.11952E-08 0.12793E+01 c omega 0.13153E+02 1 0.91640E-09 0.14407E+00 0.19760E-02 c TempK 0.94746E+02 1 0.76786E-07 0.17237E-01 0.14524E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.972e-14 7.5083e-14 -9.3371e-18 -2.4341e-18 v Velocity[Y] -0.00012196 0.00011517 -4.5159e-10 -2.9549e-12 v Velocity[Z] -0.00011511 0.00012196 1.6648e-10 -1.8204e-12 v ǁVelocityǁ 2.9571e-10 0.00013073 1.1375e-05 8.3127e-06 v Pressure -0.0014368 0.023487 0.0013462 -4.0986e-20 v k 5.7685e-10 0.00099129 0.00064402 0.00082187 v omega 12.72 1.0313e+05 2664.8 497.78 v TempK 288 342.11 294.23 291.16 v Density 1.205 1.205 1.205 1.205 v TurbVisc 6.7612e-15 9.3914e-05 5.5575e-05 7.2724e-05 v CourantNb 3.0594e-09 0.00019173 1.3828e-05 8.7531e-06 v FourierNb 0.090365 0.6281 0.18436 0.15522 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9575 4.9575 0.00055735 -5.736e-07 v volume_forces[Z] -4.9575 4.9575 -0.00055725 6.8016e-07 v ǁvolume_forcesǁ 1.0643e-08 4.9585 0.56368 0.28307 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.43 291.3 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014882 5.2639e-05 2.9365e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.090384 0.6281 0.18438 0.15523 INSTANT 0.822402000E+00 TIME STEP NUMBER 854 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.24084E-05 0.22364E-02 Friction velocity uk : 0.24096E-05 0.22364E-02 Dimensionless distance yplus : 0.16047E-04 0.14879E-01 Friction thermal sca. tstar : -0.18670E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.11270E-04 0.10450E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.24084E-05 0.22364E-02 Friction velocity uk : 0.24096E-05 0.22364E-02 Dimensionless distance yplus : 0.16047E-04 0.14879E-01 Friction thermal sca. tstar : -0.18670E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.11270E-04 0.10450E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.37738E-08 3 0.10036E-06 0.18331E-12 0.85201E+00 c Velocity[X] 0.45019E-32 c Velocity[Y] 0.91650E-13 c Velocity[Z] 0.91655E-13 c Pressure 0.71417E-14 16 0.55476E-07 0.55476E-07 0.92476E+00 c k 0.29632E-06 2 0.30767E-07 0.11899E-08 0.12781E+01 c omega 0.13153E+02 1 0.91411E-09 0.14347E+00 0.19719E-02 c TempK 0.94746E+02 1 0.76658E-07 0.17207E-01 0.14511E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.9671e-14 7.5044e-14 -9.3324e-18 -2.433e-18 v Velocity[Y] -0.00012193 0.00011514 -4.4914e-10 -2.9511e-12 v Velocity[Z] -0.00011508 0.00012194 1.6395e-10 -1.8204e-12 v ǁVelocityǁ 2.9728e-10 0.00013071 1.1378e-05 8.3186e-06 v Pressure -0.0014384 0.0235 0.0013471 1.1786e-19 v k 5.7505e-10 0.00099019 0.00064318 0.00082084 v omega 12.708 1.0313e+05 2664.8 497.77 v TempK 288 342.11 294.23 291.16 v Density 1.205 1.205 1.205 1.205 v TurbVisc 6.7401e-15 9.3904e-05 5.5559e-05 7.2704e-05 v CourantNb 3.0619e-09 0.00019166 1.3828e-05 8.7566e-06 v FourierNb 0.090297 0.6281 0.18433 0.15518 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9575 4.9576 0.00055755 -5.7386e-07 v volume_forces[Z] -4.9575 4.9576 -0.00055744 6.8043e-07 v ǁvolume_forcesǁ 1.069e-08 4.9586 0.56387 0.28323 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.44 291.3 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014879 5.2627e-05 2.9358e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.090315 0.6281 0.18434 0.15519 INSTANT 0.823365000E+00 TIME STEP NUMBER 855 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.26749E-05 0.22359E-02 Friction velocity uk : 0.26759E-05 0.22359E-02 Dimensionless distance yplus : 0.17820E-04 0.14876E-01 Friction thermal sca. tstar : -0.19132E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.12516E-04 0.10448E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.26749E-05 0.22359E-02 Friction velocity uk : 0.26759E-05 0.22359E-02 Dimensionless distance yplus : 0.17820E-04 0.14876E-01 Friction thermal sca. tstar : -0.19132E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.12516E-04 0.10448E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.37753E-08 3 0.10015E-06 0.18291E-12 0.85096E+00 c Velocity[X] 0.44857E-32 c Velocity[Y] 0.91452E-13 c Velocity[Z] 0.91458E-13 c Pressure 0.71853E-14 16 0.55814E-07 0.55814E-07 0.92363E+00 c k 0.29596E-06 2 0.30719E-07 0.11847E-08 0.12768E+01 c omega 0.13153E+02 1 0.91184E-09 0.14288E+00 0.19679E-02 c TempK 0.94747E+02 1 0.76530E-07 0.17177E-01 0.14498E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.9622e-14 7.5005e-14 -9.3277e-18 -2.4319e-18 v Velocity[Y] -0.00012191 0.00011512 -4.4669e-10 -2.9473e-12 v Velocity[Z] -0.00011505 0.00012191 1.6141e-10 -1.8204e-12 v ǁVelocityǁ 2.9911e-10 0.00013068 1.1382e-05 8.3245e-06 v Pressure -0.0014401 0.023514 0.001348 -2.2062e-19 v k 5.7325e-10 0.0009891 0.00064235 0.00081981 v omega 12.695 1.0313e+05 2664.8 497.76 v TempK 288 342.11 294.23 291.16 v Density 1.205 1.205 1.205 1.205 v TurbVisc 6.719e-15 9.3894e-05 5.5542e-05 7.2684e-05 v CourantNb 3.0644e-09 0.0001916 1.3829e-05 8.76e-06 v FourierNb 0.090228 0.6281 0.1843 0.15515 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9576 4.9576 0.00055774 -5.7411e-07 v volume_forces[Z] -4.9576 4.9576 -0.00055764 6.8071e-07 v ǁvolume_forcesǁ 1.0747e-08 4.9586 0.56406 0.2834 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.44 291.3 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014876 5.2615e-05 2.9351e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.090247 0.6281 0.18431 0.15516 INSTANT 0.824328000E+00 TIME STEP NUMBER 856 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.29176E-05 0.22354E-02 Friction velocity uk : 0.29185E-05 0.22354E-02 Dimensionless distance yplus : 0.19436E-04 0.14872E-01 Friction thermal sca. tstar : -0.19628E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.13651E-04 0.10445E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.29176E-05 0.22354E-02 Friction velocity uk : 0.29185E-05 0.22354E-02 Dimensionless distance yplus : 0.19436E-04 0.14872E-01 Friction thermal sca. tstar : -0.19628E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.13651E-04 0.10445E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.37767E-08 3 0.99911E-07 0.18251E-12 0.84991E+00 c Velocity[X] 0.44693E-32 c Velocity[Y] 0.91254E-13 c Velocity[Z] 0.91260E-13 c Pressure 0.71238E-14 16 0.55336E-07 0.55336E-07 0.92250E+00 c k 0.29561E-06 2 0.30670E-07 0.11795E-08 0.12756E+01 c omega 0.13153E+02 1 0.90956E-09 0.14230E+00 0.19638E-02 c TempK 0.94747E+02 1 0.76403E-07 0.17147E-01 0.14486E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.9573e-14 7.4966e-14 -9.3231e-18 -2.4308e-18 v Velocity[Y] -0.00012189 0.00011509 -4.4424e-10 -2.9435e-12 v Velocity[Z] -0.00011503 0.00012189 1.5888e-10 -1.8204e-12 v ǁVelocityǁ 3.0121e-10 0.00013066 1.1386e-05 8.3303e-06 v Pressure -0.0014417 0.023527 0.0013489 -2.265e-20 v k 5.7147e-10 0.00098801 0.00064152 0.00081879 v omega 12.682 1.0313e+05 2664.8 497.75 v TempK 288 342.11 294.23 291.16 v Density 1.205 1.205 1.205 1.205 v TurbVisc 6.6981e-15 9.3884e-05 5.5525e-05 7.2664e-05 v CourantNb 3.0668e-09 0.00019153 1.3829e-05 8.7635e-06 v FourierNb 0.09016 0.6281 0.18426 0.15511 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9576 4.9576 0.00055794 -5.7436e-07 v volume_forces[Z] -4.9576 4.9576 -0.00055783 6.8099e-07 v ǁvolume_forcesǁ 1.0813e-08 4.9587 0.56426 0.28356 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.44 291.3 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014872 5.2603e-05 2.9344e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.090179 0.6281 0.18428 0.15512 INSTANT 0.825291000E+00 TIME STEP NUMBER 857 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.31421E-05 0.22349E-02 Friction velocity uk : 0.31430E-05 0.22348E-02 Dimensionless distance yplus : 0.20931E-04 0.14869E-01 Friction thermal sca. tstar : -0.20161E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.14700E-04 0.10443E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.31421E-05 0.22349E-02 Friction velocity uk : 0.31430E-05 0.22348E-02 Dimensionless distance yplus : 0.20931E-04 0.14869E-01 Friction thermal sca. tstar : -0.20161E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.14700E-04 0.10443E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.37782E-08 3 0.99696E-07 0.18212E-12 0.84887E+00 c Velocity[X] 0.44530E-32 c Velocity[Y] 0.91057E-13 c Velocity[Z] 0.91063E-13 c Pressure 0.71148E-14 16 0.55265E-07 0.55265E-07 0.92137E+00 c k 0.29525E-06 2 0.30622E-07 0.11744E-08 0.12743E+01 c omega 0.13153E+02 1 0.90730E-09 0.14171E+00 0.19598E-02 c TempK 0.94748E+02 1 0.76277E-07 0.17117E-01 0.14473E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.9524e-14 7.4927e-14 -9.3184e-18 -2.4297e-18 v Velocity[Y] -0.00012186 0.00011506 -4.4179e-10 -2.9397e-12 v Velocity[Z] -0.000115 0.00012187 1.5635e-10 -1.8203e-12 v ǁVelocityǁ 3.0357e-10 0.00013063 1.1389e-05 8.3362e-06 v Pressure -0.0014434 0.023541 0.0013499 -8.1384e-20 v k 5.6969e-10 0.00098692 0.00064069 0.00081776 v omega 12.67 1.0313e+05 2664.8 497.74 v TempK 288 342.11 294.23 291.16 v Density 1.205 1.205 1.205 1.205 v TurbVisc 6.6772e-15 9.3874e-05 5.5508e-05 7.2644e-05 v CourantNb 3.0692e-09 0.00019146 1.383e-05 8.7669e-06 v FourierNb 0.090093 0.6281 0.18423 0.15508 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9577 4.9577 0.00055813 -5.7461e-07 v volume_forces[Z] -4.9577 4.9577 -0.00055803 6.8126e-07 v ǁvolume_forcesǁ 1.0889e-08 4.9587 0.56445 0.28373 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.44 291.3 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014869 5.2591e-05 2.9336e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.090111 0.6281 0.18425 0.15509 INSTANT 0.826254000E+00 TIME STEP NUMBER 858 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.33520E-05 0.22344E-02 Friction velocity uk : 0.33528E-05 0.22343E-02 Dimensionless distance yplus : 0.22328E-04 0.14865E-01 Friction thermal sca. tstar : -0.20737E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.15682E-04 0.10440E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.33520E-05 0.22344E-02 Friction velocity uk : 0.33528E-05 0.22343E-02 Dimensionless distance yplus : 0.22328E-04 0.14865E-01 Friction thermal sca. tstar : -0.20737E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.15682E-04 0.10440E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.37797E-08 3 0.99474E-07 0.18173E-12 0.84782E+00 c Velocity[X] 0.44368E-32 c Velocity[Y] 0.90860E-13 c Velocity[Z] 0.90865E-13 c Pressure 0.70919E-14 16 0.55086E-07 0.55086E-07 0.92024E+00 c k 0.29489E-06 2 0.30574E-07 0.11693E-08 0.12731E+01 c omega 0.13153E+02 1 0.90504E-09 0.14113E+00 0.19558E-02 c TempK 0.94748E+02 1 0.76150E-07 0.17087E-01 0.14460E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.9475e-14 7.4888e-14 -9.3138e-18 -2.4286e-18 v Velocity[Y] -0.00012184 0.00011504 -4.3934e-10 -2.9359e-12 v Velocity[Z] -0.00011498 0.00012185 1.5381e-10 -1.8203e-12 v ǁVelocityǁ 3.0618e-10 0.00013061 1.1393e-05 8.342e-06 v Pressure -0.0014451 0.023554 0.0013508 1.3178e-19 v k 5.6792e-10 0.00098583 0.00063987 0.00081674 v omega 12.657 1.0313e+05 2664.8 497.73 v TempK 288 342.11 294.24 291.17 v Density 1.205 1.205 1.205 1.205 v TurbVisc 6.6564e-15 9.3864e-05 5.5491e-05 7.2624e-05 v CourantNb 3.0717e-09 0.0001914 1.383e-05 8.7704e-06 v FourierNb 0.090025 0.6281 0.1842 0.15505 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9577 4.9577 0.00055832 -5.7486e-07 v volume_forces[Z] -4.9577 4.9577 -0.00055822 6.8154e-07 v ǁvolume_forcesǁ 1.0974e-08 4.9588 0.56464 0.28389 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.44 291.31 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014865 5.2579e-05 2.9329e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.090043 0.6281 0.18421 0.15505 INSTANT 0.827217000E+00 TIME STEP NUMBER 859 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.35500E-05 0.22338E-02 Friction velocity uk : 0.35508E-05 0.22338E-02 Dimensionless distance yplus : 0.23647E-04 0.14862E-01 Friction thermal sca. tstar : -0.21362E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.16608E-04 0.10438E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.35500E-05 0.22338E-02 Friction velocity uk : 0.35508E-05 0.22338E-02 Dimensionless distance yplus : 0.23647E-04 0.14862E-01 Friction thermal sca. tstar : -0.21362E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.16608E-04 0.10438E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.37812E-08 3 0.99253E-07 0.18133E-12 0.84677E+00 c Velocity[X] 0.44207E-32 c Velocity[Y] 0.90662E-13 c Velocity[Z] 0.90668E-13 c Pressure 0.70791E-14 16 0.54986E-07 0.54986E-07 0.91912E+00 c k 0.29454E-06 2 0.30526E-07 0.11642E-08 0.12718E+01 c omega 0.13153E+02 1 0.90279E-09 0.14055E+00 0.19518E-02 c TempK 0.94749E+02 1 0.76024E-07 0.17057E-01 0.14447E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.9426e-14 7.4849e-14 -9.3091e-18 -2.4275e-18 v Velocity[Y] -0.00012182 0.00011501 -4.3689e-10 -2.9321e-12 v Velocity[Z] -0.00011495 0.00012182 1.5128e-10 -1.8203e-12 v ǁVelocityǁ 3.0905e-10 0.00013058 1.1397e-05 8.3479e-06 v Pressure -0.0014467 0.023567 0.0013517 -2.8435e-20 v k 5.6615e-10 0.00098474 0.00063904 0.00081573 v omega 12.645 1.0313e+05 2664.8 497.72 v TempK 288 342.11 294.24 291.17 v Density 1.205 1.205 1.205 1.205 v TurbVisc 6.6357e-15 9.3854e-05 5.5474e-05 7.2604e-05 v CourantNb 3.0741e-09 0.00019133 1.3831e-05 8.7738e-06 v FourierNb 0.089957 0.6281 0.18417 0.15501 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9578 4.9578 0.00055852 -5.7512e-07 v volume_forces[Z] -4.9578 4.9578 -0.00055842 6.8181e-07 v ǁvolume_forcesǁ 1.1068e-08 4.9588 0.56483 0.28405 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.45 291.31 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014862 5.2567e-05 2.9322e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.089976 0.6281 0.18418 0.15502 INSTANT 0.828180000E+00 TIME STEP NUMBER 860 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.37379E-05 0.22333E-02 Friction velocity uk : 0.37387E-05 0.22333E-02 Dimensionless distance yplus : 0.24898E-04 0.14858E-01 Friction thermal sca. tstar : -0.22042E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.17487E-04 0.10436E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.37379E-05 0.22333E-02 Friction velocity uk : 0.37387E-05 0.22333E-02 Dimensionless distance yplus : 0.24898E-04 0.14858E-01 Friction thermal sca. tstar : -0.22042E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.17487E-04 0.10436E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.37826E-08 3 0.99036E-07 0.18094E-12 0.84572E+00 c Velocity[X] 0.44046E-32 c Velocity[Y] 0.90466E-13 c Velocity[Z] 0.90471E-13 c Pressure 0.70669E-14 16 0.54891E-07 0.54891E-07 0.91800E+00 c k 0.29418E-06 2 0.30478E-07 0.11591E-08 0.12706E+01 c omega 0.13153E+02 1 0.90055E-09 0.13998E+00 0.19478E-02 c TempK 0.94750E+02 1 0.75898E-07 0.17027E-01 0.14435E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.9378e-14 7.481e-14 -9.3045e-18 -2.4264e-18 v Velocity[Y] -0.0001218 0.00011498 -4.3444e-10 -2.9284e-12 v Velocity[Z] -0.00011492 0.0001218 1.4874e-10 -1.8202e-12 v ǁVelocityǁ 3.1216e-10 0.00013056 1.14e-05 8.3537e-06 v Pressure -0.0014484 0.023581 0.0013526 3.373e-20 v k 5.644e-10 0.00098366 0.00063822 0.00081471 v omega 12.632 1.0313e+05 2664.7 497.71 v TempK 288 342.11 294.24 291.17 v Density 1.205 1.205 1.205 1.205 v TurbVisc 6.6151e-15 9.3844e-05 5.5457e-05 7.2584e-05 v CourantNb 3.0765e-09 0.00019127 1.3831e-05 8.7773e-06 v FourierNb 0.08989 0.6281 0.18413 0.15498 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9578 4.9578 0.00055871 -5.7537e-07 v volume_forces[Z] -4.9578 4.9578 -0.00055861 6.8208e-07 v ǁvolume_forcesǁ 1.1172e-08 4.9588 0.56503 0.28422 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.45 291.31 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014858 5.2555e-05 2.9315e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.089909 0.6281 0.18415 0.15499 INSTANT 0.829143000E+00 TIME STEP NUMBER 861 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.39172E-05 0.22328E-02 Friction velocity uk : 0.39179E-05 0.22328E-02 Dimensionless distance yplus : 0.26092E-04 0.14855E-01 Friction thermal sca. tstar : -0.22787E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.18325E-04 0.10433E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.39172E-05 0.22328E-02 Friction velocity uk : 0.39179E-05 0.22328E-02 Dimensionless distance yplus : 0.26092E-04 0.14855E-01 Friction thermal sca. tstar : -0.22787E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.18325E-04 0.10433E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.37841E-08 3 0.98827E-07 0.18054E-12 0.84468E+00 c Velocity[X] 0.43887E-32 c Velocity[Y] 0.90269E-13 c Velocity[Z] 0.90275E-13 c Pressure 0.70616E-14 16 0.54849E-07 0.54849E-07 0.91688E+00 c k 0.29383E-06 2 0.30430E-07 0.11540E-08 0.12694E+01 c omega 0.13153E+02 1 0.89832E-09 0.13941E+00 0.19438E-02 c TempK 0.94750E+02 1 0.75773E-07 0.16998E-01 0.14422E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.9329e-14 7.4772e-14 -9.2999e-18 -2.4253e-18 v Velocity[Y] -0.00012177 0.00011496 -4.3198e-10 -2.9246e-12 v Velocity[Z] -0.0001149 0.00012178 1.4621e-10 -1.8201e-12 v ǁVelocityǁ 3.1551e-10 0.00013053 1.1404e-05 8.3596e-06 v Pressure -0.00145 0.023594 0.0013535 1.9022e-20 v k 5.6265e-10 0.00098258 0.0006374 0.00081369 v omega 12.619 1.0313e+05 2664.7 497.7 v TempK 288 342.11 294.24 291.17 v Density 1.205 1.205 1.205 1.205 v TurbVisc 6.5946e-15 9.3834e-05 5.5441e-05 7.2564e-05 v CourantNb 3.0789e-09 0.0001912 1.3832e-05 8.7807e-06 v FourierNb 0.089823 0.6281 0.1841 0.15494 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9578 4.9579 0.00055891 -5.7562e-07 v volume_forces[Z] -4.9578 4.9579 -0.0005588 6.8236e-07 v ǁvolume_forcesǁ 1.1285e-08 4.9589 0.56522 0.28438 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.45 291.31 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014855 5.2543e-05 2.9308e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.089842 0.6281 0.18411 0.15495 INSTANT 0.830106000E+00 TIME STEP NUMBER 862 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.40891E-05 0.22323E-02 Friction velocity uk : 0.40897E-05 0.22323E-02 Dimensionless distance yplus : 0.27236E-04 0.14852E-01 Friction thermal sca. tstar : -0.23609E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.19129E-04 0.10431E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.40891E-05 0.22323E-02 Friction velocity uk : 0.40897E-05 0.22323E-02 Dimensionless distance yplus : 0.27236E-04 0.14852E-01 Friction thermal sca. tstar : -0.23609E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.19129E-04 0.10431E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.37856E-08 3 0.98604E-07 0.18015E-12 0.84363E+00 c Velocity[X] 0.43728E-32 c Velocity[Y] 0.90072E-13 c Velocity[Z] 0.90078E-13 c Pressure 0.70429E-14 16 0.54703E-07 0.54703E-07 0.91577E+00 c k 0.29348E-06 2 0.30382E-07 0.11490E-08 0.12681E+01 c omega 0.13153E+02 1 0.89609E-09 0.13884E+00 0.19398E-02 c TempK 0.94751E+02 1 0.75648E-07 0.16968E-01 0.14409E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.9281e-14 7.4733e-14 -9.2953e-18 -2.4243e-18 v Velocity[Y] -0.00012175 0.00011493 -4.2952e-10 -2.9209e-12 v Velocity[Z] -0.00011487 0.00012176 1.4367e-10 -1.8201e-12 v ǁVelocityǁ 3.191e-10 0.00013051 1.1408e-05 8.3654e-06 v Pressure -0.0014517 0.023607 0.0013544 -2.569e-20 v k 5.6091e-10 0.0009815 0.00063658 0.00081268 v omega 12.607 1.0313e+05 2664.7 497.68 v TempK 288 342.11 294.25 291.17 v Density 1.205 1.205 1.205 1.205 v TurbVisc 6.5742e-15 9.3824e-05 5.5424e-05 7.2544e-05 v CourantNb 3.0814e-09 0.00019114 1.3832e-05 8.7842e-06 v FourierNb 0.089756 0.6281 0.18407 0.15491 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9579 4.9579 0.0005591 -5.7587e-07 v volume_forces[Z] -4.9579 4.9579 -0.000559 6.8263e-07 v ǁvolume_forcesǁ 1.1406e-08 4.9589 0.56541 0.28455 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.45 291.31 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014852 5.2531e-05 2.93e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.089775 0.6281 0.18408 0.15492 INSTANT 0.831069000E+00 TIME STEP NUMBER 863 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.42543E-05 0.22318E-02 Friction velocity uk : 0.42549E-05 0.22318E-02 Dimensionless distance yplus : 0.28336E-04 0.14848E-01 Friction thermal sca. tstar : -0.24520E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.19901E-04 0.10428E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.42543E-05 0.22318E-02 Friction velocity uk : 0.42549E-05 0.22318E-02 Dimensionless distance yplus : 0.28336E-04 0.14848E-01 Friction thermal sca. tstar : -0.24520E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.19901E-04 0.10428E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.37870E-08 3 0.14398E-06 0.17976E-12 0.84258E+00 c Velocity[X] 0.43570E-32 c Velocity[Y] 0.89876E-13 c Velocity[Z] 0.89882E-13 c Pressure 0.70322E-14 16 0.54619E-07 0.54619E-07 0.91465E+00 c k 0.29313E-06 2 0.30334E-07 0.11440E-08 0.12669E+01 c omega 0.13153E+02 1 0.89387E-09 0.13827E+00 0.19358E-02 c TempK 0.94751E+02 1 0.75524E-07 0.16938E-01 0.14397E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.9233e-14 7.4694e-14 -9.2907e-18 -2.4232e-18 v Velocity[Y] -0.00012173 0.00011491 -4.2707e-10 -2.9172e-12 v Velocity[Z] -0.00011484 0.00012173 1.4114e-10 -1.82e-12 v ǁVelocityǁ 3.2292e-10 0.00013048 1.1412e-05 8.3713e-06 v Pressure -0.0014533 0.02362 0.0013554 -9.3248e-20 v k 5.5917e-10 0.00098042 0.00063576 0.00081167 v omega 12.594 1.0313e+05 2664.7 497.67 v TempK 288 342.11 294.25 291.17 v Density 1.205 1.205 1.205 1.205 v TurbVisc 6.5538e-15 9.3815e-05 5.5407e-05 7.2524e-05 v CourantNb 3.0838e-09 0.00019107 1.3833e-05 8.7876e-06 v FourierNb 0.089689 0.6281 0.18403 0.15487 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9579 4.9579 0.00055929 -5.7612e-07 v volume_forces[Z] -4.9579 4.9579 -0.00055919 6.829e-07 v ǁvolume_forcesǁ 1.1536e-08 4.959 0.5656 0.28471 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.46 291.32 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014848 5.2519e-05 2.9293e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.089708 0.6281 0.18405 0.15488 INSTANT 0.832032000E+00 TIME STEP NUMBER 864 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.44137E-05 0.22313E-02 Friction velocity uk : 0.44143E-05 0.22312E-02 Dimensionless distance yplus : 0.29397E-04 0.14845E-01 Friction thermal sca. tstar : -0.25539E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.20647E-04 0.10426E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.44137E-05 0.22313E-02 Friction velocity uk : 0.44143E-05 0.22312E-02 Dimensionless distance yplus : 0.29397E-04 0.14845E-01 Friction thermal sca. tstar : -0.25539E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.20647E-04 0.10426E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.37885E-08 3 0.98182E-07 0.17937E-12 0.84153E+00 c Velocity[X] 0.43413E-32 c Velocity[Y] 0.89680E-13 c Velocity[Z] 0.89686E-13 c Pressure 0.70239E-14 16 0.54555E-07 0.54555E-07 0.91354E+00 c k 0.29277E-06 2 0.30287E-07 0.11391E-08 0.12657E+01 c omega 0.13153E+02 1 0.89166E-09 0.13770E+00 0.19319E-02 c TempK 0.94752E+02 1 0.75399E-07 0.16909E-01 0.14384E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.9184e-14 7.4656e-14 -9.2861e-18 -2.4221e-18 v Velocity[Y] -0.00012171 0.00011488 -4.2461e-10 -2.9135e-12 v Velocity[Z] -0.00011482 0.00012171 1.386e-10 -1.8199e-12 v ǁVelocityǁ 3.2696e-10 0.00013046 1.1415e-05 8.3771e-06 v Pressure -0.001455 0.023634 0.0013563 8.2364e-21 v k 5.5745e-10 0.00097935 0.00063494 0.00081067 v omega 12.582 1.0313e+05 2664.7 497.66 v TempK 288 342.11 294.25 291.18 v Density 1.205 1.205 1.205 1.205 v TurbVisc 6.5335e-15 9.3805e-05 5.539e-05 7.2504e-05 v CourantNb 3.0862e-09 0.00019101 1.3834e-05 8.7911e-06 v FourierNb 0.089623 0.6281 0.184 0.15484 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.958 4.958 0.00055949 -5.7637e-07 v volume_forces[Z] -4.958 4.958 -0.00055938 6.8318e-07 v ǁvolume_forcesǁ 1.1674e-08 4.959 0.56579 0.28487 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.46 291.32 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014845 5.2507e-05 2.9286e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.089641 0.6281 0.18402 0.15485 INSTANT 0.832995000E+00 TIME STEP NUMBER 865 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.45679E-05 0.22308E-02 Friction velocity uk : 0.45684E-05 0.22307E-02 Dimensionless distance yplus : 0.30424E-04 0.14841E-01 Friction thermal sca. tstar : -0.26690E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.21368E-04 0.10424E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.45679E-05 0.22308E-02 Friction velocity uk : 0.45684E-05 0.22307E-02 Dimensionless distance yplus : 0.30424E-04 0.14841E-01 Friction thermal sca. tstar : -0.26690E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.21368E-04 0.10424E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.37900E-08 3 0.97968E-07 0.17897E-12 0.84048E+00 c Velocity[X] 0.43257E-32 c Velocity[Y] 0.89484E-13 c Velocity[Z] 0.89490E-13 c Pressure 0.70072E-14 16 0.54424E-07 0.54424E-07 0.91244E+00 c k 0.29242E-06 2 0.30240E-07 0.11341E-08 0.12644E+01 c omega 0.13153E+02 1 0.88946E-09 0.13714E+00 0.19280E-02 c TempK 0.94752E+02 1 0.75275E-07 0.16880E-01 0.14372E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.9136e-14 7.4618e-14 -9.2815e-18 -2.421e-18 v Velocity[Y] -0.00012168 0.00011485 -4.2215e-10 -2.9099e-12 v Velocity[Z] -0.00011479 0.00012169 1.3607e-10 -1.8198e-12 v ǁVelocityǁ 3.3122e-10 0.00013043 1.1419e-05 8.3829e-06 v Pressure -0.0014567 0.023647 0.0013572 5.6184e-20 v k 5.5573e-10 0.00097828 0.00063413 0.00080966 v omega 12.569 1.0313e+05 2664.7 497.65 v TempK 288 342.11 294.25 291.18 v Density 1.205 1.205 1.205 1.205 v TurbVisc 6.5134e-15 9.3795e-05 5.5374e-05 7.2485e-05 v CourantNb 3.0886e-09 0.00019094 1.3834e-05 8.7945e-06 v FourierNb 0.089557 0.6281 0.18397 0.15481 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.958 4.958 0.00055968 -5.7661e-07 v volume_forces[Z] -4.958 4.958 -0.00055958 6.8345e-07 v ǁvolume_forcesǁ 1.182e-08 4.9591 0.56598 0.28504 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.46 291.32 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014841 5.2495e-05 2.9279e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.089575 0.6281 0.18398 0.15482 INSTANT 0.833958000E+00 TIME STEP NUMBER 866 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.47174E-05 0.22303E-02 Friction velocity uk : 0.47179E-05 0.22302E-02 Dimensionless distance yplus : 0.31419E-04 0.14838E-01 Friction thermal sca. tstar : -0.28003E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.22067E-04 0.10421E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.47174E-05 0.22303E-02 Friction velocity uk : 0.47179E-05 0.22302E-02 Dimensionless distance yplus : 0.31419E-04 0.14838E-01 Friction thermal sca. tstar : -0.28003E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.22067E-04 0.10421E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.37915E-08 3 0.97754E-07 0.17858E-12 0.83944E+00 c Velocity[X] 0.43102E-32 c Velocity[Y] 0.89288E-13 c Velocity[Z] 0.89294E-13 c Pressure 0.69952E-14 16 0.54330E-07 0.54330E-07 0.91133E+00 c k 0.29207E-06 2 0.30192E-07 0.11292E-08 0.12632E+01 c omega 0.13153E+02 1 0.88726E-09 0.13659E+00 0.19240E-02 c TempK 0.94753E+02 1 0.75152E-07 0.16850E-01 0.14359E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.9088e-14 7.4579e-14 -9.2769e-18 -2.4199e-18 v Velocity[Y] -0.00012166 0.00011483 -4.1969e-10 -2.9062e-12 v Velocity[Z] -0.00011477 0.00012167 1.3353e-10 -1.8197e-12 v ǁVelocityǁ 3.3569e-10 0.00013041 1.1423e-05 8.3887e-06 v Pressure -0.0014583 0.02366 0.0013581 -1.106e-19 v k 5.5401e-10 0.00097721 0.00063332 0.00080866 v omega 12.557 1.0313e+05 2664.7 497.64 v TempK 288 342.11 294.25 291.18 v Density 1.205 1.205 1.205 1.205 v TurbVisc 6.4933e-15 9.3785e-05 5.5357e-05 7.2465e-05 v CourantNb 3.091e-09 0.00019088 1.3835e-05 8.7979e-06 v FourierNb 0.08949 0.6281 0.18394 0.15477 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9581 4.9581 0.00055987 -5.7686e-07 v volume_forces[Z] -4.9581 4.9581 -0.00055977 6.8372e-07 v ǁvolume_forcesǁ 1.1974e-08 4.9591 0.56618 0.2852 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.46 291.32 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014838 5.2483e-05 2.9272e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.089509 0.6281 0.18395 0.15478 INSTANT 0.834921000E+00 TIME STEP NUMBER 867 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.48625E-05 0.22297E-02 Friction velocity uk : 0.48630E-05 0.22297E-02 Dimensionless distance yplus : 0.32386E-04 0.14835E-01 Friction thermal sca. tstar : -0.29522E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.22746E-04 0.10419E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.48625E-05 0.22297E-02 Friction velocity uk : 0.48630E-05 0.22297E-02 Dimensionless distance yplus : 0.32386E-04 0.14835E-01 Friction thermal sca. tstar : -0.29522E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.22746E-04 0.10419E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.37929E-08 3 0.97543E-07 0.17819E-12 0.83839E+00 c Velocity[X] 0.42947E-32 c Velocity[Y] 0.89092E-13 c Velocity[Z] 0.89099E-13 c Pressure 0.69833E-14 16 0.54237E-07 0.54237E-07 0.91023E+00 c k 0.29173E-06 2 0.30145E-07 0.11244E-08 0.12620E+01 c omega 0.13153E+02 1 0.88508E-09 0.13603E+00 0.19201E-02 c TempK 0.94753E+02 1 0.75029E-07 0.16821E-01 0.14346E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.904e-14 7.4541e-14 -9.2724e-18 -2.4189e-18 v Velocity[Y] -0.00012164 0.0001148 -4.1722e-10 -2.9025e-12 v Velocity[Z] -0.00011474 0.00012164 1.31e-10 -1.8196e-12 v ǁVelocityǁ 3.4036e-10 0.00013038 1.1426e-05 8.3945e-06 v Pressure -0.00146 0.023673 0.001359 1.2129e-19 v k 5.5231e-10 0.00097614 0.00063251 0.00080766 v omega 12.545 1.0313e+05 2664.7 497.63 v TempK 288 342.11 294.26 291.18 v Density 1.205 1.205 1.205 1.205 v TurbVisc 6.4733e-15 9.3775e-05 5.534e-05 7.2445e-05 v CourantNb 3.0933e-09 0.00019081 1.3835e-05 8.8014e-06 v FourierNb 0.089424 0.6281 0.1839 0.15474 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9581 4.9581 0.00056006 -5.7711e-07 v volume_forces[Z] -4.9581 4.9581 -0.00055996 6.8399e-07 v ǁvolume_forcesǁ 1.2135e-08 4.9591 0.56637 0.28536 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.46 291.32 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014835 5.2471e-05 2.9264e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.089443 0.6281 0.18392 0.15475 INSTANT 0.835884000E+00 TIME STEP NUMBER 868 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.50038E-05 0.22292E-02 Friction velocity uk : 0.50043E-05 0.22292E-02 Dimensionless distance yplus : 0.33326E-04 0.14831E-01 Friction thermal sca. tstar : -0.31305E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.23406E-04 0.10417E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.50038E-05 0.22292E-02 Friction velocity uk : 0.50043E-05 0.22292E-02 Dimensionless distance yplus : 0.33326E-04 0.14831E-01 Friction thermal sca. tstar : -0.31305E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.23406E-04 0.10417E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.37944E-08 3 0.97333E-07 0.17780E-12 0.83734E+00 c Velocity[X] 0.42793E-32 c Velocity[Y] 0.88897E-13 c Velocity[Z] 0.88903E-13 c Pressure 0.69761E-14 16 0.54180E-07 0.54180E-07 0.90913E+00 c k 0.29138E-06 2 0.30098E-07 0.11195E-08 0.12608E+01 c omega 0.13153E+02 1 0.88289E-09 0.13548E+00 0.19162E-02 c TempK 0.94754E+02 1 0.74906E-07 0.16792E-01 0.14334E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.8992e-14 7.4503e-14 -9.2678e-18 -2.4178e-18 v Velocity[Y] -0.00012162 0.00011478 -4.1476e-10 -2.8989e-12 v Velocity[Z] -0.00011471 0.00012162 1.2846e-10 -1.8194e-12 v ǁVelocityǁ 3.4522e-10 0.00013036 1.143e-05 8.4003e-06 v Pressure -0.0014616 0.023687 0.0013599 -4.0104e-20 v k 5.5061e-10 0.00097508 0.0006317 0.00080666 v omega 12.532 1.0313e+05 2664.7 497.62 v TempK 288 342.11 294.26 291.18 v Density 1.205 1.205 1.205 1.205 v TurbVisc 6.4533e-15 9.3765e-05 5.5324e-05 7.2425e-05 v CourantNb 3.0957e-09 0.00019075 1.3836e-05 8.8048e-06 v FourierNb 0.089358 0.6281 0.18387 0.15471 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9581 4.9582 0.00056026 -5.7736e-07 v volume_forces[Z] -4.9581 4.9582 -0.00056016 6.8426e-07 v ǁvolume_forcesǁ 1.2304e-08 4.9592 0.56656 0.28553 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.47 291.32 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014831 5.2459e-05 2.9257e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.089377 0.6281 0.18389 0.15471 INSTANT 0.836847000E+00 TIME STEP NUMBER 869 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.51415E-05 0.22287E-02 Friction velocity uk : 0.51420E-05 0.22287E-02 Dimensionless distance yplus : 0.34243E-04 0.14828E-01 Friction thermal sca. tstar : -0.33442E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.24050E-04 0.10414E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.51415E-05 0.22287E-02 Friction velocity uk : 0.51420E-05 0.22287E-02 Dimensionless distance yplus : 0.34243E-04 0.14828E-01 Friction thermal sca. tstar : -0.33442E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.24050E-04 0.10414E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.37959E-08 3 0.14323E-06 0.17741E-12 0.83629E+00 c Velocity[X] 0.42640E-32 c Velocity[Y] 0.88702E-13 c Velocity[Z] 0.88708E-13 c Pressure 0.69609E-14 16 0.54062E-07 0.54062E-07 0.90803E+00 c k 0.29103E-06 2 0.30051E-07 0.11147E-08 0.12596E+01 c omega 0.13153E+02 1 0.88072E-09 0.13493E+00 0.19123E-02 c TempK 0.94754E+02 1 0.74783E-07 0.16763E-01 0.14322E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.8944e-14 7.4465e-14 -9.2632e-18 -2.4167e-18 v Velocity[Y] -0.00012159 0.00011475 -4.1229e-10 -2.8952e-12 v Velocity[Z] -0.00011469 0.0001216 1.2592e-10 -1.8193e-12 v ǁVelocityǁ 3.5028e-10 0.00013033 1.1434e-05 8.4061e-06 v Pressure -0.0014633 0.0237 0.0013608 6.0597e-20 v k 5.4892e-10 0.00097401 0.00063089 0.00080566 v omega 12.52 1.0313e+05 2664.7 497.61 v TempK 288 342.11 294.26 291.19 v Density 1.205 1.205 1.205 1.205 v TurbVisc 6.4335e-15 9.3755e-05 5.5307e-05 7.2405e-05 v CourantNb 3.0981e-09 0.00019068 1.3836e-05 8.8082e-06 v FourierNb 0.089293 0.6281 0.18384 0.15467 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9582 4.9582 0.00056045 -5.776e-07 v volume_forces[Z] -4.9582 4.9582 -0.00056035 6.8453e-07 v ǁvolume_forcesǁ 1.248e-08 4.9592 0.56675 0.28569 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.47 291.33 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014828 5.2447e-05 2.925e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.089311 0.6281 0.18385 0.15468 INSTANT 0.837810000E+00 TIME STEP NUMBER 870 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.52759E-05 0.22282E-02 Friction velocity uk : 0.52764E-05 0.22282E-02 Dimensionless distance yplus : 0.35138E-04 0.14824E-01 Friction thermal sca. tstar : -0.36068E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.24679E-04 0.10412E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.52759E-05 0.22282E-02 Friction velocity uk : 0.52764E-05 0.22282E-02 Dimensionless distance yplus : 0.35138E-04 0.14824E-01 Friction thermal sca. tstar : -0.36068E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.24679E-04 0.10412E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.37973E-08 3 0.96917E-07 0.17702E-12 0.83525E+00 c Velocity[X] 0.42488E-32 c Velocity[Y] 0.88506E-13 c Velocity[Z] 0.88513E-13 c Pressure 0.69583E-14 16 0.54041E-07 0.54041E-07 0.90694E+00 c k 0.29068E-06 2 0.30005E-07 0.11099E-08 0.12584E+01 c omega 0.13153E+02 1 0.87855E-09 0.13438E+00 0.19084E-02 c TempK 0.94755E+02 1 0.74661E-07 0.16734E-01 0.14309E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.8896e-14 7.4427e-14 -9.2587e-18 -2.4156e-18 v Velocity[Y] -0.00012157 0.00011473 -4.0983e-10 -2.8916e-12 v Velocity[Z] -0.00011466 0.00012158 1.2339e-10 -1.8192e-12 v ǁVelocityǁ 3.5552e-10 0.00013031 1.1437e-05 8.4119e-06 v Pressure -0.0014649 0.023713 0.0013617 -2.0591e-21 v k 5.4724e-10 0.00097295 0.00063009 0.00080467 v omega 12.508 1.0313e+05 2664.7 497.6 v TempK 288 342.11 294.26 291.19 v Density 1.205 1.205 1.205 1.205 v TurbVisc 6.4137e-15 9.3745e-05 5.529e-05 7.2386e-05 v CourantNb 3.1005e-09 0.00019062 1.3837e-05 8.8117e-06 v FourierNb 0.089227 0.6281 0.18381 0.15464 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9582 4.9582 0.00056064 -5.7785e-07 v volume_forces[Z] -4.9582 4.9582 -0.00056054 6.848e-07 v ǁvolume_forcesǁ 1.2663e-08 4.9593 0.56694 0.28585 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.47 291.33 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014824 5.2435e-05 2.9243e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.089246 0.6281 0.18382 0.15465 INSTANT 0.838773000E+00 TIME STEP NUMBER 871 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.54072E-05 0.22277E-02 Friction velocity uk : 0.54077E-05 0.22277E-02 Dimensionless distance yplus : 0.36013E-04 0.14821E-01 Friction thermal sca. tstar : -0.39406E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.25293E-04 0.10409E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.54072E-05 0.22277E-02 Friction velocity uk : 0.54077E-05 0.22277E-02 Dimensionless distance yplus : 0.36013E-04 0.14821E-01 Friction thermal sca. tstar : -0.39406E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.25293E-04 0.10409E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.37988E-08 3 0.10869E-06 0.17663E-12 0.83420E+00 c Velocity[X] 0.42336E-32 c Velocity[Y] 0.88311E-13 c Velocity[Z] 0.88318E-13 c Pressure 0.69381E-14 16 0.53883E-07 0.53883E-07 0.90585E+00 c k 0.29034E-06 2 0.29958E-07 0.11051E-08 0.12571E+01 c omega 0.13153E+02 1 0.87640E-09 0.13384E+00 0.19046E-02 c TempK 0.94755E+02 1 0.74539E-07 0.16705E-01 0.14297E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.8849e-14 7.4389e-14 -9.2542e-18 -2.4146e-18 v Velocity[Y] -0.00012155 0.0001147 -4.0736e-10 -2.8881e-12 v Velocity[Z] -0.00011464 0.00012155 1.2085e-10 -1.8192e-12 v ǁVelocityǁ 3.6093e-10 0.00013029 1.1441e-05 8.4177e-06 v Pressure -0.0014666 0.023726 0.0013626 -7.7462e-21 v k 5.4556e-10 0.00097189 0.00062929 0.00080368 v omega 12.495 1.0313e+05 2664.7 497.59 v TempK 288 342.11 294.26 291.19 v Density 1.205 1.205 1.205 1.205 v TurbVisc 6.3941e-15 9.3736e-05 5.5274e-05 7.2366e-05 v CourantNb 3.1028e-09 0.00019055 1.3837e-05 8.8151e-06 v FourierNb 0.089162 0.6281 0.18377 0.1546 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9583 4.9583 0.00056083 -5.781e-07 v volume_forces[Z] -4.9583 4.9583 -0.00056073 6.8507e-07 v ǁvolume_forcesǁ 1.2852e-08 4.9593 0.56713 0.28602 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.47 291.33 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014821 5.2423e-05 2.9236e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.08918 0.6281 0.18379 0.15461 INSTANT 0.839736000E+00 TIME STEP NUMBER 872 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.55357E-05 0.22272E-02 Friction velocity uk : 0.55361E-05 0.22272E-02 Dimensionless distance yplus : 0.36868E-04 0.14818E-01 Friction thermal sca. tstar : -0.43849E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.25894E-04 0.10407E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.55357E-05 0.22272E-02 Friction velocity uk : 0.55361E-05 0.22272E-02 Dimensionless distance yplus : 0.36868E-04 0.14818E-01 Friction thermal sca. tstar : -0.43849E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.25894E-04 0.10407E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.38003E-08 3 0.96497E-07 0.17624E-12 0.83315E+00 c Velocity[X] 0.42185E-32 c Velocity[Y] 0.88117E-13 c Velocity[Z] 0.88123E-13 c Pressure 0.69276E-14 16 0.53801E-07 0.53801E-07 0.90476E+00 c k 0.28999E-06 2 0.29911E-07 0.11003E-08 0.12559E+01 c omega 0.13153E+02 1 0.87424E-09 0.13330E+00 0.19007E-02 c TempK 0.94756E+02 1 0.74418E-07 0.16677E-01 0.14284E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.8801e-14 7.4351e-14 -9.2496e-18 -2.4135e-18 v Velocity[Y] -0.00012153 0.00011468 -4.0489e-10 -2.8845e-12 v Velocity[Z] -0.00011461 0.00012153 1.1831e-10 -1.819e-12 v ǁVelocityǁ 3.6652e-10 0.00013026 1.1445e-05 8.4235e-06 v Pressure -0.0014682 0.02374 0.0013636 3.2554e-20 v k 5.4389e-10 0.00097084 0.00062849 0.00080269 v omega 12.483 1.0313e+05 2664.6 497.58 v TempK 288 342.11 294.27 291.19 v Density 1.205 1.205 1.205 1.205 v TurbVisc 6.3745e-15 9.3726e-05 5.5257e-05 7.2346e-05 v CourantNb 3.1052e-09 0.00019049 1.3838e-05 8.8185e-06 v FourierNb 0.089097 0.6281 0.18374 0.15457 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9583 4.9583 0.00056103 -5.7834e-07 v volume_forces[Z] -4.9583 4.9583 -0.00056092 6.8534e-07 v ǁvolume_forcesǁ 1.3048e-08 4.9593 0.56732 0.28618 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.47 291.33 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014818 5.2411e-05 2.9229e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.089115 0.6281 0.18376 0.15458 INSTANT 0.840699000E+00 TIME STEP NUMBER 873 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.56616E-05 0.22267E-02 Friction velocity uk : 0.56620E-05 0.22267E-02 Dimensionless distance yplus : 0.37706E-04 0.14814E-01 Friction thermal sca. tstar : -0.50189E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.26482E-04 0.10405E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.56616E-05 0.22267E-02 Friction velocity uk : 0.56620E-05 0.22267E-02 Dimensionless distance yplus : 0.37706E-04 0.14814E-01 Friction thermal sca. tstar : -0.50189E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.26482E-04 0.10405E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.38018E-08 3 0.96312E-07 0.17585E-12 0.83210E+00 c Velocity[X] 0.42034E-32 c Velocity[Y] 0.87922E-13 c Velocity[Z] 0.87929E-13 c Pressure 0.69126E-14 16 0.53684E-07 0.53684E-07 0.90367E+00 c k 0.28965E-06 2 0.29865E-07 0.10956E-08 0.12547E+01 c omega 0.13153E+02 1 0.87210E-09 0.13276E+00 0.18969E-02 c TempK 0.94757E+02 1 0.74296E-07 0.16648E-01 0.14272E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.8754e-14 7.4313e-14 -9.2451e-18 -2.4124e-18 v Velocity[Y] -0.0001215 0.00011465 -4.0242e-10 -2.8809e-12 v Velocity[Z] -0.00011459 0.00012151 1.1578e-10 -1.8189e-12 v ǁVelocityǁ 3.7227e-10 0.00013024 1.1448e-05 8.4293e-06 v Pressure -0.0014699 0.023753 0.0013645 -4.7458e-20 v k 5.4222e-10 0.00096978 0.00062769 0.0008017 v omega 12.471 1.0313e+05 2664.6 497.57 v TempK 288 342.11 294.27 291.19 v Density 1.205 1.205 1.205 1.205 v TurbVisc 6.3549e-15 9.3716e-05 5.5241e-05 7.2327e-05 v CourantNb 3.1075e-09 0.00019043 1.3838e-05 8.8219e-06 v FourierNb 0.089032 0.6281 0.18371 0.15454 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9584 4.9584 0.00056122 -5.7859e-07 v volume_forces[Z] -4.9584 4.9584 -0.00056112 6.856e-07 v ǁvolume_forcesǁ 1.325e-08 4.9594 0.56751 0.28634 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.48 291.33 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014814 5.2399e-05 2.9221e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.08905 0.6281 0.18372 0.15455 INSTANT 0.841662000E+00 TIME STEP NUMBER 874 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.57849E-05 0.22262E-02 Friction velocity uk : 0.57853E-05 0.22262E-02 Dimensionless distance yplus : 0.38528E-04 0.14811E-01 Friction thermal sca. tstar : -0.60339E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.27059E-04 0.10402E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.57849E-05 0.22262E-02 Friction velocity uk : 0.57853E-05 0.22262E-02 Dimensionless distance yplus : 0.38528E-04 0.14811E-01 Friction thermal sca. tstar : -0.60339E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.27059E-04 0.10402E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.38032E-08 3 0.96080E-07 0.17546E-12 0.83105E+00 c Velocity[X] 0.41884E-32 c Velocity[Y] 0.87727E-13 c Velocity[Z] 0.87734E-13 c Pressure 0.69011E-14 16 0.53594E-07 0.53594E-07 0.90259E+00 c k 0.28930E-06 2 0.29819E-07 0.10909E-08 0.12535E+01 c omega 0.13153E+02 1 0.86996E-09 0.13222E+00 0.18930E-02 c TempK 0.94757E+02 1 0.74176E-07 0.16619E-01 0.14259E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.8706e-14 7.4275e-14 -9.2406e-18 -2.4114e-18 v Velocity[Y] -0.00012148 0.00011462 -3.9995e-10 -2.8773e-12 v Velocity[Z] -0.00011456 0.00012149 1.1324e-10 -1.8188e-12 v ǁVelocityǁ 3.7818e-10 0.00013021 1.1452e-05 8.4351e-06 v Pressure -0.0014715 0.023766 0.0013654 4.2261e-20 v k 5.4057e-10 0.00096873 0.00062689 0.00080071 v omega 12.459 1.0313e+05 2664.6 497.55 v TempK 288 342.12 294.27 291.19 v Density 1.205 1.205 1.205 1.205 v TurbVisc 6.3355e-15 9.3706e-05 5.5224e-05 7.2307e-05 v CourantNb 3.1099e-09 0.00019036 1.3839e-05 8.8254e-06 v FourierNb 0.088967 0.6281 0.18368 0.1545 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9584 4.9584 0.00056141 -5.7883e-07 v volume_forces[Z] -4.9584 4.9584 -0.00056131 6.8587e-07 v ǁvolume_forcesǁ 1.3458e-08 4.9594 0.5677 0.2865 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.48 291.34 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014811 5.2387e-05 2.9214e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.088986 0.6281 0.18369 0.15451 INSTANT 0.842625000E+00 TIME STEP NUMBER 875 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.59060E-05 0.22257E-02 Friction velocity uk : 0.59063E-05 0.22257E-02 Dimensionless distance yplus : 0.39334E-04 0.14808E-01 Friction thermal sca. tstar : -0.80811E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.27625E-04 0.10400E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.59060E-05 0.22257E-02 Friction velocity uk : 0.59063E-05 0.22257E-02 Dimensionless distance yplus : 0.39334E-04 0.14808E-01 Friction thermal sca. tstar : -0.80811E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.27625E-04 0.10400E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.38047E-08 3 0.95877E-07 0.17507E-12 0.83001E+00 c Velocity[X] 0.41735E-32 c Velocity[Y] 0.87533E-13 c Velocity[Z] 0.87540E-13 c Pressure 0.69019E-14 16 0.53600E-07 0.53600E-07 0.90151E+00 c k 0.28896E-06 2 0.29773E-07 0.10862E-08 0.12523E+01 c omega 0.13153E+02 1 0.86783E-09 0.13169E+00 0.18892E-02 c TempK 0.94758E+02 1 0.74055E-07 0.16591E-01 0.14247E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.8659e-14 7.4237e-14 -9.2361e-18 -2.4103e-18 v Velocity[Y] -0.00012146 0.0001146 -3.9748e-10 -2.8738e-12 v Velocity[Z] -0.00011453 0.00012146 1.107e-10 -1.8186e-12 v ǁVelocityǁ 3.8425e-10 0.00013019 1.1456e-05 8.4408e-06 v Pressure -0.0014732 0.023779 0.0013663 7.6089e-20 v k 5.3892e-10 0.00096768 0.00062609 0.00079973 v omega 12.446 1.0313e+05 2664.6 497.54 v TempK 288 342.12 294.27 291.2 v Density 1.205 1.205 1.205 1.205 v TurbVisc 6.3162e-15 9.3696e-05 5.5208e-05 7.2287e-05 v CourantNb 3.1122e-09 0.0001903 1.3839e-05 8.8288e-06 v FourierNb 0.088903 0.6281 0.18365 0.15447 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9584 4.9585 0.0005616 -5.7908e-07 v volume_forces[Z] -4.9584 4.9585 -0.0005615 6.8614e-07 v ǁvolume_forcesǁ 1.3671e-08 4.9595 0.56789 0.28667 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.48 291.34 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014808 5.2375e-05 2.9207e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.088921 0.6281 0.18366 0.15448 INSTANT 0.843588000E+00 TIME STEP NUMBER 876 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.60248E-05 0.22252E-02 Friction velocity uk : 0.60252E-05 0.22252E-02 Dimensionless distance yplus : 0.40125E-04 0.14804E-01 Friction thermal sca. tstar : -0.17573E+05 0.00000E+00 Dim-less thermal sca. tplus : 0.28181E-04 0.10398E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.60248E-05 0.22252E-02 Friction velocity uk : 0.60252E-05 0.22252E-02 Dimensionless distance yplus : 0.40125E-04 0.14804E-01 Friction thermal sca. tstar : -0.17573E+05 0.00000E+00 Dim-less thermal sca. tplus : 0.28181E-04 0.10398E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.38062E-08 3 0.95669E-07 0.17468E-12 0.82896E+00 c Velocity[X] 0.41587E-32 c Velocity[Y] 0.87339E-13 c Velocity[Z] 0.87346E-13 c Pressure 0.68785E-14 16 0.53417E-07 0.53417E-07 0.90043E+00 c k 0.28862E-06 2 0.29727E-07 0.10816E-08 0.12511E+01 c omega 0.13153E+02 1 0.86571E-09 0.13116E+00 0.18854E-02 c TempK 0.94758E+02 1 0.73935E-07 0.16563E-01 0.14235E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.8612e-14 7.42e-14 -9.2316e-18 -2.4093e-18 v Velocity[Y] -0.00012144 0.00011457 -3.9501e-10 -2.8702e-12 v Velocity[Z] -0.00011451 0.00012144 1.0817e-10 -1.8185e-12 v ǁVelocityǁ 3.9046e-10 0.00013016 1.1459e-05 8.4466e-06 v Pressure -0.0014749 0.023792 0.0013672 5.0497e-20 v k 5.3728e-10 0.00096663 0.0006253 0.00079875 v omega 12.434 1.0313e+05 2664.6 497.53 v TempK 288 342.12 294.28 291.2 v Density 1.205 1.205 1.205 1.205 v TurbVisc 6.2969e-15 9.3686e-05 5.5191e-05 7.2268e-05 v CourantNb 3.1146e-09 0.00019024 1.384e-05 8.8322e-06 v FourierNb 0.088838 0.6281 0.18361 0.15444 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9585 4.9585 0.00056179 -5.7932e-07 v volume_forces[Z] -4.9585 4.9585 -0.00056169 6.864e-07 v ǁvolume_forcesǁ 1.389e-08 4.9595 0.56808 0.28683 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.48 291.34 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014804 5.2362e-05 2.9199e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.088857 0.6281 0.18363 0.15444 INSTANT 0.844551000E+00 TIME STEP NUMBER 877 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.61417E-05 0.22247E-02 Friction velocity uk : 0.61420E-05 0.22247E-02 Dimensionless distance yplus : 0.40903E-04 0.14801E-01 Friction thermal sca. tstar : -0.20722E+05 0.00000E+00 Dim-less thermal sca. tplus : 0.28728E-04 0.10395E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.61417E-05 0.22247E-02 Friction velocity uk : 0.61420E-05 0.22247E-02 Dimensionless distance yplus : 0.40903E-04 0.14801E-01 Friction thermal sca. tstar : -0.20722E+05 0.00000E+00 Dim-less thermal sca. tplus : 0.28728E-04 0.10395E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.38076E-08 3 0.95446E-07 0.17430E-12 0.82791E+00 c Velocity[X] 0.41440E-32 c Velocity[Y] 0.87145E-13 c Velocity[Z] 0.87152E-13 c Pressure 0.68562E-14 17 0.53244E-07 0.53244E-07 0.89935E+00 c k 0.28828E-06 2 0.29681E-07 0.10769E-08 0.12499E+01 c omega 0.13153E+02 1 0.86359E-09 0.13063E+00 0.18816E-02 c TempK 0.94759E+02 1 0.73815E-07 0.16534E-01 0.14223E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.8564e-14 7.4162e-14 -9.2271e-18 -2.4082e-18 v Velocity[Y] -0.00012141 0.00011455 -3.9293e-10 -3.2008e-12 v Velocity[Z] -0.00011448 0.00012142 1.0591e-10 -1.5487e-12 v ǁVelocityǁ 3.9787e-10 0.00013014 1.1463e-05 8.4524e-06 v Pressure -0.0014765 0.023806 0.0013681 -5.9518e-20 v k 5.3564e-10 0.00096559 0.00062451 0.00079777 v omega 12.422 1.0313e+05 2664.6 497.52 v TempK 288 342.12 294.28 291.2 v Density 1.205 1.205 1.205 1.205 v TurbVisc 6.2777e-15 9.3677e-05 5.5175e-05 7.2248e-05 v CourantNb 3.1176e-09 0.00019017 1.3841e-05 8.8356e-06 v FourierNb 0.088774 0.6281 0.18358 0.1544 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9585 4.9585 0.00056198 -5.7957e-07 v volume_forces[Z] -4.9585 4.9585 -0.00056188 6.8667e-07 v ǁvolume_forcesǁ 1.4115e-08 4.9596 0.56827 0.28699 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.48 291.34 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014801 5.2351e-05 2.9192e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.088792 0.6281 0.1836 0.15441 INSTANT 0.845514000E+00 TIME STEP NUMBER 878 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.62740E-05 0.22242E-02 Friction velocity uk : 0.62744E-05 0.22241E-02 Dimensionless distance yplus : 0.41784E-04 0.14798E-01 Friction thermal sca. tstar : -0.83729E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.29347E-04 0.10393E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.62740E-05 0.22242E-02 Friction velocity uk : 0.62744E-05 0.22241E-02 Dimensionless distance yplus : 0.41784E-04 0.14798E-01 Friction thermal sca. tstar : -0.83729E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.29347E-04 0.10393E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.38091E-08 3 0.95231E-07 0.17391E-12 0.82686E+00 c Velocity[X] 0.41283E-32 c Velocity[Y] 0.86951E-13 c Velocity[Z] 0.86958E-13 c Pressure 0.68450E-14 17 0.53156E-07 0.53156E-07 0.89827E+00 c k 0.28794E-06 2 0.29635E-07 0.10723E-08 0.12487E+01 c omega 0.13153E+02 1 0.86148E-09 0.13010E+00 0.18778E-02 c TempK 0.94759E+02 1 0.73695E-07 0.16506E-01 0.14210E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.8517e-14 7.4125e-14 -9.2226e-18 -2.4072e-18 v Velocity[Y] -0.00012139 0.00011452 -3.9044e-10 -3.1888e-12 v Velocity[Z] -0.00011446 0.0001214 1.0338e-10 -1.5357e-12 v ǁVelocityǁ 4.0411e-10 0.00013011 1.1467e-05 8.4581e-06 v Pressure -0.0014782 0.023819 0.001369 2.922e-20 v k 5.3401e-10 0.00096455 0.00062372 0.00079679 v omega 12.41 1.0313e+05 2664.6 497.51 v TempK 288 342.12 294.28 291.2 v Density 1.205 1.205 1.205 1.205 v TurbVisc 6.2586e-15 9.3667e-05 5.5158e-05 7.2228e-05 v CourantNb 3.12e-09 0.00019011 1.3841e-05 8.839e-06 v FourierNb 0.08871 0.6281 0.18355 0.15437 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9586 4.9586 0.00056217 -5.798e-07 v volume_forces[Z] -4.9586 4.9586 -0.00056207 6.8695e-07 v ǁvolume_forcesǁ 1.4383e-08 4.9596 0.56846 0.28715 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.49 291.34 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014798 5.234e-05 2.9186e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.088728 0.6281 0.18356 0.15438 INSTANT 0.846477000E+00 TIME STEP NUMBER 879 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.63813E-05 0.22237E-02 Friction velocity uk : 0.63816E-05 0.22236E-02 Dimensionless distance yplus : 0.42499E-04 0.14794E-01 Friction thermal sca. tstar : -0.61874E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.29848E-04 0.10391E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.63813E-05 0.22237E-02 Friction velocity uk : 0.63816E-05 0.22236E-02 Dimensionless distance yplus : 0.42499E-04 0.14794E-01 Friction thermal sca. tstar : -0.61874E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.29848E-04 0.10391E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.38106E-08 3 0.95055E-07 0.17352E-12 0.82581E+00 c Velocity[X] 0.41139E-32 c Velocity[Y] 0.86758E-13 c Velocity[Z] 0.86765E-13 c Pressure 0.68397E-14 17 0.53114E-07 0.53114E-07 0.89720E+00 c k 0.28760E-06 2 0.29589E-07 0.10677E-08 0.12476E+01 c omega 0.13153E+02 1 0.85938E-09 0.12958E+00 0.18740E-02 c TempK 0.94760E+02 1 0.73576E-07 0.16478E-01 0.14198E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.847e-14 7.4087e-14 -9.2182e-18 -2.4061e-18 v Velocity[Y] -0.00012137 0.0001145 -3.8796e-10 -3.1889e-12 v Velocity[Z] -0.00011443 0.00012138 1.0084e-10 -1.5429e-12 v ǁVelocityǁ 4.1059e-10 0.00013009 1.147e-05 8.4639e-06 v Pressure -0.0014798 0.023832 0.0013699 -4.8144e-20 v k 5.3239e-10 0.0009635 0.00062293 0.00079582 v omega 12.398 1.0313e+05 2664.6 497.5 v TempK 288 342.12 294.28 291.2 v Density 1.205 1.205 1.205 1.205 v TurbVisc 6.2395e-15 9.3657e-05 5.5142e-05 7.2209e-05 v CourantNb 3.1223e-09 0.00019005 1.3842e-05 8.8424e-06 v FourierNb 0.088646 0.6281 0.18352 0.15434 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9586 4.9586 0.00056236 -5.8004e-07 v volume_forces[Z] -4.9586 4.9586 -0.00056226 6.8721e-07 v ǁvolume_forcesǁ 1.4609e-08 4.9596 0.56864 0.28732 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.49 291.34 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014794 5.2329e-05 2.9179e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.088664 0.6281 0.18353 0.15434 INSTANT 0.847440000E+00 TIME STEP NUMBER 880 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.64897E-05 0.22232E-02 Friction velocity uk : 0.64900E-05 0.22231E-02 Dimensionless distance yplus : 0.43221E-04 0.14791E-01 Friction thermal sca. tstar : -0.51369E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.30356E-04 0.10388E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.64897E-05 0.22232E-02 Friction velocity uk : 0.64900E-05 0.22231E-02 Dimensionless distance yplus : 0.43221E-04 0.14791E-01 Friction thermal sca. tstar : -0.51369E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.30356E-04 0.10388E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.38120E-08 3 0.94870E-07 0.17314E-12 0.82477E+00 c Velocity[X] 0.40998E-32 c Velocity[Y] 0.86564E-13 c Velocity[Z] 0.86571E-13 c Pressure 0.68557E-14 17 0.53238E-07 0.53238E-07 0.89613E+00 c k 0.28726E-06 2 0.29544E-07 0.10632E-08 0.12464E+01 c omega 0.13153E+02 1 0.85729E-09 0.12906E+00 0.18703E-02 c TempK 0.94760E+02 1 0.73457E-07 0.16450E-01 0.14186E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.8423e-14 7.405e-14 -9.2137e-18 -2.4051e-18 v Velocity[Y] -0.00012135 0.00011447 -3.8549e-10 -3.1858e-12 v Velocity[Z] -0.00011441 0.00012135 9.8304e-11 -1.5429e-12 v ǁVelocityǁ 4.0831e-10 0.00013007 1.1474e-05 8.4696e-06 v Pressure -0.0014815 0.023845 0.0013708 -7.5501e-21 v k 5.3077e-10 0.00096247 0.00062214 0.00079484 v omega 12.386 1.0313e+05 2664.6 497.49 v TempK 288 342.12 294.28 291.21 v Density 1.205 1.205 1.205 1.205 v TurbVisc 6.2206e-15 9.3647e-05 5.5125e-05 7.2189e-05 v CourantNb 3.1246e-09 0.00018998 1.3842e-05 8.8458e-06 v FourierNb 0.088582 0.6281 0.18349 0.1543 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9587 4.9587 0.00056255 -5.8029e-07 v volume_forces[Z] -4.9587 4.9587 -0.00056245 6.8748e-07 v ǁvolume_forcesǁ 1.4843e-08 4.9597 0.56883 0.28748 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.49 291.35 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014791 5.2318e-05 2.9173e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.088601 0.6281 0.1835 0.15431 INSTANT 0.848403000E+00 TIME STEP NUMBER 881 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.65977E-05 0.22227E-02 Friction velocity uk : 0.65980E-05 0.22226E-02 Dimensionless distance yplus : 0.43939E-04 0.14788E-01 Friction thermal sca. tstar : -0.44904E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.30860E-04 0.10386E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.65977E-05 0.22227E-02 Friction velocity uk : 0.65980E-05 0.22226E-02 Dimensionless distance yplus : 0.43939E-04 0.14788E-01 Friction thermal sca. tstar : -0.44904E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.30860E-04 0.10386E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.38135E-08 3 0.94668E-07 0.17275E-12 0.82372E+00 c Velocity[X] 0.40855E-32 c Velocity[Y] 0.86371E-13 c Velocity[Z] 0.86378E-13 c Pressure 0.68143E-14 17 0.52916E-07 0.52916E-07 0.89507E+00 c k 0.28692E-06 2 0.29498E-07 0.10586E-08 0.12452E+01 c omega 0.13153E+02 1 0.85520E-09 0.12854E+00 0.18665E-02 c TempK 0.94761E+02 1 0.73339E-07 0.16422E-01 0.14174E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.8376e-14 7.4013e-14 -9.2092e-18 -2.404e-18 v Velocity[Y] -0.00012133 0.00011445 -3.8301e-10 -3.1821e-12 v Velocity[Z] -0.00011438 0.00012133 9.5768e-11 -1.5432e-12 v ǁVelocityǁ 4.0405e-10 0.00013004 1.1478e-05 8.4753e-06 v Pressure -0.0014831 0.023858 0.0013717 -3.1181e-20 v k 5.2916e-10 0.00096143 0.00062136 0.00079387 v omega 12.374 1.0313e+05 2664.6 497.48 v TempK 288 342.12 294.29 291.21 v Density 1.205 1.205 1.205 1.205 v TurbVisc 6.2017e-15 9.3637e-05 5.5109e-05 7.217e-05 v CourantNb 3.127e-09 0.00018992 1.3843e-05 8.8492e-06 v FourierNb 0.088519 0.6281 0.18345 0.15427 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9587 4.9587 0.00056274 -5.8053e-07 v volume_forces[Z] -4.9587 4.9587 -0.00056265 6.8774e-07 v ǁvolume_forcesǁ 1.476e-08 4.9597 0.56902 0.28764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.49 291.35 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014788 5.2307e-05 2.9166e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.088537 0.6281 0.18347 0.15428 INSTANT 0.849366000E+00 TIME STEP NUMBER 882 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.67046E-05 0.22222E-02 Friction velocity uk : 0.67049E-05 0.22221E-02 Dimensionless distance yplus : 0.44652E-04 0.14784E-01 Friction thermal sca. tstar : -0.40419E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.31360E-04 0.10384E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.67046E-05 0.22222E-02 Friction velocity uk : 0.67049E-05 0.22221E-02 Dimensionless distance yplus : 0.44652E-04 0.14784E-01 Friction thermal sca. tstar : -0.40419E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.31360E-04 0.10384E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.38150E-08 3 0.94459E-07 0.17236E-12 0.82267E+00 c Velocity[X] 0.40714E-32 c Velocity[Y] 0.86178E-13 c Velocity[Z] 0.86185E-13 c Pressure 0.68014E-14 17 0.52815E-07 0.52815E-07 0.89400E+00 c k 0.28658E-06 2 0.29453E-07 0.10541E-08 0.12440E+01 c omega 0.13153E+02 1 0.85312E-09 0.12803E+00 0.18628E-02 c TempK 0.94761E+02 1 0.73221E-07 0.16394E-01 0.14162E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.833e-14 7.3975e-14 -9.2048e-18 -2.403e-18 v Velocity[Y] -0.0001213 0.00011442 -3.8053e-10 -3.1786e-12 v Velocity[Z] -0.00011436 0.00012131 9.3232e-11 -1.5434e-12 v ǁVelocityǁ 3.9983e-10 0.00013002 1.1481e-05 8.4811e-06 v Pressure -0.0014848 0.023871 0.0013726 -6.648e-20 v k 5.2756e-10 0.00096039 0.00062058 0.0007929 v omega 12.362 1.0313e+05 2664.6 497.47 v TempK 288 342.12 294.29 291.21 v Density 1.205 1.205 1.205 1.205 v TurbVisc 6.1829e-15 9.3628e-05 5.5092e-05 7.215e-05 v CourantNb 3.1293e-09 0.00018986 1.3843e-05 8.8526e-06 v FourierNb 0.088455 0.6281 0.18342 0.15424 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9587 4.9588 0.00056293 -5.8077e-07 v volume_forces[Z] -4.9587 4.9588 -0.00056284 6.8801e-07 v ǁvolume_forcesǁ 1.4606e-08 4.9598 0.56921 0.2878 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.5 291.35 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014784 5.2295e-05 2.9159e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.088474 0.6281 0.18344 0.15424 INSTANT 0.850329000E+00 TIME STEP NUMBER 883 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.68104E-05 0.22217E-02 Friction velocity uk : 0.68107E-05 0.22216E-02 Dimensionless distance yplus : 0.45356E-04 0.14781E-01 Friction thermal sca. tstar : -0.37075E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.31855E-04 0.10381E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.68104E-05 0.22217E-02 Friction velocity uk : 0.68107E-05 0.22216E-02 Dimensionless distance yplus : 0.45356E-04 0.14781E-01 Friction thermal sca. tstar : -0.37075E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.31855E-04 0.10381E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.38165E-08 3 0.94257E-07 0.17198E-12 0.82162E+00 c Velocity[X] 0.40571E-32 c Velocity[Y] 0.85985E-13 c Velocity[Z] 0.85992E-13 c Pressure 0.68090E-14 17 0.52873E-07 0.52873E-07 0.89294E+00 c k 0.28624E-06 2 0.29408E-07 0.10497E-08 0.12428E+01 c omega 0.13153E+02 1 0.85104E-09 0.12751E+00 0.18590E-02 c TempK 0.94762E+02 1 0.73103E-07 0.16366E-01 0.14149E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.8283e-14 7.3938e-14 -9.2003e-18 -2.4019e-18 v Velocity[Y] -0.00012128 0.0001144 -3.7804e-10 -3.175e-12 v Velocity[Z] -0.00011433 0.00012129 9.0696e-11 -1.5436e-12 v ǁVelocityǁ 3.9566e-10 0.00012999 1.1485e-05 8.4868e-06 v Pressure -0.0014864 0.023884 0.0013735 4.785e-20 v k 5.2596e-10 0.00095936 0.00061979 0.00079194 v omega 12.35 1.0313e+05 2664.6 497.46 v TempK 288 342.12 294.29 291.21 v Density 1.205 1.205 1.205 1.205 v TurbVisc 6.1642e-15 9.3618e-05 5.5076e-05 7.2131e-05 v CourantNb 3.1316e-09 0.00018979 1.3844e-05 8.856e-06 v FourierNb 0.088392 0.6281 0.18339 0.1542 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9588 4.9588 0.00056312 -5.8101e-07 v volume_forces[Z] -4.9588 4.9588 -0.00056303 6.8827e-07 v ǁvolume_forcesǁ 1.4454e-08 4.9598 0.5694 0.28796 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.5 291.35 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014781 5.2284e-05 2.9153e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.08841 0.6281 0.1834 0.15421 INSTANT 0.851292000E+00 TIME STEP NUMBER 884 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.67800E-05 0.22212E-02 Friction velocity uk : 0.67803E-05 0.22211E-02 Dimensionless distance yplus : 0.45149E-04 0.14778E-01 Friction thermal sca. tstar : -0.34460E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.31710E-04 0.10379E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.67800E-05 0.22212E-02 Friction velocity uk : 0.67803E-05 0.22211E-02 Dimensionless distance yplus : 0.45149E-04 0.14778E-01 Friction thermal sca. tstar : -0.34460E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.31710E-04 0.10379E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.38179E-08 3 0.94058E-07 0.17159E-12 0.82057E+00 c Velocity[X] 0.40429E-32 c Velocity[Y] 0.85792E-13 c Velocity[Z] 0.85799E-13 c Pressure 0.67955E-14 17 0.52768E-07 0.52768E-07 0.89188E+00 c k 0.28591E-06 2 0.29362E-07 0.10452E-08 0.12416E+01 c omega 0.13153E+02 1 0.84898E-09 0.12700E+00 0.18553E-02 c TempK 0.94762E+02 1 0.72985E-07 0.16338E-01 0.14137E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.8236e-14 7.3901e-14 -9.1959e-18 -2.4009e-18 v Velocity[Y] -0.00012126 0.00011437 -3.7556e-10 -3.1715e-12 v Velocity[Z] -0.00011431 0.00012126 8.8161e-11 -1.5438e-12 v ǁVelocityǁ 3.9152e-10 0.00012997 1.1488e-05 8.4925e-06 v Pressure -0.0014881 0.023897 0.0013744 -5.5498e-20 v k 5.2437e-10 0.00095833 0.00061901 0.00079097 v omega 12.338 1.0313e+05 2664.5 497.45 v TempK 288 342.12 294.29 291.21 v Density 1.205 1.205 1.205 1.205 v TurbVisc 6.1455e-15 9.3608e-05 5.506e-05 7.2111e-05 v CourantNb 3.1339e-09 0.00018973 1.3845e-05 8.8594e-06 v FourierNb 0.088329 0.6281 0.18336 0.15417 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9588 4.9588 0.00056331 -5.8125e-07 v volume_forces[Z] -4.9588 4.9588 -0.00056322 6.8853e-07 v ǁvolume_forcesǁ 1.4303e-08 4.9598 0.56959 0.28812 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.5 291.35 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014778 5.2273e-05 2.9146e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.088347 0.6281 0.18337 0.15418 INSTANT 0.852255000E+00 TIME STEP NUMBER 885 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.67182E-05 0.22207E-02 Friction velocity uk : 0.67185E-05 0.22206E-02 Dimensionless distance yplus : 0.44738E-04 0.14774E-01 Friction thermal sca. tstar : -0.32344E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.31421E-04 0.10377E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.67182E-05 0.22207E-02 Friction velocity uk : 0.67185E-05 0.22206E-02 Dimensionless distance yplus : 0.44738E-04 0.14774E-01 Friction thermal sca. tstar : -0.32344E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.31421E-04 0.10377E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.38194E-08 3 0.93887E-07 0.17121E-12 0.81953E+00 c Velocity[X] 0.40286E-32 c Velocity[Y] 0.85599E-13 c Velocity[Z] 0.85607E-13 c Pressure 0.68044E-14 17 0.52836E-07 0.52836E-07 0.89083E+00 c k 0.28557E-06 2 0.29317E-07 0.10407E-08 0.12405E+01 c omega 0.13153E+02 1 0.84691E-09 0.12650E+00 0.18516E-02 c TempK 0.94763E+02 1 0.72868E-07 0.16310E-01 0.14125E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.819e-14 7.3864e-14 -9.1915e-18 -2.3998e-18 v Velocity[Y] -0.00012124 0.00011435 -3.7308e-10 -3.168e-12 v Velocity[Z] -0.00011428 0.00012124 8.5626e-11 -1.5441e-12 v ǁVelocityǁ 3.8741e-10 0.00012995 1.1492e-05 8.4982e-06 v Pressure -0.0014897 0.023911 0.0013753 -2.8435e-21 v k 5.2279e-10 0.0009573 0.00061824 0.00079001 v omega 12.326 1.0313e+05 2664.5 497.44 v TempK 288 342.12 294.29 291.22 v Density 1.205 1.205 1.205 1.205 v TurbVisc 6.1269e-15 9.3599e-05 5.5043e-05 7.2092e-05 v CourantNb 3.1361e-09 0.00018967 1.3845e-05 8.8628e-06 v FourierNb 0.088266 0.6281 0.18333 0.15414 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9589 4.9589 0.0005635 -5.8149e-07 v volume_forces[Z] -4.9589 4.9589 -0.00056341 6.8879e-07 v ǁvolume_forcesǁ 1.4153e-08 4.9599 0.56977 0.28829 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.5 291.36 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014774 5.2262e-05 2.9139e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.088284 0.6281 0.18334 0.15414 INSTANT 0.853218000E+00 TIME STEP NUMBER 886 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.66557E-05 0.22202E-02 Friction velocity uk : 0.66560E-05 0.22201E-02 Dimensionless distance yplus : 0.44322E-04 0.14771E-01 Friction thermal sca. tstar : -0.30587E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.31129E-04 0.10374E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.66557E-05 0.22202E-02 Friction velocity uk : 0.66560E-05 0.22201E-02 Dimensionless distance yplus : 0.44322E-04 0.14771E-01 Friction thermal sca. tstar : -0.30587E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.31129E-04 0.10374E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.38209E-08 3 0.93654E-07 0.17082E-12 0.81848E+00 c Velocity[X] 0.40148E-32 c Velocity[Y] 0.85407E-13 c Velocity[Z] 0.85414E-13 c Pressure 0.67669E-14 17 0.52544E-07 0.52544E-07 0.88977E+00 c k 0.28524E-06 2 0.29272E-07 0.10363E-08 0.12393E+01 c omega 0.13153E+02 1 0.84486E-09 0.12599E+00 0.18479E-02 c TempK 0.94764E+02 1 0.72751E-07 0.16283E-01 0.14113E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.8143e-14 7.3827e-14 -9.1871e-18 -2.3988e-18 v Velocity[Y] -0.00012122 0.00011433 -3.706e-10 -3.1645e-12 v Velocity[Z] -0.00011426 0.00012122 8.309e-11 -1.5443e-12 v ǁVelocityǁ 3.8333e-10 0.00012992 1.1496e-05 8.5039e-06 v Pressure -0.0014914 0.023924 0.0013762 4.5497e-20 v k 5.2122e-10 0.00095628 0.00061746 0.00078905 v omega 12.314 1.0313e+05 2664.5 497.43 v TempK 288 342.12 294.3 291.22 v Density 1.205 1.205 1.205 1.205 v TurbVisc 6.1085e-15 9.3589e-05 5.5027e-05 7.2072e-05 v CourantNb 3.1384e-09 0.00018961 1.3846e-05 8.8662e-06 v FourierNb 0.088204 0.6281 0.1833 0.1541 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9589 4.9589 0.00056369 -5.8173e-07 v volume_forces[Z] -4.9589 4.9589 -0.00056359 6.8906e-07 v ǁvolume_forcesǁ 1.4005e-08 4.9599 0.56996 0.28845 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.5 291.36 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014771 5.225e-05 2.9132e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.088222 0.6281 0.18331 0.15411 INSTANT 0.854181000E+00 TIME STEP NUMBER 887 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.65926E-05 0.22197E-02 Friction velocity uk : 0.65929E-05 0.22197E-02 Dimensionless distance yplus : 0.43902E-04 0.14768E-01 Friction thermal sca. tstar : -0.29098E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.30834E-04 0.10372E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.65926E-05 0.22197E-02 Friction velocity uk : 0.65929E-05 0.22197E-02 Dimensionless distance yplus : 0.43902E-04 0.14768E-01 Friction thermal sca. tstar : -0.29098E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.30834E-04 0.10372E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.38223E-08 3 0.93458E-07 0.17044E-12 0.81743E+00 c Velocity[X] 0.40006E-32 c Velocity[Y] 0.85215E-13 c Velocity[Z] 0.85222E-13 c Pressure 0.67511E-14 17 0.52422E-07 0.52422E-07 0.88872E+00 c k 0.28490E-06 2 0.29227E-07 0.10319E-08 0.12381E+01 c omega 0.13153E+02 1 0.84281E-09 0.12549E+00 0.18442E-02 c TempK 0.94764E+02 1 0.72634E-07 0.16255E-01 0.14101E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.8097e-14 7.379e-14 -9.1827e-18 -2.3978e-18 v Velocity[Y] -0.00012119 0.0001143 -3.6811e-10 -3.161e-12 v Velocity[Z] -0.00011423 0.0001212 8.0555e-11 -1.5444e-12 v ǁVelocityǁ 3.7928e-10 0.0001299 1.1499e-05 8.5096e-06 v Pressure -0.001493 0.023937 0.0013771 -6.1871e-20 v k 5.1965e-10 0.00095525 0.00061669 0.00078809 v omega 12.302 1.0313e+05 2664.5 497.42 v TempK 288 342.12 294.3 291.22 v Density 1.205 1.205 1.205 1.205 v TurbVisc 6.09e-15 9.3579e-05 5.5011e-05 7.2053e-05 v CourantNb 3.1407e-09 0.00018955 1.3846e-05 8.8696e-06 v FourierNb 0.088141 0.6281 0.18326 0.15407 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9589 4.959 0.00056388 -5.8197e-07 v volume_forces[Z] -4.9589 4.959 -0.00056378 6.8932e-07 v ǁvolume_forcesǁ 1.3857e-08 4.96 0.57015 0.28861 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.51 291.36 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014768 5.2239e-05 2.9126e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.088159 0.6281 0.18328 0.15408 INSTANT 0.855144000E+00 TIME STEP NUMBER 888 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.65288E-05 0.22192E-02 Friction velocity uk : 0.65291E-05 0.22192E-02 Dimensionless distance yplus : 0.43477E-04 0.14764E-01 Friction thermal sca. tstar : -0.27816E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.30535E-04 0.10370E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.65288E-05 0.22192E-02 Friction velocity uk : 0.65291E-05 0.22192E-02 Dimensionless distance yplus : 0.43477E-04 0.14764E-01 Friction thermal sca. tstar : -0.27816E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.30535E-04 0.10370E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.38238E-08 3 0.93256E-07 0.17005E-12 0.81638E+00 c Velocity[X] 0.39867E-32 c Velocity[Y] 0.85023E-13 c Velocity[Z] 0.85030E-13 c Pressure 0.67351E-14 17 0.52297E-07 0.52297E-07 0.88767E+00 c k 0.28457E-06 2 0.29183E-07 0.10276E-08 0.12369E+01 c omega 0.13153E+02 1 0.84076E-09 0.12499E+00 0.18405E-02 c TempK 0.94765E+02 1 0.72518E-07 0.16228E-01 0.14089E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.805e-14 7.3753e-14 -9.1782e-18 -2.3967e-18 v Velocity[Y] -0.00012117 0.00011428 -3.6563e-10 -3.1575e-12 v Velocity[Z] -0.00011421 0.00012118 7.802e-11 -1.5447e-12 v ǁVelocityǁ 3.7526e-10 0.00012987 1.1503e-05 8.5153e-06 v Pressure -0.0014947 0.02395 0.001378 7.6775e-20 v k 5.1808e-10 0.00095423 0.00061591 0.00078713 v omega 12.29 1.0313e+05 2664.5 497.41 v TempK 288 342.12 294.3 291.22 v Density 1.205 1.205 1.205 1.205 v TurbVisc 6.0717e-15 9.3569e-05 5.4994e-05 7.2034e-05 v CourantNb 3.143e-09 0.00018948 1.3847e-05 8.873e-06 v FourierNb 0.088079 0.6281 0.18323 0.15404 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.959 4.959 0.00056407 -5.8221e-07 v volume_forces[Z] -4.959 4.959 -0.00056397 6.8958e-07 v ǁvolume_forcesǁ 1.3711e-08 4.96 0.57034 0.28877 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.51 291.36 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014764 5.2228e-05 2.9119e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.088097 0.6281 0.18325 0.15405 INSTANT 0.856107000E+00 TIME STEP NUMBER 889 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.64642E-05 0.22187E-02 Friction velocity uk : 0.64645E-05 0.22187E-02 Dimensionless distance yplus : 0.43047E-04 0.14761E-01 Friction thermal sca. tstar : -0.26697E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.30233E-04 0.10367E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.64642E-05 0.22187E-02 Friction velocity uk : 0.64645E-05 0.22187E-02 Dimensionless distance yplus : 0.43047E-04 0.14761E-01 Friction thermal sca. tstar : -0.26697E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.30233E-04 0.10367E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.38253E-08 3 0.93061E-07 0.16967E-12 0.81533E+00 c Velocity[X] 0.39728E-32 c Velocity[Y] 0.84831E-13 c Velocity[Z] 0.84838E-13 c Pressure 0.67262E-14 16 0.52227E-07 0.52227E-07 0.88662E+00 c k 0.28424E-06 2 0.29138E-07 0.10232E-08 0.12358E+01 c omega 0.13153E+02 1 0.83873E-09 0.12449E+00 0.18369E-02 c TempK 0.94765E+02 1 0.72402E-07 0.16200E-01 0.14077E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.8004e-14 7.3717e-14 -9.1739e-18 -2.3957e-18 v Velocity[Y] -0.00012115 0.00011425 -3.6315e-10 -3.1681e-12 v Velocity[Z] -0.00011418 0.00012115 7.5474e-11 -1.5545e-12 v ǁVelocityǁ 3.7126e-10 0.00012985 1.1507e-05 8.521e-06 v Pressure -0.0014963 0.023963 0.0013789 3.6672e-20 v k 5.1652e-10 0.00095321 0.00061514 0.00078618 v omega 12.278 1.0313e+05 2664.5 497.4 v TempK 288 342.12 294.3 291.22 v Density 1.205 1.205 1.205 1.205 v TurbVisc 6.0534e-15 9.356e-05 5.4978e-05 7.2014e-05 v CourantNb 3.1451e-09 0.00018942 1.3847e-05 8.8764e-06 v FourierNb 0.088016 0.6281 0.1832 0.154 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.959 4.959 0.00056426 -5.8245e-07 v volume_forces[Z] -4.959 4.959 -0.00056416 6.8984e-07 v ǁvolume_forcesǁ 1.3566e-08 4.9601 0.57052 0.28893 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.51 291.36 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014761 5.2217e-05 2.9112e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.088035 0.6281 0.18321 0.15401 INSTANT 0.857070000E+00 TIME STEP NUMBER 890 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.63987E-05 0.22182E-02 Friction velocity uk : 0.63990E-05 0.22182E-02 Dimensionless distance yplus : 0.42610E-04 0.14758E-01 Friction thermal sca. tstar : -0.25710E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.29927E-04 0.10365E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.63987E-05 0.22182E-02 Friction velocity uk : 0.63990E-05 0.22182E-02 Dimensionless distance yplus : 0.42610E-04 0.14758E-01 Friction thermal sca. tstar : -0.25710E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.29927E-04 0.10365E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.38267E-08 3 0.92860E-07 0.16929E-12 0.81429E+00 c Velocity[X] 0.39590E-32 c Velocity[Y] 0.84639E-13 c Velocity[Z] 0.84646E-13 c Pressure 0.67108E-14 16 0.52107E-07 0.52107E-07 0.88558E+00 c k 0.28390E-06 2 0.29093E-07 0.10189E-08 0.12346E+01 c omega 0.13153E+02 1 0.83670E-09 0.12400E+00 0.18332E-02 c TempK 0.94766E+02 1 0.72286E-07 0.16173E-01 0.14065E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.7958e-14 7.368e-14 -9.1695e-18 -2.3947e-18 v Velocity[Y] -0.00012113 0.00011423 -3.6067e-10 -3.165e-12 v Velocity[Z] -0.00011416 0.00012113 7.294e-11 -1.5541e-12 v ǁVelocityǁ 3.6731e-10 0.00012983 1.151e-05 8.5267e-06 v Pressure -0.001498 0.023976 0.0013798 3.275e-20 v k 5.1497e-10 0.00095219 0.00061437 0.00078523 v omega 12.266 1.0313e+05 2664.5 497.39 v TempK 288 342.12 294.3 291.22 v Density 1.205 1.205 1.205 1.205 v TurbVisc 6.0352e-15 9.355e-05 5.4962e-05 7.1995e-05 v CourantNb 3.1473e-09 0.00018936 1.3848e-05 8.8798e-06 v FourierNb 0.087954 0.6281 0.18317 0.15397 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9591 4.9591 0.00056445 -5.8269e-07 v volume_forces[Z] -4.9591 4.9591 -0.00056435 6.901e-07 v ǁvolume_forcesǁ 1.3421e-08 4.9601 0.57071 0.28909 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.51 291.36 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014758 5.2205e-05 2.9106e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.087973 0.6281 0.18318 0.15398 INSTANT 0.858033000E+00 TIME STEP NUMBER 891 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.63325E-05 0.22177E-02 Friction velocity uk : 0.63328E-05 0.22177E-02 Dimensionless distance yplus : 0.42170E-04 0.14755E-01 Friction thermal sca. tstar : -0.24831E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.29617E-04 0.10363E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.63325E-05 0.22177E-02 Friction velocity uk : 0.63328E-05 0.22177E-02 Dimensionless distance yplus : 0.42170E-04 0.14755E-01 Friction thermal sca. tstar : -0.24831E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.29617E-04 0.10363E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.38282E-08 3 0.92667E-07 0.16890E-12 0.81324E+00 c Velocity[X] 0.39452E-32 c Velocity[Y] 0.84447E-13 c Velocity[Z] 0.84455E-13 c Pressure 0.67031E-14 16 0.52046E-07 0.52046E-07 0.88454E+00 c k 0.28357E-06 2 0.29049E-07 0.10146E-08 0.12334E+01 c omega 0.13153E+02 1 0.83468E-09 0.12350E+00 0.18296E-02 c TempK 0.94766E+02 1 0.72171E-07 0.16146E-01 0.14053E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.7912e-14 7.3643e-14 -9.1651e-18 -2.3936e-18 v Velocity[Y] -0.00012111 0.0001142 -3.5818e-10 -3.1613e-12 v Velocity[Z] -0.00011413 0.00012111 7.0405e-11 -1.5545e-12 v ǁVelocityǁ 3.6339e-10 0.0001298 1.1514e-05 8.5324e-06 v Pressure -0.0014996 0.023989 0.0013807 1.765e-21 v k 5.1343e-10 0.00095117 0.0006136 0.00078428 v omega 12.254 1.0313e+05 2664.5 497.38 v TempK 288 342.12 294.31 291.23 v Density 1.205 1.205 1.205 1.205 v TurbVisc 6.0171e-15 9.354e-05 5.4946e-05 7.1976e-05 v CourantNb 3.1496e-09 0.0001893 1.3848e-05 8.8831e-06 v FourierNb 0.087893 0.6281 0.18314 0.15394 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9591 4.9591 0.00056464 -5.8293e-07 v volume_forces[Z] -4.9591 4.9591 -0.00056454 6.9036e-07 v ǁvolume_forcesǁ 1.3278e-08 4.9601 0.5709 0.28925 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.51 291.37 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014755 5.2194e-05 2.9099e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.087911 0.6281 0.18315 0.15395 INSTANT 0.858996000E+00 TIME STEP NUMBER 892 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.62656E-05 0.22172E-02 Friction velocity uk : 0.62659E-05 0.22172E-02 Dimensionless distance yplus : 0.41724E-04 0.14751E-01 Friction thermal sca. tstar : -0.24043E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.29304E-04 0.10360E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.62656E-05 0.22172E-02 Friction velocity uk : 0.62659E-05 0.22172E-02 Dimensionless distance yplus : 0.41724E-04 0.14751E-01 Friction thermal sca. tstar : -0.24043E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.29304E-04 0.10360E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.38297E-08 3 0.92505E-07 0.16852E-12 0.81219E+00 c Velocity[X] 0.39315E-32 c Velocity[Y] 0.84256E-13 c Velocity[Z] 0.84263E-13 c Pressure 0.66911E-14 16 0.51953E-07 0.51953E-07 0.88350E+00 c k 0.28324E-06 2 0.29005E-07 0.10103E-08 0.12323E+01 c omega 0.13153E+02 1 0.83266E-09 0.12301E+00 0.18259E-02 c TempK 0.94767E+02 1 0.72056E-07 0.16119E-01 0.14041E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.7866e-14 7.3607e-14 -9.1607e-18 -2.3926e-18 v Velocity[Y] -0.00012108 0.00011418 -3.5569e-10 -3.1578e-12 v Velocity[Z] -0.00011411 0.00012109 6.7871e-11 -1.5547e-12 v ǁVelocityǁ 3.5951e-10 0.00012978 1.1517e-05 8.5381e-06 v Pressure -0.0015013 0.024002 0.0013816 -1.3747e-19 v k 5.1189e-10 0.00095016 0.00061284 0.00078333 v omega 12.243 1.0313e+05 2664.5 497.37 v TempK 288 342.12 294.31 291.23 v Density 1.205 1.205 1.205 1.205 v TurbVisc 5.999e-15 9.3531e-05 5.4929e-05 7.1956e-05 v CourantNb 3.1518e-09 0.00018924 1.3849e-05 8.8865e-06 v FourierNb 0.087831 0.6281 0.18311 0.1539 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9592 4.9592 0.00056483 -5.8317e-07 v volume_forces[Z] -4.9592 4.9592 -0.00056473 6.9062e-07 v ǁvolume_forcesǁ 1.3137e-08 4.9602 0.57108 0.28941 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.52 291.37 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014751 5.2183e-05 2.9092e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.087849 0.6281 0.18312 0.15391 INSTANT 0.859959000E+00 TIME STEP NUMBER 893 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.61977E-05 0.22167E-02 Friction velocity uk : 0.61980E-05 0.22167E-02 Dimensionless distance yplus : 0.41272E-04 0.14748E-01 Friction thermal sca. tstar : -0.23329E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.28987E-04 0.10358E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.61977E-05 0.22167E-02 Friction velocity uk : 0.61980E-05 0.22167E-02 Dimensionless distance yplus : 0.41272E-04 0.14748E-01 Friction thermal sca. tstar : -0.23329E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.28987E-04 0.10358E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.38311E-08 3 0.92282E-07 0.16814E-12 0.81114E+00 c Velocity[X] 0.39180E-32 c Velocity[Y] 0.84064E-13 c Velocity[Z] 0.84072E-13 c Pressure 0.66817E-14 16 0.51879E-07 0.51879E-07 0.88246E+00 c k 0.28291E-06 2 0.28960E-07 0.10061E-08 0.12311E+01 c omega 0.13153E+02 1 0.83065E-09 0.12252E+00 0.18223E-02 c TempK 0.94767E+02 1 0.71941E-07 0.16091E-01 0.14029E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.782e-14 7.357e-14 -9.1564e-18 -2.3916e-18 v Velocity[Y] -0.00012106 0.00011415 -3.532e-10 -3.1544e-12 v Velocity[Z] -0.00011408 0.00012107 6.5337e-11 -1.5548e-12 v ǁVelocityǁ 3.5567e-10 0.00012975 1.1521e-05 8.5437e-06 v Pressure -0.0015029 0.024015 0.0013825 1.9611e-20 v k 5.1036e-10 0.00094915 0.00061207 0.00078238 v omega 12.231 1.0313e+05 2664.5 497.36 v TempK 288 342.12 294.31 291.23 v Density 1.205 1.205 1.205 1.205 v TurbVisc 5.9811e-15 9.3521e-05 5.4913e-05 7.1937e-05 v CourantNb 3.154e-09 0.00018917 1.385e-05 8.8899e-06 v FourierNb 0.087769 0.6281 0.18307 0.15387 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9592 4.9592 0.00056501 -5.8341e-07 v volume_forces[Z] -4.9592 4.9592 -0.00056492 6.9088e-07 v ǁvolume_forcesǁ 1.2996e-08 4.9602 0.57127 0.28957 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.52 291.37 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014748 5.2172e-05 2.9085e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.087788 0.6281 0.18309 0.15388 INSTANT 0.860922000E+00 TIME STEP NUMBER 894 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.61289E-05 0.22162E-02 Friction velocity uk : 0.61292E-05 0.22162E-02 Dimensionless distance yplus : 0.40814E-04 0.14745E-01 Friction thermal sca. tstar : -0.22681E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.28665E-04 0.10356E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.61289E-05 0.22162E-02 Friction velocity uk : 0.61292E-05 0.22162E-02 Dimensionless distance yplus : 0.40814E-04 0.14745E-01 Friction thermal sca. tstar : -0.22681E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.28665E-04 0.10356E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.38326E-08 3 0.92085E-07 0.16775E-12 0.81009E+00 c Velocity[X] 0.39043E-32 c Velocity[Y] 0.83873E-13 c Velocity[Z] 0.83881E-13 c Pressure 0.66675E-14 16 0.51768E-07 0.51768E-07 0.88142E+00 c k 0.28258E-06 2 0.28916E-07 0.10018E-08 0.12300E+01 c omega 0.13153E+02 1 0.82865E-09 0.12204E+00 0.18187E-02 c TempK 0.94768E+02 1 0.71827E-07 0.16064E-01 0.14018E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.7774e-14 7.3534e-14 -9.152e-18 -2.3906e-18 v Velocity[Y] -0.00012104 0.00011413 -3.5071e-10 -3.1509e-12 v Velocity[Z] -0.00011406 0.00012105 6.2804e-11 -1.5549e-12 v ǁVelocityǁ 3.5187e-10 0.00012973 1.1525e-05 8.5494e-06 v Pressure -0.0015046 0.024028 0.0013834 -1.913e-19 v k 5.0883e-10 0.00094814 0.00061131 0.00078144 v omega 12.219 1.0313e+05 2664.5 497.35 v TempK 288 342.12 294.31 291.23 v Density 1.205 1.205 1.205 1.205 v TurbVisc 5.9632e-15 9.3511e-05 5.4897e-05 7.1918e-05 v CourantNb 3.1563e-09 0.00018911 1.385e-05 8.8932e-06 v FourierNb 0.087708 0.6281 0.18304 0.15384 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9592 4.9593 0.0005652 -5.8364e-07 v volume_forces[Z] -4.9592 4.9593 -0.00056511 6.9114e-07 v ǁvolume_forcesǁ 1.2858e-08 4.9603 0.57146 0.28974 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.52 291.37 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014745 5.2161e-05 2.9079e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.087726 0.6281 0.18306 0.15385 INSTANT 0.861885000E+00 TIME STEP NUMBER 895 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.60592E-05 0.22157E-02 Friction velocity uk : 0.60595E-05 0.22157E-02 Dimensionless distance yplus : 0.40350E-04 0.14741E-01 Friction thermal sca. tstar : -0.22088E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.28339E-04 0.10353E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.60592E-05 0.22157E-02 Friction velocity uk : 0.60595E-05 0.22157E-02 Dimensionless distance yplus : 0.40350E-04 0.14741E-01 Friction thermal sca. tstar : -0.22088E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.28339E-04 0.10353E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.38341E-08 3 0.91895E-07 0.16737E-12 0.80905E+00 c Velocity[X] 0.38908E-32 c Velocity[Y] 0.83682E-13 c Velocity[Z] 0.83690E-13 c Pressure 0.66613E-14 16 0.51720E-07 0.51720E-07 0.88039E+00 c k 0.28225E-06 2 0.28872E-07 0.99761E-09 0.12288E+01 c omega 0.13153E+02 1 0.82666E-09 0.12156E+00 0.18151E-02 c TempK 0.94768E+02 1 0.71713E-07 0.16037E-01 0.14006E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.7728e-14 7.3497e-14 -9.1477e-18 -2.3896e-18 v Velocity[Y] -0.00012102 0.0001141 -3.4822e-10 -3.1476e-12 v Velocity[Z] -0.00011403 0.00012102 6.0271e-11 -1.5549e-12 v ǁVelocityǁ 3.4811e-10 0.00012971 1.1528e-05 8.5551e-06 v Pressure -0.0015063 0.024041 0.0013843 -2.4121e-20 v k 5.0731e-10 0.00094713 0.00061055 0.0007805 v omega 12.207 1.0313e+05 2664.5 497.34 v TempK 288 342.12 294.32 291.23 v Density 1.205 1.205 1.205 1.205 v TurbVisc 5.9453e-15 9.3502e-05 5.4881e-05 7.1898e-05 v CourantNb 3.1585e-09 0.00018905 1.3851e-05 8.8966e-06 v FourierNb 0.087647 0.6281 0.18301 0.15381 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9593 4.9593 0.00056539 -5.8388e-07 v volume_forces[Z] -4.9593 4.9593 -0.00056529 6.9139e-07 v ǁvolume_forcesǁ 1.272e-08 4.9603 0.57164 0.2899 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.52 291.37 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014741 5.2149e-05 2.9072e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.087665 0.6281 0.18303 0.15382 INSTANT 0.862848000E+00 TIME STEP NUMBER 896 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.59885E-05 0.22152E-02 Friction velocity uk : 0.59888E-05 0.22152E-02 Dimensionless distance yplus : 0.39879E-04 0.14738E-01 Friction thermal sca. tstar : -0.21543E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.28008E-04 0.10351E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.59885E-05 0.22152E-02 Friction velocity uk : 0.59888E-05 0.22152E-02 Dimensionless distance yplus : 0.39879E-04 0.14738E-01 Friction thermal sca. tstar : -0.21543E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.28008E-04 0.10351E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.38355E-08 3 0.91719E-07 0.16699E-12 0.80800E+00 c Velocity[X] 0.38773E-32 c Velocity[Y] 0.83492E-13 c Velocity[Z] 0.83500E-13 c Pressure 0.66774E-14 16 0.51843E-07 0.51843E-07 0.87936E+00 c k 0.28193E-06 2 0.28828E-07 0.99341E-09 0.12277E+01 c omega 0.13153E+02 1 0.82467E-09 0.12108E+00 0.18115E-02 c TempK 0.94769E+02 1 0.71599E-07 0.16011E-01 0.13994E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.7682e-14 7.3461e-14 -9.1433e-18 -2.3885e-18 v Velocity[Y] -0.000121 0.00011408 -3.4565e-10 -3.0629e-12 v Velocity[Z] -0.00011401 0.000121 5.7919e-11 -1.3832e-12 v ǁVelocityǁ 3.4445e-10 0.00012968 1.1532e-05 8.5607e-06 v Pressure -0.0015079 0.024054 0.0013852 3.9809e-20 v k 5.058e-10 0.00094613 0.00060979 0.00077956 v omega 12.196 1.0313e+05 2664.4 497.32 v TempK 288 342.13 294.32 291.24 v Density 1.205 1.205 1.205 1.205 v TurbVisc 5.9276e-15 9.3492e-05 5.4865e-05 7.1879e-05 v CourantNb 3.1607e-09 0.00018899 1.3851e-05 8.9e-06 v FourierNb 0.087586 0.6281 0.18298 0.15377 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9593 4.9593 0.00056558 -5.8412e-07 v volume_forces[Z] -4.9593 4.9593 -0.00056548 6.9165e-07 v ǁvolume_forcesǁ 1.2584e-08 4.9603 0.57183 0.29006 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.52 291.38 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014738 5.2138e-05 2.9065e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.087604 0.6281 0.18299 0.15378 INSTANT 0.863811000E+00 TIME STEP NUMBER 897 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.59179E-05 0.22147E-02 Friction velocity uk : 0.59182E-05 0.22147E-02 Dimensionless distance yplus : 0.39409E-04 0.14735E-01 Friction thermal sca. tstar : -0.21041E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.27678E-04 0.10349E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.59179E-05 0.22147E-02 Friction velocity uk : 0.59182E-05 0.22147E-02 Dimensionless distance yplus : 0.39409E-04 0.14735E-01 Friction thermal sca. tstar : -0.21041E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.27678E-04 0.10349E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.38370E-08 3 0.91499E-07 0.16661E-12 0.80695E+00 c Velocity[X] 0.38639E-32 c Velocity[Y] 0.83301E-13 c Velocity[Z] 0.83309E-13 c Pressure 0.66344E-14 16 0.51510E-07 0.51510E-07 0.87833E+00 c k 0.28160E-06 2 0.28785E-07 0.98924E-09 0.12265E+01 c omega 0.13153E+02 1 0.82268E-09 0.12060E+00 0.18079E-02 c TempK 0.94769E+02 1 0.71485E-07 0.15984E-01 0.13982E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.7637e-14 7.3425e-14 -9.139e-18 -2.3875e-18 v Velocity[Y] -0.00012097 0.00011406 -3.4315e-10 -3.0527e-12 v Velocity[Z] -0.00011398 0.00012098 5.5383e-11 -1.3856e-12 v ǁVelocityǁ 3.4076e-10 0.00012966 1.1535e-05 8.5663e-06 v Pressure -0.0015096 0.024067 0.0013861 2.9122e-20 v k 5.0429e-10 0.00094512 0.00060903 0.00077862 v omega 12.184 1.0313e+05 2664.4 497.31 v TempK 288 342.13 294.32 291.24 v Density 1.205 1.205 1.205 1.205 v TurbVisc 5.9099e-15 9.3482e-05 5.4848e-05 7.186e-05 v CourantNb 3.1629e-09 0.00018893 1.3852e-05 8.9033e-06 v FourierNb 0.087525 0.6281 0.18295 0.15374 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9594 4.9594 0.00056577 -5.8435e-07 v volume_forces[Z] -4.9594 4.9594 -0.00056567 6.9191e-07 v ǁvolume_forcesǁ 1.2452e-08 4.9604 0.57201 0.29022 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.53 291.38 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014735 5.2127e-05 2.9059e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.087543 0.6281 0.18296 0.15375 INSTANT 0.864774000E+00 TIME STEP NUMBER 898 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.58449E-05 0.22143E-02 Friction velocity uk : 0.58452E-05 0.22142E-02 Dimensionless distance yplus : 0.38922E-04 0.14732E-01 Friction thermal sca. tstar : -0.20576E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.27337E-04 0.10347E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.58449E-05 0.22143E-02 Friction velocity uk : 0.58452E-05 0.22142E-02 Dimensionless distance yplus : 0.38922E-04 0.14732E-01 Friction thermal sca. tstar : -0.20576E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.27337E-04 0.10347E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.38384E-08 3 0.91318E-07 0.16623E-12 0.80590E+00 c Velocity[X] 0.38505E-32 c Velocity[Y] 0.83110E-13 c Velocity[Z] 0.83118E-13 c Pressure 0.66233E-14 16 0.51422E-07 0.51422E-07 0.87731E+00 c k 0.28127E-06 2 0.28741E-07 0.98509E-09 0.12254E+01 c omega 0.13153E+02 1 0.82071E-09 0.12012E+00 0.18043E-02 c TempK 0.94770E+02 1 0.71372E-07 0.15957E-01 0.13970E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.7591e-14 7.3389e-14 -9.1346e-18 -2.3865e-18 v Velocity[Y] -0.00012095 0.00011403 -3.4066e-10 -3.0529e-12 v Velocity[Z] -0.00011396 0.00012096 5.2851e-11 -1.3849e-12 v ǁVelocityǁ 3.3712e-10 0.00012963 1.1539e-05 8.572e-06 v Pressure -0.0015112 0.02408 0.001387 2.1179e-20 v k 5.0279e-10 0.00094412 0.00060828 0.00077768 v omega 12.172 1.0313e+05 2664.4 497.3 v TempK 288 342.13 294.32 291.24 v Density 1.205 1.205 1.205 1.205 v TurbVisc 5.8923e-15 9.3473e-05 5.4832e-05 7.1841e-05 v CourantNb 3.1651e-09 0.00018887 1.3853e-05 8.9067e-06 v FourierNb 0.087464 0.6281 0.18292 0.15371 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9594 4.9594 0.00056595 -5.8458e-07 v volume_forces[Z] -4.9594 4.9594 -0.00056586 6.9216e-07 v ǁvolume_forcesǁ 1.2319e-08 4.9604 0.5722 0.29038 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.53 291.38 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014732 5.2116e-05 2.9052e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.087482 0.6281 0.18293 0.15372 INSTANT 0.865737000E+00 TIME STEP NUMBER 899 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.57708E-05 0.22138E-02 Friction velocity uk : 0.57711E-05 0.22137E-02 Dimensionless distance yplus : 0.38429E-04 0.14728E-01 Friction thermal sca. tstar : -0.20143E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.26990E-04 0.10344E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.57708E-05 0.22138E-02 Friction velocity uk : 0.57711E-05 0.22137E-02 Dimensionless distance yplus : 0.38429E-04 0.14728E-01 Friction thermal sca. tstar : -0.20143E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.26990E-04 0.10344E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.38399E-08 3 0.91130E-07 0.16585E-12 0.80485E+00 c Velocity[X] 0.38374E-32 c Velocity[Y] 0.82920E-13 c Velocity[Z] 0.82928E-13 c Pressure 0.66125E-14 16 0.51338E-07 0.51338E-07 0.87628E+00 c k 0.28095E-06 2 0.28697E-07 0.98097E-09 0.12242E+01 c omega 0.13153E+02 1 0.81874E-09 0.11965E+00 0.18008E-02 c TempK 0.94770E+02 1 0.71259E-07 0.15930E-01 0.13958E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.7546e-14 7.3352e-14 -9.1303e-18 -2.3855e-18 v Velocity[Y] -0.00012093 0.00011401 -3.3817e-10 -3.0495e-12 v Velocity[Z] -0.00011394 0.00012094 5.0319e-11 -1.3848e-12 v ǁVelocityǁ 3.3354e-10 0.00012961 1.1543e-05 8.5776e-06 v Pressure -0.0015129 0.024093 0.0013878 3.3534e-20 v k 5.0129e-10 0.00094312 0.00060752 0.00077675 v omega 12.161 1.0313e+05 2664.4 497.29 v TempK 288 342.13 294.32 291.24 v Density 1.205 1.205 1.205 1.205 v TurbVisc 5.8747e-15 9.3463e-05 5.4816e-05 7.1821e-05 v CourantNb 3.1673e-09 0.00018881 1.3853e-05 8.91e-06 v FourierNb 0.087404 0.6281 0.18289 0.15368 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9594 4.9595 0.00056614 -5.8482e-07 v volume_forces[Z] -4.9594 4.9595 -0.00056604 6.9242e-07 v ǁvolume_forcesǁ 1.2187e-08 4.9605 0.57239 0.29054 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.53 291.38 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014728 5.2105e-05 2.9045e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.087422 0.6281 0.1829 0.15368 INSTANT 0.866700000E+00 TIME STEP NUMBER 900 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.56956E-05 0.22133E-02 Friction velocity uk : 0.56960E-05 0.22132E-02 Dimensionless distance yplus : 0.37929E-04 0.14725E-01 Friction thermal sca. tstar : -0.19740E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.26639E-04 0.10342E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.56956E-05 0.22133E-02 Friction velocity uk : 0.56960E-05 0.22132E-02 Dimensionless distance yplus : 0.37929E-04 0.14725E-01 Friction thermal sca. tstar : -0.19740E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.26639E-04 0.10342E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.38414E-08 3 0.90939E-07 0.16547E-12 0.80381E+00 c Velocity[X] 0.38243E-32 c Velocity[Y] 0.82730E-13 c Velocity[Z] 0.82738E-13 c Pressure 0.66016E-14 16 0.51253E-07 0.51253E-07 0.87526E+00 c k 0.28062E-06 2 0.28654E-07 0.97686E-09 0.12231E+01 c omega 0.13153E+02 1 0.81678E-09 0.11918E+00 0.17972E-02 c TempK 0.94771E+02 1 0.71147E-07 0.15904E-01 0.13947E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.75e-14 7.3316e-14 -9.126e-18 -2.3845e-18 v Velocity[Y] -0.00012091 0.00011398 -3.3567e-10 -3.0462e-12 v Velocity[Z] -0.00011391 0.00012091 4.7787e-11 -1.385e-12 v ǁVelocityǁ 3.3002e-10 0.00012959 1.1546e-05 8.5832e-06 v Pressure -0.0015145 0.024106 0.0013887 1.5296e-20 v k 4.9981e-10 0.00094212 0.00060677 0.00077582 v omega 12.149 1.0313e+05 2664.4 497.28 v TempK 288 342.13 294.33 291.24 v Density 1.205 1.205 1.205 1.205 v TurbVisc 5.8573e-15 9.3454e-05 5.48e-05 7.1802e-05 v CourantNb 3.1695e-09 0.00018875 1.3854e-05 8.9134e-06 v FourierNb 0.087343 0.6281 0.18286 0.15364 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9595 4.9595 0.00056633 -5.8505e-07 v volume_forces[Z] -4.9595 4.9595 -0.00056623 6.9267e-07 v ǁvolume_forcesǁ 1.2058e-08 4.9605 0.57257 0.2907 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.53 291.38 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014725 5.2093e-05 2.9039e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.087361 0.6281 0.18287 0.15365 INSTANT 0.867663000E+00 TIME STEP NUMBER 901 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.56194E-05 0.22128E-02 Friction velocity uk : 0.56198E-05 0.22128E-02 Dimensionless distance yplus : 0.37421E-04 0.14722E-01 Friction thermal sca. tstar : -0.19363E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.26282E-04 0.10340E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.56194E-05 0.22128E-02 Friction velocity uk : 0.56198E-05 0.22128E-02 Dimensionless distance yplus : 0.37421E-04 0.14722E-01 Friction thermal sca. tstar : -0.19363E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.26282E-04 0.10340E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.38428E-08 3 0.90749E-07 0.16509E-12 0.80276E+00 c Velocity[X] 0.38111E-32 c Velocity[Y] 0.82540E-13 c Velocity[Z] 0.82548E-13 c Pressure 0.65930E-14 16 0.51186E-07 0.51186E-07 0.87424E+00 c k 0.28030E-06 2 0.28611E-07 0.97278E-09 0.12219E+01 c omega 0.13153E+02 1 0.81482E-09 0.11871E+00 0.17937E-02 c TempK 0.94772E+02 1 0.71034E-07 0.15877E-01 0.13935E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.7455e-14 7.328e-14 -9.1217e-18 -2.3835e-18 v Velocity[Y] -0.00012089 0.00011396 -3.3318e-10 -3.0429e-12 v Velocity[Z] -0.00011389 0.00012089 4.5255e-11 -1.3851e-12 v ǁVelocityǁ 3.2655e-10 0.00012956 1.155e-05 8.5889e-06 v Pressure -0.0015162 0.024119 0.0013896 7.2363e-20 v k 4.9832e-10 0.00094113 0.00060602 0.00077489 v omega 12.137 1.0313e+05 2664.4 497.27 v TempK 288 342.13 294.33 291.24 v Density 1.205 1.205 1.205 1.205 v TurbVisc 5.8399e-15 9.3444e-05 5.4784e-05 7.1783e-05 v CourantNb 3.1717e-09 0.00018869 1.3854e-05 8.9167e-06 v FourierNb 0.087283 0.6281 0.18283 0.15361 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9595 4.9595 0.00056651 -5.8529e-07 v volume_forces[Z] -4.9595 4.9595 -0.00056642 6.9293e-07 v ǁvolume_forcesǁ 1.193e-08 4.9605 0.57276 0.29086 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.53 291.38 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014722 5.2082e-05 2.9032e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.087301 0.6281 0.18284 0.15362 INSTANT 0.868626000E+00 TIME STEP NUMBER 902 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.55420E-05 0.22123E-02 Friction velocity uk : 0.55423E-05 0.22123E-02 Dimensionless distance yplus : 0.36906E-04 0.14719E-01 Friction thermal sca. tstar : -0.19009E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.25920E-04 0.10337E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.55420E-05 0.22123E-02 Friction velocity uk : 0.55423E-05 0.22123E-02 Dimensionless distance yplus : 0.36906E-04 0.14719E-01 Friction thermal sca. tstar : -0.19009E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.25920E-04 0.10337E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.38443E-08 3 0.90559E-07 0.16471E-12 0.80171E+00 c Velocity[X] 0.37980E-32 c Velocity[Y] 0.82350E-13 c Velocity[Z] 0.82358E-13 c Pressure 0.65800E-14 16 0.51084E-07 0.51084E-07 0.87323E+00 c k 0.27997E-06 2 0.28567E-07 0.96871E-09 0.12208E+01 c omega 0.13153E+02 1 0.81287E-09 0.11824E+00 0.17902E-02 c TempK 0.94772E+02 1 0.70922E-07 0.15851E-01 0.13923E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.741e-14 7.3244e-14 -9.1174e-18 -2.3825e-18 v Velocity[Y] -0.00012087 0.00011394 -3.3069e-10 -3.0396e-12 v Velocity[Z] -0.00011386 0.00012087 4.2724e-11 -1.3852e-12 v ǁVelocityǁ 3.2313e-10 0.00012954 1.1553e-05 8.5945e-06 v Pressure -0.0015178 0.024132 0.0013905 -8.0207e-20 v k 4.9684e-10 0.00094013 0.00060527 0.00077396 v omega 12.126 1.0313e+05 2664.4 497.26 v TempK 288 342.13 294.33 291.25 v Density 1.205 1.205 1.205 1.205 v TurbVisc 5.8225e-15 9.3434e-05 5.4768e-05 7.1764e-05 v CourantNb 3.1739e-09 0.00018863 1.3855e-05 8.9201e-06 v FourierNb 0.087223 0.6281 0.18279 0.15358 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9596 4.9596 0.0005667 -5.8552e-07 v volume_forces[Z] -4.9596 4.9596 -0.00056661 6.9318e-07 v ǁvolume_forcesǁ 1.1805e-08 4.9606 0.57294 0.29102 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.54 291.39 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014719 5.2071e-05 2.9025e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.087241 0.6281 0.18281 0.15359 INSTANT 0.869589000E+00 TIME STEP NUMBER 903 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.54633E-05 0.22118E-02 Friction velocity uk : 0.54636E-05 0.22118E-02 Dimensionless distance yplus : 0.36382E-04 0.14715E-01 Friction thermal sca. tstar : -0.18677E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.25552E-04 0.10335E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.54633E-05 0.22118E-02 Friction velocity uk : 0.54636E-05 0.22118E-02 Dimensionless distance yplus : 0.36382E-04 0.14715E-01 Friction thermal sca. tstar : -0.18677E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.25552E-04 0.10335E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.38457E-08 3 0.90371E-07 0.16433E-12 0.80066E+00 c Velocity[X] 0.37850E-32 c Velocity[Y] 0.82160E-13 c Velocity[Z] 0.82169E-13 c Pressure 0.65694E-14 16 0.51001E-07 0.51001E-07 0.87221E+00 c k 0.27965E-06 2 0.28524E-07 0.96467E-09 0.12197E+01 c omega 0.13153E+02 1 0.81093E-09 0.11777E+00 0.17866E-02 c TempK 0.94773E+02 1 0.70811E-07 0.15825E-01 0.13912E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.7365e-14 7.3209e-14 -9.1131e-18 -2.3815e-18 v Velocity[Y] -0.00012084 0.00011391 -3.2819e-10 -3.0363e-12 v Velocity[Z] -0.00011384 0.00012085 4.0194e-11 -1.3853e-12 v ǁVelocityǁ 3.1978e-10 0.00012951 1.1557e-05 8.6001e-06 v Pressure -0.0015195 0.024145 0.0013914 9.0209e-20 v k 4.9537e-10 0.00093914 0.00060452 0.00077303 v omega 12.114 1.0313e+05 2664.4 497.25 v TempK 288 342.13 294.33 291.25 v Density 1.205 1.205 1.205 1.205 v TurbVisc 5.8053e-15 9.3425e-05 5.4752e-05 7.1745e-05 v CourantNb 3.1761e-09 0.00018856 1.3855e-05 8.9234e-06 v FourierNb 0.087163 0.6281 0.18276 0.15355 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9596 4.9596 0.00056689 -5.8576e-07 v volume_forces[Z] -4.9596 4.9596 -0.00056679 6.9344e-07 v ǁvolume_forcesǁ 1.1681e-08 4.9606 0.57313 0.29118 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.54 291.39 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014715 5.206e-05 2.9019e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.087181 0.6281 0.18278 0.15355 INSTANT 0.870552000E+00 TIME STEP NUMBER 904 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.53832E-05 0.22113E-02 Friction velocity uk : 0.53836E-05 0.22113E-02 Dimensionless distance yplus : 0.35849E-04 0.14712E-01 Friction thermal sca. tstar : -0.18365E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.25178E-04 0.10333E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.53832E-05 0.22113E-02 Friction velocity uk : 0.53836E-05 0.22113E-02 Dimensionless distance yplus : 0.35849E-04 0.14712E-01 Friction thermal sca. tstar : -0.18365E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.25178E-04 0.10333E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.38472E-08 3 0.90183E-07 0.16395E-12 0.79961E+00 c Velocity[X] 0.37721E-32 c Velocity[Y] 0.81971E-13 c Velocity[Z] 0.81979E-13 c Pressure 0.65587E-14 16 0.50917E-07 0.50917E-07 0.87120E+00 c k 0.27933E-06 2 0.28481E-07 0.96065E-09 0.12185E+01 c omega 0.13153E+02 1 0.80899E-09 0.11731E+00 0.17831E-02 c TempK 0.94773E+02 1 0.70699E-07 0.15798E-01 0.13900E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.7319e-14 7.3173e-14 -9.1088e-18 -2.3805e-18 v Velocity[Y] -0.00012082 0.00011389 -3.2569e-10 -3.033e-12 v Velocity[Z] -0.00011381 0.00012083 3.7664e-11 -1.3855e-12 v ǁVelocityǁ 3.1649e-10 0.00012949 1.156e-05 8.6057e-06 v Pressure -0.0015211 0.024158 0.0013923 -6.7558e-20 v k 4.9391e-10 0.00093815 0.00060377 0.00077211 v omega 12.103 1.0313e+05 2664.4 497.24 v TempK 288 342.13 294.33 291.25 v Density 1.205 1.205 1.205 1.205 v TurbVisc 5.7881e-15 9.3415e-05 5.4736e-05 7.1726e-05 v CourantNb 3.1783e-09 0.0001885 1.3856e-05 8.9267e-06 v FourierNb 0.087103 0.6281 0.18273 0.15351 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9596 4.9597 0.00056707 -5.8599e-07 v volume_forces[Z] -4.9596 4.9597 -0.00056698 6.9369e-07 v ǁvolume_forcesǁ 1.156e-08 4.9607 0.57331 0.29134 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.54 291.39 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014712 5.2049e-05 2.9012e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.087121 0.6281 0.18275 0.15352 INSTANT 0.871515000E+00 TIME STEP NUMBER 905 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.53018E-05 0.22108E-02 Friction velocity uk : 0.53022E-05 0.22108E-02 Dimensionless distance yplus : 0.35306E-04 0.14709E-01 Friction thermal sca. tstar : -0.18069E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.24797E-04 0.10331E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.53018E-05 0.22108E-02 Friction velocity uk : 0.53022E-05 0.22108E-02 Dimensionless distance yplus : 0.35306E-04 0.14709E-01 Friction thermal sca. tstar : -0.18069E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.24797E-04 0.10331E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.38487E-08 3 0.89997E-07 0.16357E-12 0.79857E+00 c Velocity[X] 0.37592E-32 c Velocity[Y] 0.81781E-13 c Velocity[Z] 0.81790E-13 c Pressure 0.65486E-14 16 0.50839E-07 0.50839E-07 0.87019E+00 c k 0.27900E-06 2 0.28438E-07 0.95664E-09 0.12174E+01 c omega 0.13153E+02 1 0.80706E-09 0.11685E+00 0.17796E-02 c TempK 0.94774E+02 1 0.70588E-07 0.15772E-01 0.13888E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.7274e-14 7.3137e-14 -9.1046e-18 -2.3795e-18 v Velocity[Y] -0.0001208 0.00011386 -3.232e-10 -3.0298e-12 v Velocity[Z] -0.00011379 0.00012081 3.5135e-11 -1.3856e-12 v ǁVelocityǁ 3.1326e-10 0.00012947 1.1564e-05 8.6113e-06 v Pressure -0.0015228 0.024171 0.0013932 4.3732e-20 v k 4.9245e-10 0.00093716 0.00060303 0.00077119 v omega 12.091 1.0313e+05 2664.4 497.23 v TempK 288 342.13 294.34 291.25 v Density 1.205 1.205 1.205 1.205 v TurbVisc 5.771e-15 9.3406e-05 5.472e-05 7.1707e-05 v CourantNb 3.1804e-09 0.00018844 1.3857e-05 8.9301e-06 v FourierNb 0.087044 0.6281 0.1827 0.15348 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9597 4.9597 0.00056726 -5.8623e-07 v volume_forces[Z] -4.9597 4.9597 -0.00056717 6.9395e-07 v ǁvolume_forcesǁ 1.1441e-08 4.9607 0.57349 0.2915 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.54 291.39 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014709 5.2038e-05 2.9005e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.087062 0.6281 0.18272 0.15349 INSTANT 0.872478000E+00 TIME STEP NUMBER 906 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.52189E-05 0.22103E-02 Friction velocity uk : 0.52193E-05 0.22103E-02 Dimensionless distance yplus : 0.34755E-04 0.14706E-01 Friction thermal sca. tstar : -0.17790E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.24409E-04 0.10328E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.52189E-05 0.22103E-02 Friction velocity uk : 0.52193E-05 0.22103E-02 Dimensionless distance yplus : 0.34755E-04 0.14706E-01 Friction thermal sca. tstar : -0.17790E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.24409E-04 0.10328E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.38501E-08 3 0.89812E-07 0.16319E-12 0.79752E+00 c Velocity[X] 0.37463E-32 c Velocity[Y] 0.81592E-13 c Velocity[Z] 0.81601E-13 c Pressure 0.65387E-14 16 0.50762E-07 0.50762E-07 0.86918E+00 c k 0.27868E-06 2 0.28396E-07 0.95266E-09 0.12163E+01 c omega 0.13153E+02 1 0.80513E-09 0.11639E+00 0.17761E-02 c TempK 0.94774E+02 1 0.70477E-07 0.15746E-01 0.13877E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.7229e-14 7.3101e-14 -9.1003e-18 -2.3785e-18 v Velocity[Y] -0.00012078 0.00011384 -3.207e-10 -3.0264e-12 v Velocity[Z] -0.00011377 0.00012078 3.2606e-11 -1.3856e-12 v ǁVelocityǁ 3.101e-10 0.00012944 1.1568e-05 8.6169e-06 v Pressure -0.0015244 0.024184 0.0013941 -1.4492e-19 v k 4.9099e-10 0.00093618 0.00060229 0.00077027 v omega 12.08 1.0313e+05 2664.4 497.22 v TempK 288 342.13 294.34 291.25 v Density 1.205 1.205 1.205 1.205 v TurbVisc 5.7539e-15 9.3396e-05 5.4704e-05 7.1688e-05 v CourantNb 3.1826e-09 0.00018838 1.3857e-05 8.9334e-06 v FourierNb 0.086984 0.6281 0.18267 0.15345 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9597 4.9597 0.00056745 -5.8646e-07 v volume_forces[Z] -4.9597 4.9597 -0.00056735 6.942e-07 v ǁvolume_forcesǁ 1.1324e-08 4.9607 0.57368 0.29166 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.55 291.39 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014706 5.2026e-05 2.8999e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.087002 0.6281 0.18268 0.15346 INSTANT 0.873441000E+00 TIME STEP NUMBER 907 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.51345E-05 0.22099E-02 Friction velocity uk : 0.51349E-05 0.22098E-02 Dimensionless distance yplus : 0.34193E-04 0.14702E-01 Friction thermal sca. tstar : -0.17526E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.24015E-04 0.10326E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.51345E-05 0.22099E-02 Friction velocity uk : 0.51349E-05 0.22098E-02 Dimensionless distance yplus : 0.34193E-04 0.14702E-01 Friction thermal sca. tstar : -0.17526E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.24015E-04 0.10326E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.38516E-08 3 0.89625E-07 0.16281E-12 0.79647E+00 c Velocity[X] 0.37336E-32 c Velocity[Y] 0.81403E-13 c Velocity[Z] 0.81412E-13 c Pressure 0.65281E-14 16 0.50679E-07 0.50679E-07 0.86818E+00 c k 0.27836E-06 2 0.28353E-07 0.94870E-09 0.12151E+01 c omega 0.13153E+02 1 0.80322E-09 0.11594E+00 0.17727E-02 c TempK 0.94775E+02 1 0.70367E-07 0.15720E-01 0.13865E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.7184e-14 7.3066e-14 -9.096e-18 -2.3775e-18 v Velocity[Y] -0.00012076 0.00011382 -3.1821e-10 -3.0317e-12 v Velocity[Z] -0.00011374 0.00012076 3.0073e-11 -1.3899e-12 v ǁVelocityǁ 3.0702e-10 0.00012942 1.1571e-05 8.6224e-06 v Pressure -0.0015261 0.024197 0.001395 -2.6866e-20 v k 4.8955e-10 0.00093519 0.00060155 0.00076935 v omega 12.068 1.0313e+05 2664.4 497.21 v TempK 288 342.13 294.34 291.26 v Density 1.205 1.205 1.205 1.205 v TurbVisc 5.7369e-15 9.3387e-05 5.4688e-05 7.1669e-05 v CourantNb 3.1848e-09 0.00018832 1.3858e-05 8.9367e-06 v FourierNb 0.086925 0.6281 0.18264 0.15342 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9598 4.9598 0.00056763 -5.8669e-07 v volume_forces[Z] -4.9598 4.9598 -0.00056754 6.9445e-07 v ǁvolume_forcesǁ 1.121e-08 4.9608 0.57386 0.29182 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.55 291.4 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014702 5.2015e-05 2.8992e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.086943 0.6281 0.18265 0.15342 INSTANT 0.874404000E+00 TIME STEP NUMBER 908 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.50487E-05 0.22094E-02 Friction velocity uk : 0.50490E-05 0.22093E-02 Dimensionless distance yplus : 0.33621E-04 0.14699E-01 Friction thermal sca. tstar : -0.17275E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.23613E-04 0.10324E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.50487E-05 0.22094E-02 Friction velocity uk : 0.50490E-05 0.22093E-02 Dimensionless distance yplus : 0.33621E-04 0.14699E-01 Friction thermal sca. tstar : -0.17275E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.23613E-04 0.10324E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.38530E-08 3 0.89439E-07 0.16244E-12 0.79542E+00 c Velocity[X] 0.37209E-32 c Velocity[Y] 0.81214E-13 c Velocity[Z] 0.81223E-13 c Pressure 0.65166E-14 16 0.50588E-07 0.50588E-07 0.86718E+00 c k 0.27804E-06 2 0.28310E-07 0.94476E-09 0.12140E+01 c omega 0.13153E+02 1 0.80130E-09 0.11549E+00 0.17692E-02 c TempK 0.94775E+02 1 0.70256E-07 0.15694E-01 0.13854E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.714e-14 7.303e-14 -9.0918e-18 -2.3765e-18 v Velocity[Y] -0.00012074 0.00011379 -3.1572e-10 -3.0287e-12 v Velocity[Z] -0.00011372 0.00012074 2.7546e-11 -1.3896e-12 v ǁVelocityǁ 3.04e-10 0.0001294 1.1575e-05 8.628e-06 v Pressure -0.0015277 0.024209 0.0013958 -1.1227e-19 v k 4.881e-10 0.00093421 0.00060081 0.00076843 v omega 12.057 1.0313e+05 2664.4 497.2 v TempK 288 342.13 294.34 291.26 v Density 1.205 1.205 1.205 1.205 v TurbVisc 5.72e-15 9.3377e-05 5.4672e-05 7.1649e-05 v CourantNb 3.1869e-09 0.00018826 1.3858e-05 8.94e-06 v FourierNb 0.086866 0.6281 0.18261 0.15338 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9598 4.9598 0.00056782 -5.8692e-07 v volume_forces[Z] -4.9598 4.9598 -0.00056772 6.947e-07 v ǁvolume_forcesǁ 1.1099e-08 4.9608 0.57405 0.29197 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.55 291.4 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014699 5.2004e-05 2.8985e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.086884 0.6281 0.18262 0.15339 INSTANT 0.875367000E+00 TIME STEP NUMBER 909 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.49609E-05 0.22089E-02 Friction velocity uk : 0.49613E-05 0.22089E-02 Dimensionless distance yplus : 0.33037E-04 0.14696E-01 Friction thermal sca. tstar : -0.17037E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.23203E-04 0.10321E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.49609E-05 0.22089E-02 Friction velocity uk : 0.49613E-05 0.22089E-02 Dimensionless distance yplus : 0.33037E-04 0.14696E-01 Friction thermal sca. tstar : -0.17037E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.23203E-04 0.10321E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.38545E-08 3 0.89257E-07 0.16206E-12 0.79437E+00 c Velocity[X] 0.37082E-32 c Velocity[Y] 0.81025E-13 c Velocity[Z] 0.81034E-13 c Pressure 0.65166E-14 16 0.50588E-07 0.50588E-07 0.86617E+00 c k 0.27772E-06 2 0.28268E-07 0.94084E-09 0.12129E+01 c omega 0.13153E+02 1 0.79940E-09 0.11503E+00 0.17657E-02 c TempK 0.94776E+02 1 0.70147E-07 0.15668E-01 0.13842E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.7095e-14 7.2995e-14 -9.0876e-18 -2.3755e-18 v Velocity[Y] -0.00012071 0.00011377 -3.1322e-10 -3.0253e-12 v Velocity[Z] -0.00011369 0.00012072 2.5019e-11 -1.3898e-12 v ǁVelocityǁ 3.0105e-10 0.00012937 1.1578e-05 8.6336e-06 v Pressure -0.0015294 0.024222 0.0013967 -3.7162e-20 v k 4.8667e-10 0.00093323 0.00060007 0.00076752 v omega 12.045 1.0313e+05 2664.3 497.19 v TempK 288 342.13 294.34 291.26 v Density 1.205 1.205 1.205 1.205 v TurbVisc 5.7032e-15 9.3368e-05 5.4656e-05 7.163e-05 v CourantNb 3.1891e-09 0.0001882 1.3859e-05 8.9434e-06 v FourierNb 0.086807 0.6281 0.18258 0.15335 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9598 4.9599 0.000568 -5.8715e-07 v volume_forces[Z] -4.9598 4.9599 -0.00056791 6.9496e-07 v ǁvolume_forcesǁ 1.0989e-08 4.9609 0.57423 0.29213 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.55 291.4 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014696 5.1993e-05 2.8979e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.086825 0.6281 0.18259 0.15336 INSTANT 0.876330000E+00 TIME STEP NUMBER 910 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.48713E-05 0.22084E-02 Friction velocity uk : 0.48717E-05 0.22084E-02 Dimensionless distance yplus : 0.32440E-04 0.14693E-01 Friction thermal sca. tstar : -0.16810E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.22784E-04 0.10319E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.48713E-05 0.22084E-02 Friction velocity uk : 0.48717E-05 0.22084E-02 Dimensionless distance yplus : 0.32440E-04 0.14693E-01 Friction thermal sca. tstar : -0.16810E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.22784E-04 0.10319E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.38559E-08 3 0.89072E-07 0.16168E-12 0.79333E+00 c Velocity[X] 0.36956E-32 c Velocity[Y] 0.80837E-13 c Velocity[Z] 0.80846E-13 c Pressure 0.64967E-14 16 0.50433E-07 0.50433E-07 0.86518E+00 c k 0.27740E-06 2 0.28226E-07 0.93694E-09 0.12118E+01 c omega 0.13153E+02 1 0.79750E-09 0.11459E+00 0.17623E-02 c TempK 0.94776E+02 1 0.70037E-07 0.15642E-01 0.13831E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.705e-14 7.2959e-14 -9.0833e-18 -2.3745e-18 v Velocity[Y] -0.00012069 0.00011375 -3.1072e-10 -3.0221e-12 v Velocity[Z] -0.00011367 0.0001207 2.2492e-11 -1.3899e-12 v ǁVelocityǁ 2.9819e-10 0.00012935 1.1582e-05 8.6391e-06 v Pressure -0.001531 0.024235 0.0013976 -4.9026e-22 v k 4.8524e-10 0.00093225 0.00059933 0.0007666 v omega 12.034 1.0313e+05 2664.3 497.18 v TempK 288 342.13 294.35 291.26 v Density 1.205 1.205 1.205 1.205 v TurbVisc 5.6864e-15 9.3358e-05 5.464e-05 7.1611e-05 v CourantNb 3.1912e-09 0.00018814 1.3859e-05 8.9467e-06 v FourierNb 0.086748 0.6281 0.18255 0.15332 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9599 4.9599 0.00056819 -5.8739e-07 v volume_forces[Z] -4.9599 4.9599 -0.0005681 6.9521e-07 v ǁvolume_forcesǁ 1.0883e-08 4.9609 0.57441 0.29229 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.55 291.4 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014693 5.1982e-05 2.8972e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.086766 0.6281 0.18256 0.15333 INSTANT 0.877293000E+00 TIME STEP NUMBER 911 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.47799E-05 0.22079E-02 Friction velocity uk : 0.47803E-05 0.22079E-02 Dimensionless distance yplus : 0.31832E-04 0.14689E-01 Friction thermal sca. tstar : -0.16594E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.22356E-04 0.10317E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.47799E-05 0.22079E-02 Friction velocity uk : 0.47803E-05 0.22079E-02 Dimensionless distance yplus : 0.31832E-04 0.14689E-01 Friction thermal sca. tstar : -0.16594E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.22356E-04 0.10317E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.38574E-08 3 0.88887E-07 0.16131E-12 0.79228E+00 c Velocity[X] 0.36831E-32 c Velocity[Y] 0.80648E-13 c Velocity[Z] 0.80657E-13 c Pressure 0.64854E-14 16 0.50345E-07 0.50345E-07 0.86418E+00 c k 0.27709E-06 2 0.28183E-07 0.93306E-09 0.12107E+01 c omega 0.13153E+02 1 0.79561E-09 0.11414E+00 0.17588E-02 c TempK 0.94777E+02 1 0.69928E-07 0.15616E-01 0.13819E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.7006e-14 7.2924e-14 -9.0791e-18 -2.3735e-18 v Velocity[Y] -0.00012067 0.00011372 -3.0822e-10 -3.0188e-12 v Velocity[Z] -0.00011365 0.00012068 1.9966e-11 -1.3899e-12 v ǁVelocityǁ 2.9541e-10 0.00012932 1.1585e-05 8.6447e-06 v Pressure -0.0015327 0.024248 0.0013985 4.6477e-20 v k 4.8381e-10 0.00093128 0.0005986 0.00076569 v omega 12.023 1.0313e+05 2664.3 497.17 v TempK 288 342.13 294.35 291.26 v Density 1.205 1.205 1.205 1.205 v TurbVisc 5.6697e-15 9.3349e-05 5.4624e-05 7.1592e-05 v CourantNb 3.1933e-09 0.00018808 1.386e-05 8.95e-06 v FourierNb 0.08669 0.6281 0.18252 0.15329 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9599 4.9599 0.00056838 -5.8762e-07 v volume_forces[Z] -4.9599 4.9599 -0.00056828 6.9546e-07 v ǁvolume_forcesǁ 1.078e-08 4.9609 0.5746 0.29245 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.56 291.4 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014689 5.1971e-05 2.8965e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.086708 0.6281 0.18253 0.1533 INSTANT 0.878256000E+00 TIME STEP NUMBER 912 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.46865E-05 0.22074E-02 Friction velocity uk : 0.46869E-05 0.22074E-02 Dimensionless distance yplus : 0.31210E-04 0.14686E-01 Friction thermal sca. tstar : -0.16388E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.21920E-04 0.10315E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.46865E-05 0.22074E-02 Friction velocity uk : 0.46869E-05 0.22074E-02 Dimensionless distance yplus : 0.31210E-04 0.14686E-01 Friction thermal sca. tstar : -0.16388E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.21920E-04 0.10315E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.38589E-08 3 0.88706E-07 0.16093E-12 0.79123E+00 c Velocity[X] 0.36706E-32 c Velocity[Y] 0.80460E-13 c Velocity[Z] 0.80469E-13 c Pressure 0.64807E-14 16 0.50308E-07 0.50308E-07 0.86319E+00 c k 0.27677E-06 2 0.28141E-07 0.92920E-09 0.12095E+01 c omega 0.13153E+02 1 0.79372E-09 0.11369E+00 0.17554E-02 c TempK 0.94777E+02 1 0.69819E-07 0.15591E-01 0.13808E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.6961e-14 7.2888e-14 -9.0749e-18 -2.3725e-18 v Velocity[Y] -0.00012065 0.0001137 -3.0572e-10 -3.0156e-12 v Velocity[Z] -0.00011362 0.00012065 1.7441e-11 -1.3899e-12 v ǁVelocityǁ 2.9272e-10 0.0001293 1.1589e-05 8.6503e-06 v Pressure -0.0015343 0.024261 0.0013994 -4.5202e-20 v k 4.8239e-10 0.0009303 0.00059786 0.00076478 v omega 12.011 1.0313e+05 2664.3 497.16 v TempK 288 342.13 294.35 291.26 v Density 1.205 1.205 1.205 1.205 v TurbVisc 5.653e-15 9.3339e-05 5.4609e-05 7.1574e-05 v CourantNb 3.1955e-09 0.00018802 1.3861e-05 8.9533e-06 v FourierNb 0.086631 0.6281 0.18249 0.15325 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.96 4.96 0.00056856 -5.8785e-07 v volume_forces[Z] -4.96 4.96 -0.00056847 6.9571e-07 v ǁvolume_forcesǁ 1.0679e-08 4.961 0.57478 0.29261 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.56 291.4 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014686 5.196e-05 2.8959e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.086649 0.6281 0.1825 0.15326 INSTANT 0.879219000E+00 TIME STEP NUMBER 913 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.45910E-05 0.22070E-02 Friction velocity uk : 0.45914E-05 0.22069E-02 Dimensionless distance yplus : 0.30574E-04 0.14683E-01 Friction thermal sca. tstar : -0.16191E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.21473E-04 0.10312E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.45910E-05 0.22070E-02 Friction velocity uk : 0.45914E-05 0.22069E-02 Dimensionless distance yplus : 0.30574E-04 0.14683E-01 Friction thermal sca. tstar : -0.16191E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.21473E-04 0.10312E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.38603E-08 3 0.88524E-07 0.16055E-12 0.79018E+00 c Velocity[X] 0.36582E-32 c Velocity[Y] 0.80272E-13 c Velocity[Z] 0.80281E-13 c Pressure 0.64705E-14 16 0.50228E-07 0.50228E-07 0.86219E+00 c k 0.27645E-06 2 0.28099E-07 0.92536E-09 0.12084E+01 c omega 0.13153E+02 1 0.79184E-09 0.11325E+00 0.17520E-02 c TempK 0.94778E+02 1 0.69710E-07 0.15565E-01 0.13796E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.6917e-14 7.2853e-14 -9.0706e-18 -2.3715e-18 v Velocity[Y] -0.00012063 0.00011367 -3.0322e-10 -3.0124e-12 v Velocity[Z] -0.0001136 0.00012063 1.4917e-11 -1.3899e-12 v ǁVelocityǁ 2.9011e-10 0.00012928 1.1592e-05 8.6558e-06 v Pressure -0.001536 0.024274 0.0014003 -1.4041e-19 v k 4.8098e-10 0.00092933 0.00059713 0.00076388 v omega 12 1.0313e+05 2664.3 497.15 v TempK 288 342.13 294.35 291.27 v Density 1.205 1.205 1.205 1.205 v TurbVisc 5.6364e-15 9.333e-05 5.4593e-05 7.1555e-05 v CourantNb 3.1976e-09 0.00018797 1.3861e-05 8.9566e-06 v FourierNb 0.086573 0.6281 0.18246 0.15322 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.96 4.96 0.00056875 -5.8808e-07 v volume_forces[Z] -4.96 4.96 -0.00056865 6.9596e-07 v ǁvolume_forcesǁ 1.0582e-08 4.961 0.57496 0.29277 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.56 291.41 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014683 5.1949e-05 2.8952e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.086591 0.6281 0.18247 0.15323 INSTANT 0.880182000E+00 TIME STEP NUMBER 914 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.44932E-05 0.22065E-02 Friction velocity uk : 0.44936E-05 0.22064E-02 Dimensionless distance yplus : 0.29923E-04 0.14680E-01 Friction thermal sca. tstar : -0.16003E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.21016E-04 0.10310E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.44932E-05 0.22065E-02 Friction velocity uk : 0.44936E-05 0.22064E-02 Dimensionless distance yplus : 0.29923E-04 0.14680E-01 Friction thermal sca. tstar : -0.16003E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.21016E-04 0.10310E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.38618E-08 3 0.88341E-07 0.16018E-12 0.78913E+00 c Velocity[X] 0.36458E-32 c Velocity[Y] 0.80084E-13 c Velocity[Z] 0.80093E-13 c Pressure 0.64541E-14 16 0.50100E-07 0.50100E-07 0.86121E+00 c k 0.27613E-06 2 0.28057E-07 0.92153E-09 0.12073E+01 c omega 0.13153E+02 1 0.78996E-09 0.11281E+00 0.17486E-02 c TempK 0.94778E+02 1 0.69601E-07 0.15539E-01 0.13785E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.6872e-14 7.2818e-14 -9.0664e-18 -2.3705e-18 v Velocity[Y] -0.00012061 0.00011365 -3.0072e-10 -3.0091e-12 v Velocity[Z] -0.00011357 0.00012061 1.2393e-11 -1.39e-12 v ǁVelocityǁ 2.876e-10 0.00012925 1.1596e-05 8.6613e-06 v Pressure -0.0015376 0.024287 0.0014011 8.3933e-20 v k 4.7957e-10 0.00092836 0.0005964 0.00076297 v omega 11.989 1.0313e+05 2664.3 497.14 v TempK 288 342.13 294.35 291.27 v Density 1.205 1.205 1.205 1.205 v TurbVisc 5.6199e-15 9.332e-05 5.4577e-05 7.1536e-05 v CourantNb 3.1997e-09 0.00018791 1.3862e-05 8.9599e-06 v FourierNb 0.086515 0.6281 0.18243 0.15319 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.96 4.9601 0.00056893 -5.8831e-07 v volume_forces[Z] -4.96 4.9601 -0.00056884 6.9621e-07 v ǁvolume_forcesǁ 1.0488e-08 4.9611 0.57515 0.29293 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.56 291.41 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.01468 5.1938e-05 2.8946e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.086533 0.6281 0.18244 0.1532 INSTANT 0.881145000E+00 TIME STEP NUMBER 915 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.43930E-05 0.22060E-02 Friction velocity uk : 0.43934E-05 0.22060E-02 Dimensionless distance yplus : 0.29256E-04 0.14677E-01 Friction thermal sca. tstar : -0.15822E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.20547E-04 0.10308E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.43930E-05 0.22060E-02 Friction velocity uk : 0.43934E-05 0.22060E-02 Dimensionless distance yplus : 0.29256E-04 0.14677E-01 Friction thermal sca. tstar : -0.15822E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.20547E-04 0.10308E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.38632E-08 3 0.88159E-07 0.15980E-12 0.78809E+00 c Velocity[X] 0.36335E-32 c Velocity[Y] 0.79896E-13 c Velocity[Z] 0.79905E-13 c Pressure 0.64436E-14 16 0.50018E-07 0.50018E-07 0.86022E+00 c k 0.27582E-06 2 0.28015E-07 0.91773E-09 0.12062E+01 c omega 0.13153E+02 1 0.78809E-09 0.11237E+00 0.17452E-02 c TempK 0.94779E+02 1 0.69493E-07 0.15514E-01 0.13773E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.6828e-14 7.2783e-14 -9.0622e-18 -2.3695e-18 v Velocity[Y] -0.00012058 0.00011363 -2.9822e-10 -3.0059e-12 v Velocity[Z] -0.00011355 0.00012059 9.8701e-12 -1.39e-12 v ǁVelocityǁ 2.8518e-10 0.00012923 1.1599e-05 8.6669e-06 v Pressure -0.0015392 0.0243 0.001402 -9.0797e-20 v k 4.7817e-10 0.00092739 0.00059567 0.00076207 v omega 11.977 1.0313e+05 2664.3 497.13 v TempK 288 342.13 294.36 291.27 v Density 1.205 1.205 1.205 1.205 v TurbVisc 5.6034e-15 9.3311e-05 5.4561e-05 7.1517e-05 v CourantNb 3.2018e-09 0.00018785 1.3862e-05 8.9632e-06 v FourierNb 0.086457 0.6281 0.1824 0.15316 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9601 4.9601 0.00056912 -5.8854e-07 v volume_forces[Z] -4.9601 4.9601 -0.00056902 6.9646e-07 v ǁvolume_forcesǁ 1.0397e-08 4.9611 0.57533 0.29309 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.56 291.41 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014677 5.1927e-05 2.8939e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.086474 0.6281 0.18241 0.15317 INSTANT 0.882108000E+00 TIME STEP NUMBER 916 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.42902E-05 0.22055E-02 Friction velocity uk : 0.42907E-05 0.22055E-02 Dimensionless distance yplus : 0.28571E-04 0.14673E-01 Friction thermal sca. tstar : -0.15650E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.20067E-04 0.10306E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.42902E-05 0.22055E-02 Friction velocity uk : 0.42907E-05 0.22055E-02 Dimensionless distance yplus : 0.28571E-04 0.14673E-01 Friction thermal sca. tstar : -0.15650E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.20067E-04 0.10306E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.38647E-08 3 0.87980E-07 0.15943E-12 0.78704E+00 c Velocity[X] 0.36213E-32 c Velocity[Y] 0.79708E-13 c Velocity[Z] 0.79718E-13 c Pressure 0.64334E-14 16 0.49938E-07 0.49938E-07 0.85923E+00 c k 0.27550E-06 2 0.27974E-07 0.91395E-09 0.12051E+01 c omega 0.13153E+02 1 0.78623E-09 0.11194E+00 0.17418E-02 c TempK 0.94780E+02 1 0.69385E-07 0.15488E-01 0.13762E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.6784e-14 7.2748e-14 -9.058e-18 -2.3686e-18 v Velocity[Y] -0.00012056 0.0001136 -2.9572e-10 -3.0028e-12 v Velocity[Z] -0.00011353 0.00012057 7.3476e-12 -1.39e-12 v ǁVelocityǁ 2.8286e-10 0.00012921 1.1603e-05 8.6724e-06 v Pressure -0.0015409 0.024312 0.0014029 6.1479e-20 v k 4.7677e-10 0.00092643 0.00059494 0.00076117 v omega 11.966 1.0313e+05 2664.3 497.12 v TempK 288 342.13 294.36 291.27 v Density 1.205 1.205 1.205 1.205 v TurbVisc 5.5871e-15 9.3301e-05 5.4545e-05 7.1498e-05 v CourantNb 3.2039e-09 0.00018779 1.3863e-05 8.9665e-06 v FourierNb 0.086399 0.6281 0.18237 0.15313 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9601 4.9601 0.0005693 -5.8877e-07 v volume_forces[Z] -4.9601 4.9601 -0.00056921 6.9671e-07 v ǁvolume_forcesǁ 1.0309e-08 4.9611 0.57551 0.29325 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.57 291.41 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014673 5.1916e-05 2.8932e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.086417 0.6281 0.18238 0.15314 INSTANT 0.883071000E+00 TIME STEP NUMBER 917 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.41847E-05 0.22050E-02 Friction velocity uk : 0.41852E-05 0.22050E-02 Dimensionless distance yplus : 0.27869E-04 0.14670E-01 Friction thermal sca. tstar : -0.15484E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.19573E-04 0.10303E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.41847E-05 0.22050E-02 Friction velocity uk : 0.41852E-05 0.22050E-02 Dimensionless distance yplus : 0.27869E-04 0.14670E-01 Friction thermal sca. tstar : -0.15484E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.19573E-04 0.10303E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.38661E-08 3 0.87805E-07 0.15905E-12 0.78599E+00 c Velocity[X] 0.36091E-32 c Velocity[Y] 0.79521E-13 c Velocity[Z] 0.79530E-13 c Pressure 0.64314E-14 16 0.49923E-07 0.49923E-07 0.85825E+00 c k 0.27519E-06 2 0.27932E-07 0.91019E-09 0.12040E+01 c omega 0.13153E+02 1 0.78438E-09 0.11150E+00 0.17384E-02 c TempK 0.94780E+02 1 0.69278E-07 0.15463E-01 0.13751E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.674e-14 7.2713e-14 -9.0539e-18 -2.3676e-18 v Velocity[Y] -0.00012054 0.00011358 -2.9322e-10 -2.9996e-12 v Velocity[Z] -0.0001135 0.00012055 4.826e-12 -1.39e-12 v ǁVelocityǁ 2.8064e-10 0.00012918 1.1606e-05 8.6779e-06 v Pressure -0.0015425 0.024325 0.0014038 -6.9127e-20 v k 4.7538e-10 0.00092546 0.00059422 0.00076027 v omega 11.955 1.0313e+05 2664.3 497.11 v TempK 288 342.13 294.36 291.27 v Density 1.205 1.205 1.205 1.205 v TurbVisc 5.5707e-15 9.3292e-05 5.4529e-05 7.1479e-05 v CourantNb 3.206e-09 0.00018773 1.3864e-05 8.9698e-06 v FourierNb 0.086341 0.6281 0.18233 0.15309 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9602 4.9602 0.00056948 -5.89e-07 v volume_forces[Z] -4.9602 4.9602 -0.00056939 6.9695e-07 v ǁvolume_forcesǁ 1.0225e-08 4.9612 0.5757 0.2934 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.57 291.41 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.01467 5.1905e-05 2.8926e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.086359 0.6281 0.18235 0.1531 INSTANT 0.884034000E+00 TIME STEP NUMBER 918 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.40762E-05 0.22046E-02 Friction velocity uk : 0.40767E-05 0.22045E-02 Dimensionless distance yplus : 0.27146E-04 0.14667E-01 Friction thermal sca. tstar : -0.15325E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.19066E-04 0.10301E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.40762E-05 0.22046E-02 Friction velocity uk : 0.40767E-05 0.22045E-02 Dimensionless distance yplus : 0.27146E-04 0.14667E-01 Friction thermal sca. tstar : -0.15325E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.19066E-04 0.10301E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.38676E-08 3 0.87624E-07 0.15868E-12 0.78494E+00 c Velocity[X] 0.35969E-32 c Velocity[Y] 0.79334E-13 c Velocity[Z] 0.79343E-13 c Pressure 0.64193E-14 16 0.49828E-07 0.49828E-07 0.85727E+00 c k 0.27488E-06 2 0.27891E-07 0.90644E-09 0.12029E+01 c omega 0.13153E+02 1 0.78252E-09 0.11107E+00 0.17350E-02 c TempK 0.94781E+02 1 0.69170E-07 0.15438E-01 0.13739E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.6696e-14 7.2678e-14 -9.0497e-18 -2.3666e-18 v Velocity[Y] -0.00012052 0.00011356 -2.9072e-10 -2.9964e-12 v Velocity[Z] -0.00011348 0.00012052 2.3051e-12 -1.39e-12 v ǁVelocityǁ 2.7853e-10 0.00012916 1.161e-05 8.6834e-06 v Pressure -0.0015442 0.024338 0.0014047 7.1873e-20 v k 4.7399e-10 0.0009245 0.0005935 0.00075937 v omega 11.944 1.0313e+05 2664.3 497.1 v TempK 288 342.13 294.36 291.28 v Density 1.205 1.205 1.205 1.205 v TurbVisc 5.5545e-15 9.3282e-05 5.4514e-05 7.146e-05 v CourantNb 3.2081e-09 0.00018767 1.3864e-05 8.973e-06 v FourierNb 0.086283 0.6281 0.1823 0.15306 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9602 4.9602 0.00056967 -5.8922e-07 v volume_forces[Z] -4.9602 4.9602 -0.00056958 6.972e-07 v ǁvolume_forcesǁ 1.0145e-08 4.9612 0.57588 0.29356 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.57 291.42 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014667 5.1894e-05 2.8919e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.086301 0.6281 0.18232 0.15307 INSTANT 0.884997000E+00 TIME STEP NUMBER 919 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.39645E-05 0.22041E-02 Friction velocity uk : 0.39650E-05 0.22040E-02 Dimensionless distance yplus : 0.26402E-04 0.14664E-01 Friction thermal sca. tstar : -0.15172E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.18543E-04 0.10299E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.39645E-05 0.22041E-02 Friction velocity uk : 0.39650E-05 0.22040E-02 Dimensionless distance yplus : 0.26402E-04 0.14664E-01 Friction thermal sca. tstar : -0.15172E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.18543E-04 0.10299E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.38690E-08 3 0.87438E-07 0.15830E-12 0.78390E+00 c Velocity[X] 0.35848E-32 c Velocity[Y] 0.79146E-13 c Velocity[Z] 0.79156E-13 c Pressure 0.64046E-14 16 0.49713E-07 0.49713E-07 0.85629E+00 c k 0.27456E-06 2 0.27849E-07 0.90271E-09 0.12018E+01 c omega 0.13153E+02 1 0.78068E-09 0.11064E+00 0.17317E-02 c TempK 0.94781E+02 1 0.69063E-07 0.15413E-01 0.13728E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.6651e-14 7.2643e-14 -9.0455e-18 -2.3656e-18 v Velocity[Y] -0.0001205 0.00011353 -2.8822e-10 -2.9933e-12 v Velocity[Z] -0.00011346 0.0001205 -2.15e-13 -1.39e-12 v ǁVelocityǁ 2.7653e-10 0.00012914 1.1613e-05 8.6889e-06 v Pressure -0.0015458 0.024351 0.0014055 3.8241e-20 v k 4.7261e-10 0.00092354 0.00059277 0.00075847 v omega 11.932 1.0313e+05 2664.3 497.1 v TempK 288 342.14 294.36 291.28 v Density 1.205 1.205 1.205 1.205 v TurbVisc 5.5383e-15 9.3273e-05 5.4498e-05 7.1441e-05 v CourantNb 3.2101e-09 0.00018761 1.3865e-05 8.9763e-06 v FourierNb 0.086226 0.6281 0.18227 0.15303 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9602 4.9603 0.00056985 -5.8945e-07 v volume_forces[Z] -4.9602 4.9603 -0.00056976 6.9745e-07 v ǁvolume_forcesǁ 1.0069e-08 4.9612 0.57606 0.29372 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.57 291.42 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014664 5.1883e-05 2.8913e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.086244 0.6281 0.18229 0.15304 INSTANT 0.885960000E+00 TIME STEP NUMBER 920 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.38492E-05 0.22036E-02 Friction velocity uk : 0.38497E-05 0.22036E-02 Dimensionless distance yplus : 0.25635E-04 0.14661E-01 Friction thermal sca. tstar : -0.15025E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.18004E-04 0.10297E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.38492E-05 0.22036E-02 Friction velocity uk : 0.38497E-05 0.22036E-02 Dimensionless distance yplus : 0.25635E-04 0.14661E-01 Friction thermal sca. tstar : -0.15025E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.18004E-04 0.10297E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.38704E-08 3 0.87261E-07 0.15793E-12 0.78285E+00 c Velocity[X] 0.35728E-32 c Velocity[Y] 0.78959E-13 c Velocity[Z] 0.78969E-13 c Pressure 0.63962E-14 16 0.49648E-07 0.49648E-07 0.85531E+00 c k 0.27425E-06 2 0.27808E-07 0.89901E-09 0.12007E+01 c omega 0.13153E+02 1 0.77884E-09 0.11021E+00 0.17283E-02 c TempK 0.94782E+02 1 0.68956E-07 0.15387E-01 0.13717E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.6608e-14 7.2608e-14 -9.0413e-18 -2.3647e-18 v Velocity[Y] -0.00012048 0.00011351 -2.8572e-10 -2.9901e-12 v Velocity[Z] -0.00011343 0.00012048 -2.7342e-12 -1.39e-12 v ǁVelocityǁ 2.7463e-10 0.00012911 1.1617e-05 8.6944e-06 v Pressure -0.0015475 0.024364 0.0014064 3.4122e-20 v k 4.7124e-10 0.00092258 0.00059205 0.00075758 v omega 11.921 1.0313e+05 2664.3 497.09 v TempK 288 342.14 294.37 291.28 v Density 1.205 1.205 1.205 1.205 v TurbVisc 5.5222e-15 9.3263e-05 5.4482e-05 7.1422e-05 v CourantNb 3.2122e-09 0.00018755 1.3865e-05 8.9796e-06 v FourierNb 0.086169 0.6281 0.18224 0.153 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9603 4.9603 0.00057004 -5.8968e-07 v volume_forces[Z] -4.9603 4.9603 -0.00056994 6.977e-07 v ǁvolume_forcesǁ 9.9964e-09 4.9613 0.57624 0.29388 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.57 291.42 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014661 5.1872e-05 2.8906e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.086187 0.6281 0.18226 0.15301 INSTANT 0.886923000E+00 TIME STEP NUMBER 921 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.37301E-05 0.22031E-02 Friction velocity uk : 0.37307E-05 0.22031E-02 Dimensionless distance yplus : 0.24842E-04 0.14658E-01 Friction thermal sca. tstar : -0.14884E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.17448E-04 0.10294E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.37301E-05 0.22031E-02 Friction velocity uk : 0.37307E-05 0.22031E-02 Dimensionless distance yplus : 0.24842E-04 0.14658E-01 Friction thermal sca. tstar : -0.14884E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.17448E-04 0.10294E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.38719E-08 3 0.87083E-07 0.15755E-12 0.78180E+00 c Velocity[X] 0.35608E-32 c Velocity[Y] 0.78773E-13 c Velocity[Z] 0.78782E-13 c Pressure 0.63823E-14 16 0.49539E-07 0.49539E-07 0.85434E+00 c k 0.27394E-06 2 0.27767E-07 0.89532E-09 0.11996E+01 c omega 0.13153E+02 1 0.77701E-09 0.10979E+00 0.17250E-02 c TempK 0.94782E+02 1 0.68850E-07 0.15362E-01 0.13705E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.6564e-14 7.2573e-14 -9.0372e-18 -2.3637e-18 v Velocity[Y] -0.00012045 0.00011349 -2.8322e-10 -2.987e-12 v Velocity[Z] -0.00011341 0.00012046 -5.2528e-12 -1.39e-12 v ǁVelocityǁ 2.7285e-10 0.00012909 1.162e-05 8.6999e-06 v Pressure -0.0015491 0.024376 0.0014073 6.8147e-20 v k 4.6987e-10 0.00092162 0.00059133 0.00075669 v omega 11.91 1.0313e+05 2664.3 497.08 v TempK 288 342.14 294.37 291.28 v Density 1.205 1.205 1.205 1.205 v TurbVisc 5.5061e-15 9.3254e-05 5.4466e-05 7.1404e-05 v CourantNb 3.2143e-09 0.00018749 1.3866e-05 8.9829e-06 v FourierNb 0.086112 0.6281 0.18221 0.15297 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9603 4.9603 0.00057022 -5.8991e-07 v volume_forces[Z] -4.9603 4.9603 -0.00057013 6.9794e-07 v ǁvolume_forcesǁ 9.928e-09 4.9613 0.57642 0.29404 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.58 291.42 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014658 5.1861e-05 2.89e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.08613 0.6281 0.18223 0.15298 INSTANT 0.887886000E+00 TIME STEP NUMBER 922 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.36069E-05 0.22026E-02 Friction velocity uk : 0.36074E-05 0.22026E-02 Dimensionless distance yplus : 0.24021E-04 0.14654E-01 Friction thermal sca. tstar : -0.14747E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.16871E-04 0.10292E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.36069E-05 0.22026E-02 Friction velocity uk : 0.36074E-05 0.22026E-02 Dimensionless distance yplus : 0.24021E-04 0.14654E-01 Friction thermal sca. tstar : -0.14747E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.16871E-04 0.10292E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.38733E-08 3 0.86909E-07 0.15718E-12 0.78075E+00 c Velocity[X] 0.35488E-32 c Velocity[Y] 0.78586E-13 c Velocity[Z] 0.78596E-13 c Pressure 0.63797E-14 16 0.49519E-07 0.49519E-07 0.85337E+00 c k 0.27363E-06 2 0.27726E-07 0.89165E-09 0.11985E+01 c omega 0.13153E+02 1 0.77518E-09 0.10936E+00 0.17216E-02 c TempK 0.94783E+02 1 0.68744E-07 0.15337E-01 0.13694E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.652e-14 7.2538e-14 -9.033e-18 -2.3627e-18 v Velocity[Y] -0.00012043 0.00011346 -2.8072e-10 -2.9839e-12 v Velocity[Z] -0.00011339 0.00012044 -7.7705e-12 -1.39e-12 v ǁVelocityǁ 2.7119e-10 0.00012906 1.1624e-05 8.7054e-06 v Pressure -0.0015508 0.024389 0.0014082 -2.922e-20 v k 4.6851e-10 0.00092067 0.00059061 0.0007558 v omega 11.899 1.0313e+05 2664.2 497.07 v TempK 288 342.14 294.37 291.28 v Density 1.205 1.205 1.205 1.205 v TurbVisc 5.4901e-15 9.3245e-05 5.4451e-05 7.1385e-05 v CourantNb 3.2164e-09 0.00018743 1.3866e-05 8.9862e-06 v FourierNb 0.086055 0.6281 0.18218 0.15294 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9604 4.9604 0.0005704 -5.9013e-07 v volume_forces[Z] -4.9604 4.9604 -0.00057031 6.9819e-07 v ǁvolume_forcesǁ 9.8637e-09 4.9614 0.57661 0.2942 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.58 291.42 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014654 5.185e-05 2.8893e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.086073 0.6281 0.1822 0.15294 INSTANT 0.888849000E+00 TIME STEP NUMBER 923 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.34789E-05 0.22022E-02 Friction velocity uk : 0.34795E-05 0.22021E-02 Dimensionless distance yplus : 0.23170E-04 0.14651E-01 Friction thermal sca. tstar : -0.14616E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.16273E-04 0.10290E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.34789E-05 0.22022E-02 Friction velocity uk : 0.34795E-05 0.22021E-02 Dimensionless distance yplus : 0.23170E-04 0.14651E-01 Friction thermal sca. tstar : -0.14616E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.16273E-04 0.10290E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.38748E-08 3 0.86728E-07 0.15681E-12 0.77971E+00 c Velocity[X] 0.35370E-32 c Velocity[Y] 0.78399E-13 c Velocity[Z] 0.78409E-13 c Pressure 0.63620E-14 16 0.49380E-07 0.49380E-07 0.85240E+00 c k 0.27332E-06 2 0.27685E-07 0.88800E-09 0.11974E+01 c omega 0.13153E+02 1 0.77336E-09 0.10894E+00 0.17183E-02 c TempK 0.94783E+02 1 0.68638E-07 0.15312E-01 0.13683E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.6476e-14 7.2504e-14 -9.0289e-18 -2.3617e-18 v Velocity[Y] -0.00012041 0.00011344 -2.7821e-10 -2.9808e-12 v Velocity[Z] -0.00011336 0.00012042 -1.0287e-11 -1.3899e-12 v ǁVelocityǁ 2.6965e-10 0.00012904 1.1627e-05 8.7109e-06 v Pressure -0.0015524 0.024402 0.001409 4.9909e-20 v k 4.6715e-10 0.00091972 0.0005899 0.00075491 v omega 11.888 1.0313e+05 2664.2 497.06 v TempK 288 342.14 294.37 291.28 v Density 1.205 1.205 1.205 1.205 v TurbVisc 5.4741e-15 9.3235e-05 5.4435e-05 7.1366e-05 v CourantNb 3.2184e-09 0.00018738 1.3867e-05 8.9894e-06 v FourierNb 0.085998 0.6281 0.18215 0.1529 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9604 4.9604 0.00057059 -5.9036e-07 v volume_forces[Z] -4.9604 4.9604 -0.0005705 6.9843e-07 v ǁvolume_forcesǁ 9.8036e-09 4.9614 0.57679 0.29435 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.58 291.42 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014651 5.1839e-05 2.8887e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.086016 0.6281 0.18217 0.15291 INSTANT 0.889812000E+00 TIME STEP NUMBER 924 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.33458E-05 0.22017E-02 Friction velocity uk : 0.33464E-05 0.22017E-02 Dimensionless distance yplus : 0.22283E-04 0.14648E-01 Friction thermal sca. tstar : -0.14490E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.15650E-04 0.10288E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.33458E-05 0.22017E-02 Friction velocity uk : 0.33464E-05 0.22017E-02 Dimensionless distance yplus : 0.22283E-04 0.14648E-01 Friction thermal sca. tstar : -0.14490E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.15650E-04 0.10288E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.38762E-08 3 0.86553E-07 0.15644E-12 0.77866E+00 c Velocity[X] 0.35251E-32 c Velocity[Y] 0.78213E-13 c Velocity[Z] 0.78223E-13 c Pressure 0.63539E-14 16 0.49317E-07 0.49317E-07 0.85143E+00 c k 0.27301E-06 2 0.27644E-07 0.88437E-09 0.11963E+01 c omega 0.13153E+02 1 0.77155E-09 0.10852E+00 0.17150E-02 c TempK 0.94784E+02 1 0.68532E-07 0.15287E-01 0.13672E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.6432e-14 7.2469e-14 -9.0247e-18 -2.3608e-18 v Velocity[Y] -0.00012039 0.00011342 -2.7571e-10 -2.9777e-12 v Velocity[Z] -0.00011334 0.00012039 -1.2803e-11 -1.3899e-12 v ǁVelocityǁ 2.6824e-10 0.00012902 1.1631e-05 8.7163e-06 v Pressure -0.0015541 0.024415 0.0014099 -2.5886e-20 v k 4.6579e-10 0.00091876 0.00058918 0.00075402 v omega 11.877 1.0313e+05 2664.2 497.05 v TempK 288 342.14 294.38 291.29 v Density 1.205 1.205 1.205 1.205 v TurbVisc 5.4583e-15 9.3226e-05 5.4419e-05 7.1347e-05 v CourantNb 3.2205e-09 0.00018732 1.3868e-05 8.9927e-06 v FourierNb 0.085941 0.6281 0.18212 0.15287 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9604 4.9605 0.00057077 -5.9059e-07 v volume_forces[Z] -4.9604 4.9605 -0.00057068 6.9868e-07 v ǁvolume_forcesǁ 9.7479e-09 4.9614 0.57697 0.29451 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.58 291.43 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014648 5.1828e-05 2.888e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.085959 0.6281 0.18214 0.15288 INSTANT 0.890775000E+00 TIME STEP NUMBER 925 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.32068E-05 0.22012E-02 Friction velocity uk : 0.32074E-05 0.22012E-02 Dimensionless distance yplus : 0.21358E-04 0.14645E-01 Friction thermal sca. tstar : -0.14367E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.15000E-04 0.10286E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.32068E-05 0.22012E-02 Friction velocity uk : 0.32074E-05 0.22012E-02 Dimensionless distance yplus : 0.21358E-04 0.14645E-01 Friction thermal sca. tstar : -0.14367E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.15000E-04 0.10286E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.38777E-08 3 0.86380E-07 0.15606E-12 0.77761E+00 c Velocity[X] 0.35134E-32 c Velocity[Y] 0.78027E-13 c Velocity[Z] 0.78037E-13 c Pressure 0.63552E-14 16 0.49327E-07 0.49327E-07 0.85047E+00 c k 0.27270E-06 2 0.27603E-07 0.88075E-09 0.11952E+01 c omega 0.13153E+02 1 0.76974E-09 0.10810E+00 0.17117E-02 c TempK 0.94784E+02 1 0.68427E-07 0.15263E-01 0.13661E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.6389e-14 7.2434e-14 -9.0206e-18 -2.3598e-18 v Velocity[Y] -0.00012037 0.00011339 -2.7321e-10 -2.9746e-12 v Velocity[Z] -0.00011332 0.00012037 -1.5318e-11 -1.3899e-12 v ǁVelocityǁ 2.6695e-10 0.00012899 1.1634e-05 8.7218e-06 v Pressure -0.0015557 0.024428 0.0014108 -4.6967e-20 v k 4.6444e-10 0.00091781 0.00058847 0.00075314 v omega 11.866 1.0313e+05 2664.2 497.04 v TempK 288 342.14 294.38 291.29 v Density 1.205 1.205 1.205 1.205 v TurbVisc 5.4425e-15 9.3216e-05 5.4404e-05 7.1329e-05 v CourantNb 3.2225e-09 0.00018726 1.3868e-05 8.996e-06 v FourierNb 0.085885 0.6281 0.18209 0.15284 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9605 4.9605 0.00057095 -5.9081e-07 v volume_forces[Z] -4.9605 4.9605 -0.00057086 6.9892e-07 v ǁvolume_forcesǁ 9.6967e-09 4.9615 0.57715 0.29467 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.58 291.43 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014645 5.1817e-05 2.8874e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.085903 0.6281 0.18211 0.15285 INSTANT 0.891738000E+00 TIME STEP NUMBER 926 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.30611E-05 0.22007E-02 Friction velocity uk : 0.30618E-05 0.22007E-02 Dimensionless distance yplus : 0.20388E-04 0.14642E-01 Friction thermal sca. tstar : -0.14249E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.14319E-04 0.10283E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.30611E-05 0.22007E-02 Friction velocity uk : 0.30618E-05 0.22007E-02 Dimensionless distance yplus : 0.20388E-04 0.14642E-01 Friction thermal sca. tstar : -0.14249E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.14319E-04 0.10283E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.38791E-08 3 0.86200E-07 0.15569E-12 0.77656E+00 c Velocity[X] 0.35017E-32 c Velocity[Y] 0.77841E-13 c Velocity[Z] 0.77851E-13 c Pressure 0.63318E-14 16 0.49144E-07 0.49144E-07 0.84950E+00 c k 0.27239E-06 2 0.27562E-07 0.87716E-09 0.11941E+01 c omega 0.13153E+02 1 0.76793E-09 0.10769E+00 0.17084E-02 c TempK 0.94785E+02 1 0.68322E-07 0.15238E-01 0.13649E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.6345e-14 7.24e-14 -9.0165e-18 -2.3588e-18 v Velocity[Y] -0.00012035 0.00011337 -2.7071e-10 -2.9715e-12 v Velocity[Z] -0.00011329 0.00012035 -1.7833e-11 -1.3898e-12 v ǁVelocityǁ 2.6579e-10 0.00012897 1.1638e-05 8.7273e-06 v Pressure -0.0015574 0.02444 0.0014117 -7.354e-20 v k 4.631e-10 0.00091687 0.00058776 0.00075226 v omega 11.855 1.0313e+05 2664.2 497.03 v TempK 288 342.14 294.38 291.29 v Density 1.205 1.205 1.205 1.205 v TurbVisc 5.4267e-15 9.3207e-05 5.4388e-05 7.131e-05 v CourantNb 3.2245e-09 0.0001872 1.3869e-05 8.9992e-06 v FourierNb 0.085828 0.6281 0.18206 0.15281 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9605 4.9605 0.00057114 -5.9104e-07 v volume_forces[Z] -4.9605 4.9605 -0.00057105 6.9917e-07 v ǁvolume_forcesǁ 9.6501e-09 4.9615 0.57733 0.29483 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.59 291.43 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014642 5.1806e-05 2.8867e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.085846 0.6281 0.18208 0.15282 INSTANT 0.892701000E+00 TIME STEP NUMBER 927 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.29079E-05 0.22003E-02 Friction velocity uk : 0.29086E-05 0.22002E-02 Dimensionless distance yplus : 0.19368E-04 0.14639E-01 Friction thermal sca. tstar : -0.14136E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.13603E-04 0.10281E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.29079E-05 0.22003E-02 Friction velocity uk : 0.29086E-05 0.22002E-02 Dimensionless distance yplus : 0.19368E-04 0.14639E-01 Friction thermal sca. tstar : -0.14136E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.13603E-04 0.10281E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.38805E-08 3 0.86027E-07 0.15532E-12 0.77551E+00 c Velocity[X] 0.34900E-32 c Velocity[Y] 0.77655E-13 c Velocity[Z] 0.77665E-13 c Pressure 0.63218E-14 16 0.49066E-07 0.49066E-07 0.84854E+00 c k 0.27208E-06 2 0.27521E-07 0.87358E-09 0.11930E+01 c omega 0.13153E+02 1 0.76614E-09 0.10727E+00 0.17051E-02 c TempK 0.94785E+02 1 0.68217E-07 0.15213E-01 0.13638E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.6302e-14 7.2366e-14 -9.0124e-18 -2.3579e-18 v Velocity[Y] -0.00012032 0.00011335 -2.682e-10 -2.9684e-12 v Velocity[Z] -0.00011327 0.00012033 -2.0346e-11 -1.3897e-12 v ǁVelocityǁ 2.6476e-10 0.00012895 1.1641e-05 8.7327e-06 v Pressure -0.001559 0.024453 0.0014125 -9.5994e-20 v k 4.6176e-10 0.00091592 0.00058705 0.00075138 v omega 11.844 1.0313e+05 2664.2 497.02 v TempK 288 342.14 294.38 291.29 v Density 1.205 1.205 1.205 1.205 v TurbVisc 5.411e-15 9.3198e-05 5.4372e-05 7.1291e-05 v CourantNb 3.2266e-09 0.00018714 1.3869e-05 9.0025e-06 v FourierNb 0.085772 0.6281 0.18203 0.15278 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9606 4.9606 0.00057132 -5.9126e-07 v volume_forces[Z] -4.9606 4.9606 -0.00057123 6.9941e-07 v ǁvolume_forcesǁ 9.6082e-09 4.9616 0.57751 0.29498 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.59 291.43 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014639 5.1795e-05 2.8861e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.08579 0.6281 0.18205 0.15279 INSTANT 0.893664000E+00 TIME STEP NUMBER 928 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.27457E-05 0.21998E-02 Friction velocity uk : 0.27464E-05 0.21998E-02 Dimensionless distance yplus : 0.18288E-04 0.14635E-01 Friction thermal sca. tstar : -0.14026E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.12844E-04 0.10279E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.27457E-05 0.21998E-02 Friction velocity uk : 0.27464E-05 0.21998E-02 Dimensionless distance yplus : 0.18288E-04 0.14635E-01 Friction thermal sca. tstar : -0.14026E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.12844E-04 0.10279E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.38820E-08 3 0.85854E-07 0.15495E-12 0.77447E+00 c Velocity[X] 0.34784E-32 c Velocity[Y] 0.77469E-13 c Velocity[Z] 0.77479E-13 c Pressure 0.63139E-14 16 0.49005E-07 0.49005E-07 0.84758E+00 c k 0.27178E-06 2 0.27481E-07 0.87002E-09 0.11920E+01 c omega 0.13153E+02 1 0.76434E-09 0.10686E+00 0.17019E-02 c TempK 0.94786E+02 1 0.68112E-07 0.15189E-01 0.13627E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.6259e-14 7.2331e-14 -9.0083e-18 -2.3569e-18 v Velocity[Y] -0.0001203 0.00011333 -2.657e-10 -2.9654e-12 v Velocity[Z] -0.00011325 0.00012031 -2.2858e-11 -1.3897e-12 v ǁVelocityǁ 2.6387e-10 0.00012892 1.1645e-05 8.7381e-06 v Pressure -0.0015607 0.024466 0.0014134 -4.6869e-20 v k 4.6043e-10 0.00091498 0.00058634 0.0007505 v omega 11.833 1.0313e+05 2664.2 497.01 v TempK 288 342.14 294.38 291.29 v Density 1.205 1.205 1.205 1.205 v TurbVisc 5.3954e-15 9.3188e-05 5.4357e-05 7.1272e-05 v CourantNb 3.2286e-09 0.00018709 1.387e-05 9.0057e-06 v FourierNb 0.085716 0.6281 0.182 0.15275 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9606 4.9606 0.0005715 -5.9149e-07 v volume_forces[Z] -4.9606 4.9606 -0.00057141 6.9966e-07 v ǁvolume_forcesǁ 9.5711e-09 4.9616 0.57769 0.29514 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.59 291.43 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014635 5.1784e-05 2.8854e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.085734 0.6281 0.18202 0.15275 INSTANT 0.894627000E+00 TIME STEP NUMBER 929 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.25729E-05 0.21993E-02 Friction velocity uk : 0.25737E-05 0.21993E-02 Dimensionless distance yplus : 0.17138E-04 0.14632E-01 Friction thermal sca. tstar : -0.13919E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.12037E-04 0.10277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.25729E-05 0.21993E-02 Friction velocity uk : 0.25737E-05 0.21993E-02 Dimensionless distance yplus : 0.17138E-04 0.14632E-01 Friction thermal sca. tstar : -0.13919E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.12037E-04 0.10277E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.38834E-08 3 0.85680E-07 0.15458E-12 0.77342E+00 c Velocity[X] 0.34668E-32 c Velocity[Y] 0.77283E-13 c Velocity[Z] 0.77294E-13 c Pressure 0.63021E-14 16 0.48912E-07 0.48912E-07 0.84662E+00 c k 0.27147E-06 2 0.27441E-07 0.86647E-09 0.11909E+01 c omega 0.13153E+02 1 0.76256E-09 0.10645E+00 0.16986E-02 c TempK 0.94786E+02 1 0.68008E-07 0.15164E-01 0.13616E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.6215e-14 7.2297e-14 -9.0042e-18 -2.356e-18 v Velocity[Y] -0.00012028 0.0001133 -2.632e-10 -2.9623e-12 v Velocity[Z] -0.00011322 0.00012029 -2.537e-11 -1.3896e-12 v ǁVelocityǁ 2.6311e-10 0.0001289 1.1648e-05 8.7436e-06 v Pressure -0.0015623 0.024479 0.0014143 6.0204e-20 v k 4.591e-10 0.00091404 0.00058563 0.00074962 v omega 11.822 1.0313e+05 2664.2 497 v TempK 288 342.14 294.39 291.3 v Density 1.205 1.205 1.205 1.205 v TurbVisc 5.3798e-15 9.3179e-05 5.4341e-05 7.1254e-05 v CourantNb 3.2306e-09 0.00018703 1.387e-05 9.009e-06 v FourierNb 0.08566 0.6281 0.18197 0.15271 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9606 4.9607 0.00057169 -5.9171e-07 v volume_forces[Z] -4.9606 4.9607 -0.00057159 6.999e-07 v ǁvolume_forcesǁ 9.5388e-09 4.9616 0.57787 0.2953 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.59 291.44 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014632 5.1773e-05 2.8848e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.085678 0.6281 0.18199 0.15272 INSTANT 0.895590000E+00 TIME STEP NUMBER 930 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.23872E-05 0.21988E-02 Friction velocity uk : 0.23881E-05 0.21988E-02 Dimensionless distance yplus : 0.15902E-04 0.14629E-01 Friction thermal sca. tstar : -0.13816E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.11169E-04 0.10275E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.23872E-05 0.21988E-02 Friction velocity uk : 0.23881E-05 0.21988E-02 Dimensionless distance yplus : 0.15902E-04 0.14629E-01 Friction thermal sca. tstar : -0.13816E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.11169E-04 0.10275E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.38849E-08 3 0.85508E-07 0.15421E-12 0.77237E+00 c Velocity[X] 0.34553E-32 c Velocity[Y] 0.77098E-13 c Velocity[Z] 0.77108E-13 c Pressure 0.62924E-14 16 0.48836E-07 0.48836E-07 0.84567E+00 c k 0.27116E-06 2 0.27400E-07 0.86295E-09 0.11898E+01 c omega 0.13153E+02 1 0.76078E-09 0.10605E+00 0.16953E-02 c TempK 0.94787E+02 1 0.67904E-07 0.15140E-01 0.13605E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.6172e-14 7.2263e-14 -9.0001e-18 -2.355e-18 v Velocity[Y] -0.00012026 0.00011328 -2.607e-10 -2.9593e-12 v Velocity[Z] -0.0001132 0.00012026 -2.788e-11 -1.3896e-12 v ǁVelocityǁ 2.625e-10 0.00012888 1.1652e-05 8.749e-06 v Pressure -0.001564 0.024491 0.0014152 7.1186e-20 v k 4.5778e-10 0.0009131 0.00058493 0.00074874 v omega 11.811 1.0313e+05 2664.2 496.99 v TempK 288 342.14 294.39 291.3 v Density 1.205 1.205 1.205 1.205 v TurbVisc 5.3643e-15 9.317e-05 5.4326e-05 7.1235e-05 v CourantNb 3.2326e-09 0.00018697 1.3871e-05 9.0122e-06 v FourierNb 0.085604 0.6281 0.18194 0.15268 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9607 4.9607 0.00057187 -5.9194e-07 v volume_forces[Z] -4.9607 4.9607 -0.00057178 7.0014e-07 v ǁvolume_forcesǁ 9.5115e-09 4.9617 0.57805 0.29546 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.59 291.44 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014629 5.1762e-05 2.8841e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.085622 0.6281 0.18196 0.15269 INSTANT 0.896553000E+00 TIME STEP NUMBER 931 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.21854E-05 0.21984E-02 Friction velocity uk : 0.21863E-05 0.21983E-02 Dimensionless distance yplus : 0.14558E-04 0.14626E-01 Friction thermal sca. tstar : -0.13716E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.10225E-04 0.10272E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.21854E-05 0.21984E-02 Friction velocity uk : 0.21863E-05 0.21983E-02 Dimensionless distance yplus : 0.14558E-04 0.14626E-01 Friction thermal sca. tstar : -0.13716E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.10225E-04 0.10272E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.38863E-08 3 0.85334E-07 0.15384E-12 0.77133E+00 c Velocity[X] 0.34439E-32 c Velocity[Y] 0.76913E-13 c Velocity[Z] 0.76923E-13 c Pressure 0.62819E-14 16 0.48755E-07 0.48755E-07 0.84472E+00 c k 0.27086E-06 2 0.27360E-07 0.85944E-09 0.11887E+01 c omega 0.13153E+02 1 0.75900E-09 0.10564E+00 0.16921E-02 c TempK 0.94788E+02 1 0.67800E-07 0.15115E-01 0.13594E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.6129e-14 7.2228e-14 -8.996e-18 -2.3541e-18 v Velocity[Y] -0.00012024 0.00011326 -2.5819e-10 -2.9563e-12 v Velocity[Z] -0.00011318 0.00012024 -3.039e-11 -1.3895e-12 v ǁVelocityǁ 2.6202e-10 0.00012885 1.1655e-05 8.7544e-06 v Pressure -0.0015656 0.024504 0.001416 -1.9414e-20 v k 4.5647e-10 0.00091216 0.00058422 0.00074787 v omega 11.8 1.0313e+05 2664.2 496.98 v TempK 288 342.14 294.39 291.3 v Density 1.205 1.205 1.205 1.205 v TurbVisc 5.3489e-15 9.316e-05 5.431e-05 7.1217e-05 v CourantNb 3.2346e-09 0.00018691 1.3872e-05 9.0154e-06 v FourierNb 0.085549 0.6281 0.18191 0.15265 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9607 4.9607 0.00057205 -5.9216e-07 v volume_forces[Z] -4.9607 4.9607 -0.00057196 7.0038e-07 v ǁvolume_forcesǁ 9.4892e-09 4.9617 0.57823 0.29561 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.6 291.44 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014626 5.1751e-05 2.8835e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.085567 0.6281 0.18193 0.15266 INSTANT 0.897516000E+00 TIME STEP NUMBER 932 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19623E-05 0.21979E-02 Friction velocity uk : 0.19633E-05 0.21979E-02 Dimensionless distance yplus : 0.13074E-04 0.14623E-01 Friction thermal sca. tstar : -0.13620E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.91821E-05 0.10270E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19623E-05 0.21979E-02 Friction velocity uk : 0.19633E-05 0.21979E-02 Dimensionless distance yplus : 0.13074E-04 0.14623E-01 Friction thermal sca. tstar : -0.13620E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.91821E-05 0.10270E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.38877E-08 3 0.85212E-07 0.15347E-12 0.77028E+00 c Velocity[X] 0.34325E-32 c Velocity[Y] 0.76728E-13 c Velocity[Z] 0.76738E-13 c Pressure 0.63944E-14 16 0.49627E-07 0.49627E-07 0.84377E+00 c k 0.27055E-06 2 0.27320E-07 0.85595E-09 0.11876E+01 c omega 0.13153E+02 1 0.75723E-09 0.10524E+00 0.16888E-02 c TempK 0.94788E+02 1 0.67697E-07 0.15091E-01 0.13583E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.6086e-14 7.2194e-14 -8.9919e-18 -2.3531e-18 v Velocity[Y] -0.00012022 0.00011323 -2.5569e-10 -2.9533e-12 v Velocity[Z] -0.00011315 0.00012022 -3.2898e-11 -1.3894e-12 v ǁVelocityǁ 2.6169e-10 0.00012883 1.1658e-05 8.7598e-06 v Pressure -0.0015673 0.024517 0.0014169 -9.5896e-20 v k 4.5515e-10 0.00091122 0.00058352 0.000747 v omega 11.789 1.0313e+05 2664.2 496.97 v TempK 288 342.14 294.39 291.3 v Density 1.205 1.205 1.205 1.205 v TurbVisc 5.3335e-15 9.3151e-05 5.4295e-05 7.1198e-05 v CourantNb 3.2367e-09 0.00018685 1.3872e-05 9.0187e-06 v FourierNb 0.085493 0.6281 0.18188 0.15262 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9607 4.9608 0.00057223 -5.9238e-07 v volume_forces[Z] -4.9607 4.9608 -0.00057214 7.0063e-07 v ǁvolume_forcesǁ 9.472e-09 4.9617 0.57841 0.29577 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.6 291.44 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014623 5.174e-05 2.8828e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.085511 0.6281 0.1819 0.15263 INSTANT 0.898479000E+00 TIME STEP NUMBER 933 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.17098E-05 0.21974E-02 Friction velocity uk : 0.17110E-05 0.21974E-02 Dimensionless distance yplus : 0.11393E-04 0.14620E-01 Friction thermal sca. tstar : -0.13526E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.80019E-05 0.10268E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.17098E-05 0.21974E-02 Friction velocity uk : 0.17110E-05 0.21974E-02 Dimensionless distance yplus : 0.11393E-04 0.14620E-01 Friction thermal sca. tstar : -0.13526E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.80019E-05 0.10268E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.38892E-08 3 0.84995E-07 0.15310E-12 0.76923E+00 c Velocity[X] 0.34211E-32 c Velocity[Y] 0.76543E-13 c Velocity[Z] 0.76553E-13 c Pressure 0.62661E-14 16 0.48631E-07 0.48631E-07 0.84282E+00 c k 0.27025E-06 2 0.27280E-07 0.85248E-09 0.11866E+01 c omega 0.13153E+02 1 0.75547E-09 0.10483E+00 0.16856E-02 c TempK 0.94789E+02 1 0.67594E-07 0.15066E-01 0.13572E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.6043e-14 7.216e-14 -8.9878e-18 -2.3521e-18 v Velocity[Y] -0.00012019 0.00011321 -2.5319e-10 -2.9503e-12 v Velocity[Z] -0.00011313 0.0001202 -3.5406e-11 -1.3893e-12 v ǁVelocityǁ 2.615e-10 0.0001288 1.1662e-05 8.7653e-06 v Pressure -0.0015689 0.024529 0.0014178 -7.452e-20 v k 4.5385e-10 0.00091029 0.00058282 0.00074613 v omega 11.778 1.0313e+05 2664.2 496.96 v TempK 288 342.14 294.39 291.3 v Density 1.205 1.205 1.205 1.205 v TurbVisc 5.3181e-15 9.3141e-05 5.4279e-05 7.1179e-05 v CourantNb 3.2386e-09 0.0001868 1.3873e-05 9.0219e-06 v FourierNb 0.085438 0.6281 0.18185 0.15259 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9608 4.9608 0.00057241 -5.9261e-07 v volume_forces[Z] -4.9608 4.9608 -0.00057232 7.0087e-07 v ǁvolume_forcesǁ 9.46e-09 4.9618 0.57859 0.29593 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.6 291.44 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.01462 5.1729e-05 2.8822e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.085456 0.6281 0.18187 0.1526 INSTANT 0.899442000E+00 TIME STEP NUMBER 934 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.14121E-05 0.21970E-02 Friction velocity uk : 0.14136E-05 0.21969E-02 Dimensionless distance yplus : 0.94129E-05 0.14617E-01 Friction thermal sca. tstar : -0.13436E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.66110E-05 0.10266E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.14121E-05 0.21970E-02 Friction velocity uk : 0.14136E-05 0.21969E-02 Dimensionless distance yplus : 0.94129E-05 0.14617E-01 Friction thermal sca. tstar : -0.13436E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.66110E-05 0.10266E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.38906E-08 3 0.84828E-07 0.15273E-12 0.76819E+00 c Velocity[X] 0.34099E-32 c Velocity[Y] 0.76358E-13 c Velocity[Z] 0.76369E-13 c Pressure 0.62533E-14 16 0.48531E-07 0.48531E-07 0.84187E+00 c k 0.26995E-06 2 0.27240E-07 0.84903E-09 0.11855E+01 c omega 0.13153E+02 1 0.75371E-09 0.10443E+00 0.16824E-02 c TempK 0.94789E+02 1 0.67491E-07 0.15042E-01 0.13561E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.6e-14 7.2126e-14 -8.9837e-18 -2.3512e-18 v Velocity[Y] -0.00012017 0.00011319 -2.5069e-10 -2.9473e-12 v Velocity[Z] -0.00011311 0.00012018 -3.7912e-11 -1.3892e-12 v ǁVelocityǁ 2.6146e-10 0.00012878 1.1665e-05 8.7707e-06 v Pressure -0.0015706 0.024542 0.0014186 2.314e-20 v k 4.5255e-10 0.00090935 0.00058212 0.00074526 v omega 11.767 1.0313e+05 2664.2 496.95 v TempK 288 342.14 294.4 291.3 v Density 1.205 1.205 1.205 1.205 v TurbVisc 5.3029e-15 9.3132e-05 5.4263e-05 7.1161e-05 v CourantNb 3.2406e-09 0.00018674 1.3873e-05 9.0251e-06 v FourierNb 0.085383 0.6281 0.18182 0.15256 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9608 4.9608 0.0005726 -5.9283e-07 v volume_forces[Z] -4.9608 4.9608 -0.00057251 7.0111e-07 v ǁvolume_forcesǁ 9.4532e-09 4.9618 0.57877 0.29608 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.6 291.44 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014617 5.1718e-05 2.8815e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.085401 0.6281 0.18184 0.15257 INSTANT 0.900405000E+00 TIME STEP NUMBER 935 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10309E-05 0.21965E-02 Friction velocity uk : 0.10329E-05 0.21965E-02 Dimensionless distance yplus : 0.68780E-05 0.14613E-01 Friction thermal sca. tstar : -0.13348E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.48307E-05 0.10264E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10309E-05 0.21965E-02 Friction velocity uk : 0.10329E-05 0.21965E-02 Dimensionless distance yplus : 0.68780E-05 0.14613E-01 Friction thermal sca. tstar : -0.13348E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.48307E-05 0.10264E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.38920E-08 3 0.84655E-07 0.15236E-12 0.76714E+00 c Velocity[X] 0.33987E-32 c Velocity[Y] 0.76173E-13 c Velocity[Z] 0.76184E-13 c Pressure 0.62435E-14 16 0.48454E-07 0.48454E-07 0.84093E+00 c k 0.26964E-06 2 0.27200E-07 0.84559E-09 0.11844E+01 c omega 0.13153E+02 1 0.75196E-09 0.10404E+00 0.16792E-02 c TempK 0.94790E+02 1 0.67388E-07 0.15018E-01 0.13550E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.5957e-14 7.2092e-14 -8.9797e-18 -2.3502e-18 v Velocity[Y] -0.00012015 0.00011317 -2.4818e-10 -2.9444e-12 v Velocity[Z] -0.00011308 0.00012016 -4.0417e-11 -1.3891e-12 v ǁVelocityǁ 2.6156e-10 0.00012876 1.1669e-05 8.776e-06 v Pressure -0.0015722 0.024555 0.0014195 -3.8633e-20 v k 4.5125e-10 0.00090842 0.00058142 0.00074439 v omega 11.756 1.0313e+05 2664.1 496.94 v TempK 288 342.14 294.4 291.31 v Density 1.205 1.205 1.205 1.205 v TurbVisc 5.2877e-15 9.3123e-05 5.4248e-05 7.1142e-05 v CourantNb 3.2426e-09 0.00018668 1.3874e-05 9.0283e-06 v FourierNb 0.085328 0.6281 0.1818 0.15252 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9609 4.9609 0.00057278 -5.9305e-07 v volume_forces[Z] -4.9609 4.9609 -0.00057269 7.0135e-07 v ǁvolume_forcesǁ 9.4517e-09 4.9619 0.57895 0.29624 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.6 291.45 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014613 5.1707e-05 2.8809e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.085346 0.6281 0.18181 0.15253 INSTANT 0.901368000E+00 TIME STEP NUMBER 936 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.38491E-06 0.21960E-02 Friction velocity uk : 0.39016E-06 0.21960E-02 Dimensionless distance yplus : 0.25980E-05 0.14610E-01 Friction thermal sca. tstar : -0.13263E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.18247E-05 0.10261E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.38491E-06 0.21960E-02 Friction velocity uk : 0.39016E-06 0.21960E-02 Dimensionless distance yplus : 0.25980E-05 0.14610E-01 Friction thermal sca. tstar : -0.13263E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.18247E-05 0.10261E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.38935E-08 3 0.84482E-07 0.15199E-12 0.76609E+00 c Velocity[X] 0.33875E-32 c Velocity[Y] 0.75989E-13 c Velocity[Z] 0.76000E-13 c Pressure 0.62330E-14 16 0.48373E-07 0.48373E-07 0.83998E+00 c k 0.26934E-06 2 0.27160E-07 0.84217E-09 0.11834E+01 c omega 0.13153E+02 1 0.75021E-09 0.10364E+00 0.16760E-02 c TempK 0.94790E+02 1 0.67286E-07 0.14994E-01 0.13539E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.5914e-14 7.2058e-14 -8.9756e-18 -2.3493e-18 v Velocity[Y] -0.00012013 0.00011314 -2.4568e-10 -2.9414e-12 v Velocity[Z] -0.00011306 0.00012013 -4.2922e-11 -1.389e-12 v ǁVelocityǁ 2.6182e-10 0.00012873 1.1672e-05 8.7814e-06 v Pressure -0.0015739 0.024568 0.0014204 4.2751e-20 v k 4.4996e-10 0.00090749 0.00058072 0.00074353 v omega 11.745 1.0313e+05 2664.1 496.93 v TempK 288 342.14 294.4 291.31 v Density 1.205 1.205 1.205 1.205 v TurbVisc 5.2725e-15 9.3114e-05 5.4233e-05 7.1124e-05 v CourantNb 3.2446e-09 0.00018662 1.3875e-05 9.0316e-06 v FourierNb 0.085273 0.6281 0.18177 0.15249 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9609 4.9609 0.00057296 -5.9328e-07 v volume_forces[Z] -4.9609 4.9609 -0.00057287 7.0159e-07 v ǁvolume_forcesǁ 9.4555e-09 4.9619 0.57913 0.2964 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.61 291.45 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.01461 5.1697e-05 2.8802e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.085291 0.6281 0.18178 0.1525 INSTANT 0.902331000E+00 TIME STEP NUMBER 937 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.89556E-06 0.21956E-02 Friction velocity uk : 0.89782E-06 0.21955E-02 Dimensionless distance yplus : 0.59785E-05 0.14607E-01 Friction thermal sca. tstar : -0.13180E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.41989E-05 0.10259E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.89556E-06 0.21956E-02 Friction velocity uk : 0.89782E-06 0.21955E-02 Dimensionless distance yplus : 0.59785E-05 0.14607E-01 Friction thermal sca. tstar : -0.13180E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.41989E-05 0.10259E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.38949E-08 3 0.84311E-07 0.15162E-12 0.76505E+00 c Velocity[X] 0.33763E-32 c Velocity[Y] 0.75805E-13 c Velocity[Z] 0.75816E-13 c Pressure 0.62233E-14 16 0.48296E-07 0.48296E-07 0.83904E+00 c k 0.26904E-06 2 0.27121E-07 0.83876E-09 0.11823E+01 c omega 0.13153E+02 1 0.74847E-09 0.10324E+00 0.16728E-02 c TempK 0.94791E+02 1 0.67183E-07 0.14970E-01 0.13528E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.5871e-14 7.2024e-14 -8.9716e-18 -2.3484e-18 v Velocity[Y] -0.00012011 0.00011312 -2.4318e-10 -2.9384e-12 v Velocity[Z] -0.00011304 0.00012011 -4.5425e-11 -1.3889e-12 v ǁVelocityǁ 2.6222e-10 0.00012871 1.1676e-05 8.7868e-06 v Pressure -0.0015755 0.02458 0.0014212 8.8149e-20 v k 4.4867e-10 0.00090657 0.00058003 0.00074266 v omega 11.734 1.0313e+05 2664.1 496.92 v TempK 288 342.14 294.4 291.31 v Density 1.205 1.205 1.205 1.205 v TurbVisc 5.2574e-15 9.3104e-05 5.4217e-05 7.1105e-05 v CourantNb 3.2466e-09 0.00018657 1.3875e-05 9.0348e-06 v FourierNb 0.085218 0.6281 0.18174 0.15246 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9609 4.961 0.00057314 -5.935e-07 v volume_forces[Z] -4.9609 4.961 -0.00057305 7.0183e-07 v ǁvolume_forcesǁ 9.4646e-09 4.9619 0.57931 0.29656 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.61 291.45 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014607 5.1686e-05 2.8796e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.085236 0.6281 0.18175 0.15247 INSTANT 0.903294000E+00 TIME STEP NUMBER 938 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.13189E-05 0.21951E-02 Friction velocity uk : 0.13205E-05 0.21951E-02 Dimensionless distance yplus : 0.87928E-05 0.14604E-01 Friction thermal sca. tstar : -0.13100E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.61755E-05 0.10257E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.13189E-05 0.21951E-02 Friction velocity uk : 0.13205E-05 0.21951E-02 Dimensionless distance yplus : 0.87928E-05 0.14604E-01 Friction thermal sca. tstar : -0.13100E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.61755E-05 0.10257E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.38963E-08 3 0.84143E-07 0.15125E-12 0.76400E+00 c Velocity[X] 0.33652E-32 c Velocity[Y] 0.75621E-13 c Velocity[Z] 0.75632E-13 c Pressure 0.62137E-14 16 0.48221E-07 0.48221E-07 0.83811E+00 c k 0.26874E-06 2 0.27081E-07 0.83538E-09 0.11812E+01 c omega 0.13153E+02 1 0.74674E-09 0.10285E+00 0.16696E-02 c TempK 0.94791E+02 1 0.67082E-07 0.14946E-01 0.13517E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.5829e-14 7.199e-14 -8.9675e-18 -2.3474e-18 v Velocity[Y] -0.00012009 0.0001131 -2.4068e-10 -2.9355e-12 v Velocity[Z] -0.00011301 0.00012009 -4.7927e-11 -1.3888e-12 v ǁVelocityǁ 2.6276e-10 0.00012869 1.1679e-05 8.7922e-06 v Pressure -0.0015772 0.024593 0.0014221 -5.9518e-20 v k 4.4739e-10 0.00090564 0.00057934 0.0007418 v omega 11.724 1.0313e+05 2664.1 496.91 v TempK 288 342.14 294.4 291.31 v Density 1.205 1.205 1.205 1.205 v TurbVisc 5.2424e-15 9.3095e-05 5.4202e-05 7.1087e-05 v CourantNb 3.2485e-09 0.00018651 1.3876e-05 9.038e-06 v FourierNb 0.085163 0.6281 0.18171 0.15243 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.961 4.961 0.00057332 -5.9372e-07 v volume_forces[Z] -4.961 4.961 -0.00057323 7.0207e-07 v ǁvolume_forcesǁ 9.4791e-09 4.962 0.57949 0.29671 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.61 291.45 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014604 5.1675e-05 2.8789e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.085181 0.6281 0.18172 0.15244 INSTANT 0.904257000E+00 TIME STEP NUMBER 939 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.16368E-05 0.21946E-02 Friction velocity uk : 0.16381E-05 0.21946E-02 Dimensionless distance yplus : 0.10908E-04 0.14601E-01 Friction thermal sca. tstar : -0.13022E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.76608E-05 0.10255E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.16368E-05 0.21946E-02 Friction velocity uk : 0.16381E-05 0.21946E-02 Dimensionless distance yplus : 0.10908E-04 0.14601E-01 Friction thermal sca. tstar : -0.13022E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.76608E-05 0.10255E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.38977E-08 3 0.83977E-07 0.15088E-12 0.76295E+00 c Velocity[X] 0.33542E-32 c Velocity[Y] 0.75437E-13 c Velocity[Z] 0.75448E-13 c Pressure 0.62123E-14 16 0.48210E-07 0.48210E-07 0.83717E+00 c k 0.26844E-06 2 0.27042E-07 0.83201E-09 0.11802E+01 c omega 0.13153E+02 1 0.74501E-09 0.10246E+00 0.16664E-02 c TempK 0.94792E+02 1 0.66980E-07 0.14922E-01 0.13506E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.5786e-14 7.1957e-14 -8.9635e-18 -2.3465e-18 v Velocity[Y] -0.00012006 0.00011307 -2.3817e-10 -2.9325e-12 v Velocity[Z] -0.00011299 0.00012007 -5.0428e-11 -1.3887e-12 v ǁVelocityǁ 2.6346e-10 0.00012866 1.1682e-05 8.7976e-06 v Pressure -0.0015788 0.024605 0.001423 4.2065e-20 v k 4.4611e-10 0.00090472 0.00057864 0.00074094 v omega 11.713 1.0313e+05 2664.1 496.9 v TempK 288 342.14 294.41 291.31 v Density 1.205 1.205 1.205 1.205 v TurbVisc 5.2274e-15 9.3086e-05 5.4186e-05 7.1068e-05 v CourantNb 3.2505e-09 0.00018645 1.3876e-05 9.0412e-06 v FourierNb 0.085109 0.6281 0.18168 0.1524 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.961 4.961 0.0005735 -5.9394e-07 v volume_forces[Z] -4.961 4.961 -0.00057341 7.0231e-07 v ǁvolume_forcesǁ 9.499e-09 4.962 0.57967 0.29687 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.61 291.45 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014601 5.1664e-05 2.8783e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.085127 0.6281 0.18169 0.15241 INSTANT 0.905220000E+00 TIME STEP NUMBER 940 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19029E-05 0.21942E-02 Friction velocity uk : 0.19039E-05 0.21941E-02 Dimensionless distance yplus : 0.12678E-04 0.14598E-01 Friction thermal sca. tstar : -0.12947E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.89042E-05 0.10253E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19029E-05 0.21942E-02 Friction velocity uk : 0.19039E-05 0.21941E-02 Dimensionless distance yplus : 0.12678E-04 0.14598E-01 Friction thermal sca. tstar : -0.12947E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.89042E-05 0.10253E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.38992E-08 3 0.83822E-07 0.15052E-12 0.76191E+00 c Velocity[X] 0.33432E-32 c Velocity[Y] 0.75253E-13 c Velocity[Z] 0.75264E-13 c Pressure 0.62052E-14 16 0.48155E-07 0.48155E-07 0.83623E+00 c k 0.26814E-06 2 0.27003E-07 0.82865E-09 0.11791E+01 c omega 0.13153E+02 1 0.74328E-09 0.10207E+00 0.16633E-02 c TempK 0.94792E+02 1 0.66879E-07 0.14898E-01 0.13495E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.5744e-14 7.1923e-14 -8.9595e-18 -2.3455e-18 v Velocity[Y] -0.00012004 0.00011305 -2.3567e-10 -2.9296e-12 v Velocity[Z] -0.00011297 0.00012005 -5.2928e-11 -1.3885e-12 v ǁVelocityǁ 2.6431e-10 0.00012864 1.1686e-05 8.8029e-06 v Pressure -0.0015805 0.024618 0.0014238 1.3727e-20 v k 4.4484e-10 0.00090379 0.00057795 0.00074009 v omega 11.702 1.0313e+05 2664.1 496.89 v TempK 288 342.14 294.41 291.31 v Density 1.205 1.205 1.205 1.205 v TurbVisc 5.2125e-15 9.3076e-05 5.4171e-05 7.105e-05 v CourantNb 3.2524e-09 0.0001864 1.3877e-05 9.0444e-06 v FourierNb 0.085055 0.6281 0.18165 0.15237 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9611 4.9611 0.00057368 -5.9416e-07 v volume_forces[Z] -4.9611 4.9611 -0.00057359 7.0255e-07 v ǁvolume_forcesǁ 9.5242e-09 4.962 0.57985 0.29702 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.61 291.45 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014598 5.1653e-05 2.8776e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.085072 0.6281 0.18166 0.15238 INSTANT 0.906183000E+00 TIME STEP NUMBER 941 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.21365E-05 0.21937E-02 Friction velocity uk : 0.21374E-05 0.21937E-02 Dimensionless distance yplus : 0.14233E-04 0.14595E-01 Friction thermal sca. tstar : -0.12873E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.99963E-05 0.10250E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.21365E-05 0.21937E-02 Friction velocity uk : 0.21374E-05 0.21937E-02 Dimensionless distance yplus : 0.14233E-04 0.14595E-01 Friction thermal sca. tstar : -0.12873E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.99963E-05 0.10250E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.39006E-08 3 0.83647E-07 0.15015E-12 0.76086E+00 c Velocity[X] 0.33323E-32 c Velocity[Y] 0.75069E-13 c Velocity[Z] 0.75081E-13 c Pressure 0.61950E-14 16 0.48075E-07 0.48075E-07 0.83530E+00 c k 0.26784E-06 2 0.26963E-07 0.82532E-09 0.11781E+01 c omega 0.13153E+02 1 0.74157E-09 0.10168E+00 0.16601E-02 c TempK 0.94793E+02 1 0.66777E-07 0.14874E-01 0.13484E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.5701e-14 7.1889e-14 -8.9554e-18 -2.3446e-18 v Velocity[Y] -0.00012002 0.00011303 -2.3317e-10 -2.9267e-12 v Velocity[Z] -0.00011295 0.00012003 -5.5427e-11 -1.3884e-12 v ǁVelocityǁ 2.653e-10 0.00012862 1.1689e-05 8.8083e-06 v Pressure -0.0015821 0.024631 0.0014247 -6.7068e-20 v k 4.4358e-10 0.00090287 0.00057726 0.00073923 v omega 11.691 1.0313e+05 2664.1 496.88 v TempK 288 342.14 294.41 291.32 v Density 1.205 1.205 1.205 1.205 v TurbVisc 5.1977e-15 9.3067e-05 5.4155e-05 7.1031e-05 v CourantNb 3.2544e-09 0.00018634 1.3877e-05 9.0476e-06 v FourierNb 0.085001 0.6281 0.18162 0.15234 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9611 4.9611 0.00057386 -5.9438e-07 v volume_forces[Z] -4.9611 4.9611 -0.00057378 7.0278e-07 v ǁvolume_forcesǁ 9.5547e-09 4.9621 0.58003 0.29718 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.62 291.46 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014595 5.1642e-05 2.877e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.085018 0.6281 0.18163 0.15235 INSTANT 0.907146000E+00 TIME STEP NUMBER 942 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.23475E-05 0.21932E-02 Friction velocity uk : 0.23483E-05 0.21932E-02 Dimensionless distance yplus : 0.15637E-04 0.14592E-01 Friction thermal sca. tstar : -0.12802E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.10982E-04 0.10248E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.23475E-05 0.21932E-02 Friction velocity uk : 0.23483E-05 0.21932E-02 Dimensionless distance yplus : 0.15637E-04 0.14592E-01 Friction thermal sca. tstar : -0.12802E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.10982E-04 0.10248E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.39020E-08 3 0.83467E-07 0.14978E-12 0.75981E+00 c Velocity[X] 0.33213E-32 c Velocity[Y] 0.74886E-13 c Velocity[Z] 0.74897E-13 c Pressure 0.61896E-14 16 0.48032E-07 0.48032E-07 0.83437E+00 c k 0.26754E-06 2 0.26924E-07 0.82200E-09 0.11770E+01 c omega 0.13153E+02 1 0.73985E-09 0.10130E+00 0.16570E-02 c TempK 0.94793E+02 1 0.66677E-07 0.14851E-01 0.13473E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.5659e-14 7.1856e-14 -8.9514e-18 -2.3437e-18 v Velocity[Y] -0.00012 0.00011301 -2.3067e-10 -2.9238e-12 v Velocity[Z] -0.00011292 0.00012 -5.7924e-11 -1.3883e-12 v ǁVelocityǁ 2.6644e-10 0.00012859 1.1692e-05 8.8136e-06 v Pressure -0.0015838 0.024643 0.0014256 -2.6278e-20 v k 4.4231e-10 0.00090196 0.00057657 0.00073838 v omega 11.681 1.0313e+05 2664.1 496.88 v TempK 288 342.14 294.41 291.32 v Density 1.205 1.205 1.205 1.205 v TurbVisc 5.1829e-15 9.3058e-05 5.414e-05 7.1013e-05 v CourantNb 3.2563e-09 0.00018628 1.3878e-05 9.0508e-06 v FourierNb 0.084946 0.6281 0.18159 0.15231 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9611 4.9611 0.00057404 -5.946e-07 v volume_forces[Z] -4.9611 4.9611 -0.00057396 7.0302e-07 v ǁvolume_forcesǁ 9.5907e-09 4.9621 0.58021 0.29734 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.62 291.46 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014592 5.1632e-05 2.8764e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.084964 0.6281 0.1816 0.15232 INSTANT 0.908109000E+00 TIME STEP NUMBER 943 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.25414E-05 0.21928E-02 Friction velocity uk : 0.25421E-05 0.21927E-02 Dimensionless distance yplus : 0.16928E-04 0.14589E-01 Friction thermal sca. tstar : -0.12733E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.11889E-04 0.10246E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.25414E-05 0.21928E-02 Friction velocity uk : 0.25421E-05 0.21927E-02 Dimensionless distance yplus : 0.16928E-04 0.14589E-01 Friction thermal sca. tstar : -0.12733E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.11889E-04 0.10246E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.39034E-08 3 0.83308E-07 0.14942E-12 0.75877E+00 c Velocity[X] 0.33103E-32 c Velocity[Y] 0.74703E-13 c Velocity[Z] 0.74714E-13 c Pressure 0.61799E-14 16 0.47957E-07 0.47957E-07 0.83344E+00 c k 0.26724E-06 2 0.26885E-07 0.81869E-09 0.11760E+01 c omega 0.13153E+02 1 0.73814E-09 0.10092E+00 0.16538E-02 c TempK 0.94794E+02 1 0.66576E-07 0.14827E-01 0.13463E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.5616e-14 7.1822e-14 -8.9474e-18 -2.3427e-18 v Velocity[Y] -0.00011998 0.00011298 -2.2817e-10 -2.9209e-12 v Velocity[Z] -0.0001129 0.00011998 -6.0421e-11 -1.3881e-12 v ǁVelocityǁ 2.6773e-10 0.00012857 1.1696e-05 8.8189e-06 v Pressure -0.0015854 0.024656 0.0014264 5.2949e-21 v k 4.4106e-10 0.00090104 0.00057589 0.00073752 v omega 11.67 1.0313e+05 2664.1 496.87 v TempK 288 342.15 294.41 291.32 v Density 1.205 1.205 1.205 1.205 v TurbVisc 5.1681e-15 9.3049e-05 5.4125e-05 7.0994e-05 v CourantNb 3.2582e-09 0.00018623 1.3879e-05 9.0539e-06 v FourierNb 0.084893 0.6281 0.18156 0.15228 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9612 4.9612 0.00057423 -5.9482e-07 v volume_forces[Z] -4.9612 4.9612 -0.00057414 7.0326e-07 v ǁvolume_forcesǁ 9.6319e-09 4.9622 0.58039 0.29749 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.62 291.46 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014589 5.1621e-05 2.8757e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.08491 0.6281 0.18157 0.15228 INSTANT 0.909072000E+00 TIME STEP NUMBER 944 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.27219E-05 0.21923E-02 Friction velocity uk : 0.27225E-05 0.21923E-02 Dimensionless distance yplus : 0.18129E-04 0.14585E-01 Friction thermal sca. tstar : -0.12665E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.12733E-04 0.10244E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.27219E-05 0.21923E-02 Friction velocity uk : 0.27225E-05 0.21923E-02 Dimensionless distance yplus : 0.18129E-04 0.14585E-01 Friction thermal sca. tstar : -0.12665E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.12733E-04 0.10244E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.39048E-08 3 0.13091E-06 0.14905E-12 0.75772E+00 c Velocity[X] 0.32995E-32 c Velocity[Y] 0.74519E-13 c Velocity[Z] 0.74531E-13 c Pressure 0.61899E-14 16 0.48034E-07 0.48034E-07 0.83252E+00 c k 0.26694E-06 2 0.26846E-07 0.81541E-09 0.11749E+01 c omega 0.13153E+02 1 0.73644E-09 0.10053E+00 0.16507E-02 c TempK 0.94794E+02 1 0.66476E-07 0.14803E-01 0.13452E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.5574e-14 7.1789e-14 -8.9434e-18 -2.3418e-18 v Velocity[Y] -0.00011996 0.00011296 -2.2567e-10 -2.918e-12 v Velocity[Z] -0.00011288 0.00011996 -6.2916e-11 -1.388e-12 v ǁVelocityǁ 2.6916e-10 0.00012854 1.1699e-05 8.8243e-06 v Pressure -0.001587 0.024669 0.0014273 2.9024e-20 v k 4.398e-10 0.00090012 0.0005752 0.00073667 v omega 11.659 1.0313e+05 2664.1 496.86 v TempK 288 342.15 294.42 291.32 v Density 1.205 1.205 1.205 1.205 v TurbVisc 5.1534e-15 9.3039e-05 5.4109e-05 7.0976e-05 v CourantNb 3.2602e-09 0.00018617 1.3879e-05 9.0571e-06 v FourierNb 0.084839 0.6281 0.18153 0.15224 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9612 4.9612 0.00057441 -5.9504e-07 v volume_forces[Z] -4.9612 4.9612 -0.00057432 7.035e-07 v ǁvolume_forcesǁ 9.6784e-09 4.9622 0.58056 0.29765 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.62 291.46 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014585 5.161e-05 2.8751e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.084857 0.6281 0.18154 0.15225 INSTANT 0.910035000E+00 TIME STEP NUMBER 945 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.28915E-05 0.21918E-02 Friction velocity uk : 0.28921E-05 0.21918E-02 Dimensionless distance yplus : 0.19258E-04 0.14582E-01 Friction thermal sca. tstar : -0.12600E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.13526E-04 0.10242E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.28915E-05 0.21918E-02 Friction velocity uk : 0.28921E-05 0.21918E-02 Dimensionless distance yplus : 0.19258E-04 0.14582E-01 Friction thermal sca. tstar : -0.12600E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.13526E-04 0.10242E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.39063E-08 3 0.13499E-06 0.14868E-12 0.75668E+00 c Velocity[X] 0.32889E-32 c Velocity[Y] 0.74336E-13 c Velocity[Z] 0.74348E-13 c Pressure 0.62075E-14 16 0.48170E-07 0.48170E-07 0.83159E+00 c k 0.26665E-06 2 0.26807E-07 0.81214E-09 0.11739E+01 c omega 0.13153E+02 1 0.73474E-09 0.10015E+00 0.16476E-02 c TempK 0.94795E+02 1 0.66376E-07 0.14780E-01 0.13441E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.5532e-14 7.1755e-14 -8.9394e-18 -2.3409e-18 v Velocity[Y] -0.00011993 0.00011294 -2.2317e-10 -2.9151e-12 v Velocity[Z] -0.00011285 0.00011994 -6.541e-11 -1.3878e-12 v ǁVelocityǁ 2.7074e-10 0.00012852 1.1703e-05 8.8296e-06 v Pressure -0.0015887 0.024681 0.0014282 -2.5298e-20 v k 4.3856e-10 0.00089921 0.00057452 0.00073582 v omega 11.648 1.0313e+05 2664.1 496.85 v TempK 288 342.15 294.42 291.32 v Density 1.205 1.205 1.205 1.205 v TurbVisc 5.1388e-15 9.303e-05 5.4094e-05 7.0957e-05 v CourantNb 3.2621e-09 0.00018611 1.388e-05 9.0603e-06 v FourierNb 0.084785 0.6281 0.1815 0.15221 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9612 4.9613 0.00057459 -5.9526e-07 v volume_forces[Z] -4.9612 4.9613 -0.0005745 7.0373e-07 v ǁvolume_forcesǁ 9.7302e-09 4.9622 0.58074 0.29781 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.62 291.46 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014582 5.1599e-05 2.8744e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.084803 0.6281 0.18152 0.15222 INSTANT 0.910998000E+00 TIME STEP NUMBER 946 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.30520E-05 0.21914E-02 Friction velocity uk : 0.30526E-05 0.21913E-02 Dimensionless distance yplus : 0.20327E-04 0.14579E-01 Friction thermal sca. tstar : -0.12536E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.14276E-04 0.10240E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.30520E-05 0.21914E-02 Friction velocity uk : 0.30526E-05 0.21913E-02 Dimensionless distance yplus : 0.20327E-04 0.14579E-01 Friction thermal sca. tstar : -0.12536E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.14276E-04 0.10240E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.39077E-08 3 0.12581E-06 0.14832E-12 0.75563E+00 c Velocity[X] 0.32781E-32 c Velocity[Y] 0.74154E-13 c Velocity[Z] 0.74165E-13 c Pressure 0.61849E-14 16 0.47994E-07 0.47994E-07 0.83067E+00 c k 0.26635E-06 2 0.26769E-07 0.80888E-09 0.11728E+01 c omega 0.13153E+02 1 0.73305E-09 0.99776E-01 0.16445E-02 c TempK 0.94795E+02 1 0.66276E-07 0.14756E-01 0.13430E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.549e-14 7.1722e-14 -8.9354e-18 -2.3399e-18 v Velocity[Y] -0.00011991 0.00011292 -2.2067e-10 -2.9122e-12 v Velocity[Z] -0.00011283 0.00011992 -6.7902e-11 -1.3876e-12 v ǁVelocityǁ 2.7246e-10 0.0001285 1.1706e-05 8.8349e-06 v Pressure -0.0015903 0.024694 0.001429 1.4914e-19 v k 4.3732e-10 0.0008983 0.00057384 0.00073498 v omega 11.638 1.0313e+05 2664.1 496.84 v TempK 288 342.15 294.42 291.33 v Density 1.205 1.205 1.205 1.205 v TurbVisc 5.1242e-15 9.3021e-05 5.4079e-05 7.0939e-05 v CourantNb 3.264e-09 0.00018606 1.388e-05 9.0635e-06 v FourierNb 0.084732 0.6281 0.18147 0.15218 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9613 4.9613 0.00057477 -5.9548e-07 v volume_forces[Z] -4.9613 4.9613 -0.00057468 7.0397e-07 v ǁvolume_forcesǁ 9.7871e-09 4.9623 0.58092 0.29796 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.63 291.47 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014579 5.1589e-05 2.8738e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.084749 0.6281 0.18149 0.15219 INSTANT 0.911961000E+00 TIME STEP NUMBER 947 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.32048E-05 0.21909E-02 Friction velocity uk : 0.32054E-05 0.21909E-02 Dimensionless distance yplus : 0.21344E-04 0.14576E-01 Friction thermal sca. tstar : -0.12474E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.14991E-04 0.10237E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.32048E-05 0.21909E-02 Friction velocity uk : 0.32054E-05 0.21909E-02 Dimensionless distance yplus : 0.21344E-04 0.14576E-01 Friction thermal sca. tstar : -0.12474E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.14991E-04 0.10237E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.39091E-08 3 0.82670E-07 0.14795E-12 0.75459E+00 c Velocity[X] 0.32675E-32 c Velocity[Y] 0.73971E-13 c Velocity[Z] 0.73983E-13 c Pressure 0.61324E-14 16 0.47586E-07 0.47586E-07 0.82975E+00 c k 0.26606E-06 2 0.26730E-07 0.80564E-09 0.11718E+01 c omega 0.13153E+02 1 0.73137E-09 0.99400E-01 0.16413E-02 c TempK 0.94796E+02 1 0.66176E-07 0.14733E-01 0.13420E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.5448e-14 7.1689e-14 -8.9314e-18 -2.339e-18 v Velocity[Y] -0.00011989 0.00011289 -2.1817e-10 -2.9092e-12 v Velocity[Z] -0.00011281 0.0001199 -7.0393e-11 -1.3874e-12 v ǁVelocityǁ 2.7431e-10 0.00012847 1.1709e-05 8.8402e-06 v Pressure -0.001592 0.024706 0.0014299 -4.6281e-20 v k 4.3608e-10 0.00089739 0.00057316 0.00073413 v omega 11.627 1.0313e+05 2664.1 496.83 v TempK 288 342.15 294.42 291.33 v Density 1.205 1.205 1.205 1.205 v TurbVisc 5.1097e-15 9.3012e-05 5.4063e-05 7.0921e-05 v CourantNb 3.2659e-09 0.000186 1.3881e-05 9.0666e-06 v FourierNb 0.084678 0.6281 0.18144 0.15215 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9613 4.9613 0.00057495 -5.9569e-07 v volume_forces[Z] -4.9613 4.9613 -0.00057486 7.042e-07 v ǁvolume_forcesǁ 9.8493e-09 4.9623 0.5811 0.29812 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.63 291.47 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014576 5.1578e-05 2.8732e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.084696 0.6281 0.18146 0.15216 INSTANT 0.912924000E+00 TIME STEP NUMBER 948 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.33510E-05 0.21904E-02 Friction velocity uk : 0.33515E-05 0.21904E-02 Dimensionless distance yplus : 0.22318E-04 0.14573E-01 Friction thermal sca. tstar : -0.12414E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.15674E-04 0.10235E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.33510E-05 0.21904E-02 Friction velocity uk : 0.33515E-05 0.21904E-02 Dimensionless distance yplus : 0.22318E-04 0.14573E-01 Friction thermal sca. tstar : -0.12414E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.15674E-04 0.10235E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.39105E-08 3 0.82510E-07 0.14759E-12 0.75354E+00 c Velocity[X] 0.32569E-32 c Velocity[Y] 0.73789E-13 c Velocity[Z] 0.73801E-13 c Pressure 0.61530E-14 16 0.47745E-07 0.47745E-07 0.82883E+00 c k 0.26576E-06 2 0.26691E-07 0.80242E-09 0.11707E+01 c omega 0.13153E+02 1 0.72968E-09 0.99025E-01 0.16383E-02 c TempK 0.94796E+02 1 0.66077E-07 0.14710E-01 0.13409E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.5406e-14 7.1655e-14 -8.9275e-18 -2.3381e-18 v Velocity[Y] -0.00011987 0.00011287 -2.1567e-10 -2.9064e-12 v Velocity[Z] -0.00011279 0.00011987 -7.2884e-11 -1.3873e-12 v ǁVelocityǁ 2.7631e-10 0.00012845 1.1713e-05 8.8455e-06 v Pressure -0.0015936 0.024719 0.0014307 2.8533e-20 v k 4.3484e-10 0.00089648 0.00057248 0.00073329 v omega 11.617 1.0313e+05 2664.1 496.82 v TempK 288 342.15 294.42 291.33 v Density 1.205 1.205 1.205 1.205 v TurbVisc 5.0953e-15 9.3002e-05 5.4048e-05 7.0902e-05 v CourantNb 3.2678e-09 0.00018594 1.3881e-05 9.0698e-06 v FourierNb 0.084625 0.6281 0.18141 0.15212 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9614 4.9614 0.00057513 -5.9591e-07 v volume_forces[Z] -4.9614 4.9614 -0.00057504 7.0444e-07 v ǁvolume_forcesǁ 9.9165e-09 4.9623 0.58128 0.29827 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.63 291.47 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014573 5.1567e-05 2.8725e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.084641 0.6281 0.18143 0.15213 INSTANT 0.913887000E+00 TIME STEP NUMBER 949 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.34914E-05 0.21900E-02 Friction velocity uk : 0.34919E-05 0.21899E-02 Dimensionless distance yplus : 0.23252E-04 0.14570E-01 Friction thermal sca. tstar : -0.12355E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.16331E-04 0.10233E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.34914E-05 0.21900E-02 Friction velocity uk : 0.34919E-05 0.21899E-02 Dimensionless distance yplus : 0.23252E-04 0.14570E-01 Friction thermal sca. tstar : -0.12355E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.16331E-04 0.10233E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.39119E-08 3 0.82341E-07 0.14723E-12 0.75250E+00 c Velocity[X] 0.32464E-32 c Velocity[Y] 0.73607E-13 c Velocity[Z] 0.73618E-13 c Pressure 0.61202E-14 16 0.47491E-07 0.47491E-07 0.82792E+00 c k 0.26547E-06 2 0.26653E-07 0.79921E-09 0.11697E+01 c omega 0.13153E+02 1 0.72801E-09 0.98652E-01 0.16352E-02 c TempK 0.94797E+02 1 0.65978E-07 0.14686E-01 0.13398E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.5364e-14 7.1622e-14 -8.9235e-18 -2.3371e-18 v Velocity[Y] -0.00011985 0.00011285 -2.1317e-10 -2.9035e-12 v Velocity[Z] -0.00011276 0.00011985 -7.5373e-11 -1.3871e-12 v ǁVelocityǁ 2.7845e-10 0.00012843 1.1716e-05 8.8508e-06 v Pressure -0.0015953 0.024732 0.0014316 7.7266e-20 v k 4.3362e-10 0.00089558 0.0005718 0.00073244 v omega 11.606 1.0313e+05 2664 496.81 v TempK 288 342.15 294.43 291.33 v Density 1.205 1.205 1.205 1.205 v TurbVisc 5.0808e-15 9.2993e-05 5.4033e-05 7.0884e-05 v CourantNb 3.2719e-09 0.00018589 1.3882e-05 9.073e-06 v FourierNb 0.08457 0.6281 0.18138 0.15209 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9614 4.9614 0.0005753 -5.9613e-07 v volume_forces[Z] -4.9614 4.9614 -0.00057522 7.0467e-07 v ǁvolume_forcesǁ 9.9887e-09 4.9624 0.58145 0.29843 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.63 291.47 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.01457 5.1556e-05 2.8719e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.084578 0.6281 0.1814 0.1521 INSTANT 0.914850000E+00 TIME STEP NUMBER 950 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.36266E-05 0.21895E-02 Friction velocity uk : 0.36271E-05 0.21895E-02 Dimensionless distance yplus : 0.24152E-04 0.14567E-01 Friction thermal sca. tstar : -0.12298E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.16963E-04 0.10231E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.36266E-05 0.21895E-02 Friction velocity uk : 0.36271E-05 0.21895E-02 Dimensionless distance yplus : 0.24152E-04 0.14567E-01 Friction thermal sca. tstar : -0.12298E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.16963E-04 0.10231E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.39133E-08 3 0.82179E-07 0.14686E-12 0.75145E+00 c Velocity[X] 0.32358E-32 c Velocity[Y] 0.73425E-13 c Velocity[Z] 0.73437E-13 c Pressure 0.61356E-14 16 0.47610E-07 0.47610E-07 0.82700E+00 c k 0.26517E-06 2 0.26614E-07 0.79602E-09 0.11686E+01 c omega 0.13153E+02 1 0.72634E-09 0.98281E-01 0.16321E-02 c TempK 0.94798E+02 1 0.65879E-07 0.14663E-01 0.13387E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.5322e-14 7.1589e-14 -8.9195e-18 -2.3362e-18 v Velocity[Y] -0.00011983 0.00011283 -2.1067e-10 -2.9006e-12 v Velocity[Z] -0.00011274 0.00011983 -7.786e-11 -1.3869e-12 v ǁVelocityǁ 2.8071e-10 0.0001284 1.1719e-05 8.8561e-06 v Pressure -0.0015969 0.024744 0.0014325 3.9221e-21 v k 4.3239e-10 0.00089467 0.00057112 0.0007316 v omega 11.595 1.0313e+05 2664 496.8 v TempK 288 342.15 294.43 291.33 v Density 1.205 1.205 1.205 1.205 v TurbVisc 5.0665e-15 9.2984e-05 5.4017e-05 7.0866e-05 v CourantNb 3.2763e-09 0.00018583 1.3882e-05 9.0761e-06 v FourierNb 0.084507 0.6281 0.18136 0.15206 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9614 4.9615 0.00057548 -5.9635e-07 v volume_forces[Z] -4.9614 4.9615 -0.0005754 7.0491e-07 v ǁvolume_forcesǁ 1.0066e-08 4.9624 0.58163 0.29858 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.63 291.47 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014567 5.1546e-05 2.8713e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.084516 0.6281 0.18137 0.15207 INSTANT 0.915813000E+00 TIME STEP NUMBER 951 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.37572E-05 0.21890E-02 Friction velocity uk : 0.37577E-05 0.21890E-02 Dimensionless distance yplus : 0.25022E-04 0.14564E-01 Friction thermal sca. tstar : -0.12243E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.17574E-04 0.10229E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.37572E-05 0.21890E-02 Friction velocity uk : 0.37577E-05 0.21890E-02 Dimensionless distance yplus : 0.25022E-04 0.14564E-01 Friction thermal sca. tstar : -0.12243E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.17574E-04 0.10229E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.39148E-08 3 0.81998E-07 0.14650E-12 0.75041E+00 c Velocity[X] 0.32253E-32 c Velocity[Y] 0.73243E-13 c Velocity[Z] 0.73255E-13 c Pressure 0.60905E-14 16 0.47259E-07 0.47259E-07 0.82609E+00 c k 0.26488E-06 2 0.26576E-07 0.79285E-09 0.11676E+01 c omega 0.13153E+02 1 0.72467E-09 0.97912E-01 0.16290E-02 c TempK 0.94798E+02 1 0.65781E-07 0.14640E-01 0.13377E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.528e-14 7.1556e-14 -8.9156e-18 -2.3353e-18 v Velocity[Y] -0.0001198 0.00011281 -2.0817e-10 -2.8977e-12 v Velocity[Z] -0.00011272 0.00011981 -8.0346e-11 -1.3866e-12 v ǁVelocityǁ 2.8312e-10 0.00012838 1.1723e-05 8.8614e-06 v Pressure -0.0015986 0.024757 0.0014333 -5.9322e-20 v k 4.3117e-10 0.00089377 0.00057045 0.00073077 v omega 11.585 1.0313e+05 2664 496.79 v TempK 288 342.15 294.43 291.33 v Density 1.205 1.205 1.205 1.205 v TurbVisc 5.0522e-15 9.2975e-05 5.4002e-05 7.0847e-05 v CourantNb 3.2781e-09 0.00018578 1.3883e-05 9.0793e-06 v FourierNb 0.084445 0.6281 0.18133 0.15203 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9615 4.9615 0.00057566 -5.9656e-07 v volume_forces[Z] -4.9615 4.9615 -0.00057558 7.0514e-07 v ǁvolume_forcesǁ 1.0148e-08 4.9625 0.58181 0.29874 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.64 291.47 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014564 5.1535e-05 2.8706e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.084453 0.6281 0.18134 0.15204 INSTANT 0.916776000E+00 TIME STEP NUMBER 952 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.38837E-05 0.21886E-02 Friction velocity uk : 0.38841E-05 0.21886E-02 Dimensionless distance yplus : 0.25864E-04 0.14561E-01 Friction thermal sca. tstar : -0.12188E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.18165E-04 0.10227E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.38837E-05 0.21886E-02 Friction velocity uk : 0.38841E-05 0.21886E-02 Dimensionless distance yplus : 0.25864E-04 0.14561E-01 Friction thermal sca. tstar : -0.12188E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.18165E-04 0.10227E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.39162E-08 3 0.81839E-07 0.14613E-12 0.74936E+00 c Velocity[X] 0.32149E-32 c Velocity[Y] 0.73061E-13 c Velocity[Z] 0.73073E-13 c Pressure 0.60810E-14 16 0.47185E-07 0.47185E-07 0.82518E+00 c k 0.26459E-06 2 0.26538E-07 0.78969E-09 0.11666E+01 c omega 0.13153E+02 1 0.72301E-09 0.97544E-01 0.16260E-02 c TempK 0.94799E+02 1 0.65682E-07 0.14617E-01 0.13366E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.5238e-14 7.1523e-14 -8.9116e-18 -2.3344e-18 v Velocity[Y] -0.00011978 0.00011278 -2.0567e-10 -2.8948e-12 v Velocity[Z] -0.0001127 0.00011979 -8.2831e-11 -1.3864e-12 v ǁVelocityǁ 2.8565e-10 0.00012836 1.1726e-05 8.8666e-06 v Pressure -0.0016002 0.024769 0.0014342 -4.2163e-20 v k 4.2996e-10 0.00089287 0.00056977 0.00072993 v omega 11.574 1.0313e+05 2664 496.78 v TempK 288 342.15 294.43 291.34 v Density 1.205 1.205 1.205 1.205 v TurbVisc 5.038e-15 9.2966e-05 5.3987e-05 7.0829e-05 v CourantNb 3.28e-09 0.00018572 1.3884e-05 9.0824e-06 v FourierNb 0.084383 0.6281 0.1813 0.152 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9615 4.9615 0.00057584 -5.9678e-07 v volume_forces[Z] -4.9615 4.9615 -0.00057576 7.0538e-07 v ǁvolume_forcesǁ 1.0235e-08 4.9625 0.58199 0.29889 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.64 291.48 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014561 5.1524e-05 2.87e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.084391 0.6281 0.18131 0.15201 INSTANT 0.917739000E+00 TIME STEP NUMBER 953 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.40065E-05 0.21881E-02 Friction velocity uk : 0.40069E-05 0.21881E-02 Dimensionless distance yplus : 0.26682E-04 0.14558E-01 Friction thermal sca. tstar : -0.12136E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.18739E-04 0.10224E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.40065E-05 0.21881E-02 Friction velocity uk : 0.40069E-05 0.21881E-02 Dimensionless distance yplus : 0.26682E-04 0.14558E-01 Friction thermal sca. tstar : -0.12136E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.18739E-04 0.10224E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.39176E-08 3 0.81677E-07 0.14577E-12 0.74832E+00 c Velocity[X] 0.32045E-32 c Velocity[Y] 0.72880E-13 c Velocity[Z] 0.72892E-13 c Pressure 0.60712E-14 16 0.47109E-07 0.47109E-07 0.82427E+00 c k 0.26429E-06 2 0.26500E-07 0.78654E-09 0.11655E+01 c omega 0.13153E+02 1 0.72136E-09 0.97178E-01 0.16229E-02 c TempK 0.94799E+02 1 0.65584E-07 0.14594E-01 0.13355E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.5197e-14 7.149e-14 -8.9077e-18 -2.3335e-18 v Velocity[Y] -0.00011976 0.00011276 -2.0317e-10 -2.892e-12 v Velocity[Z] -0.00011267 0.00011977 -8.5315e-11 -1.3862e-12 v ǁVelocityǁ 2.883e-10 0.00012833 1.1729e-05 8.8719e-06 v Pressure -0.0016019 0.024782 0.001435 -8.7071e-20 v k 4.2875e-10 0.00089197 0.0005691 0.00072909 v omega 11.564 1.0313e+05 2664 496.77 v TempK 288 342.15 294.43 291.34 v Density 1.205 1.205 1.205 1.205 v TurbVisc 5.0238e-15 9.2956e-05 5.3972e-05 7.0811e-05 v CourantNb 3.2818e-09 0.00018566 1.3884e-05 9.0855e-06 v FourierNb 0.084321 0.6281 0.18127 0.15197 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9615 4.9616 0.00057602 -5.97e-07 v volume_forces[Z] -4.9615 4.9616 -0.00057593 7.0561e-07 v ǁvolume_forcesǁ 1.0326e-08 4.9625 0.58216 0.29905 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.64 291.48 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014558 5.1513e-05 2.8694e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.084329 0.6281 0.18128 0.15198 INSTANT 0.918702000E+00 TIME STEP NUMBER 954 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.41258E-05 0.21877E-02 Friction velocity uk : 0.41262E-05 0.21876E-02 Dimensionless distance yplus : 0.27476E-04 0.14555E-01 Friction thermal sca. tstar : -0.12085E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.19298E-04 0.10222E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.41258E-05 0.21877E-02 Friction velocity uk : 0.41262E-05 0.21876E-02 Dimensionless distance yplus : 0.27476E-04 0.14555E-01 Friction thermal sca. tstar : -0.12085E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.19298E-04 0.10222E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.39190E-08 3 0.81517E-07 0.14541E-12 0.74727E+00 c Velocity[X] 0.31942E-32 c Velocity[Y] 0.72698E-13 c Velocity[Z] 0.72710E-13 c Pressure 0.60652E-14 16 0.47062E-07 0.47062E-07 0.82336E+00 c k 0.26400E-06 2 0.26462E-07 0.78341E-09 0.11645E+01 c omega 0.13153E+02 1 0.71971E-09 0.96814E-01 0.16199E-02 c TempK 0.94800E+02 1 0.65486E-07 0.14571E-01 0.13345E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.5155e-14 7.1457e-14 -8.9037e-18 -2.3325e-18 v Velocity[Y] -0.00011974 0.00011274 -2.0067e-10 -2.8891e-12 v Velocity[Z] -0.00011265 0.00011974 -8.7797e-11 -1.3859e-12 v ǁVelocityǁ 2.9109e-10 0.00012831 1.1733e-05 8.8771e-06 v Pressure -0.0016035 0.024794 0.0014359 1.1472e-19 v k 4.2755e-10 0.00089107 0.00056843 0.00072826 v omega 11.553 1.0313e+05 2664 496.76 v TempK 288 342.15 294.44 291.34 v Density 1.205 1.205 1.205 1.205 v TurbVisc 5.0096e-15 9.2947e-05 5.3957e-05 7.0793e-05 v CourantNb 3.2836e-09 0.00018561 1.3885e-05 9.0887e-06 v FourierNb 0.084259 0.6281 0.18124 0.15194 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9616 4.9616 0.0005762 -5.9721e-07 v volume_forces[Z] -4.9616 4.9616 -0.00057611 7.0584e-07 v ǁvolume_forcesǁ 1.0422e-08 4.9626 0.58234 0.2992 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.64 291.48 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014555 5.1503e-05 2.8687e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.084267 0.6281 0.18125 0.15194 INSTANT 0.919665000E+00 TIME STEP NUMBER 955 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.42421E-05 0.21872E-02 Friction velocity uk : 0.42425E-05 0.21872E-02 Dimensionless distance yplus : 0.28250E-04 0.14552E-01 Friction thermal sca. tstar : -0.12035E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.19841E-04 0.10220E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.42421E-05 0.21872E-02 Friction velocity uk : 0.42425E-05 0.21872E-02 Dimensionless distance yplus : 0.28250E-04 0.14552E-01 Friction thermal sca. tstar : -0.12035E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.19841E-04 0.10220E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.39204E-08 3 0.81359E-07 0.14505E-12 0.74623E+00 c Velocity[X] 0.31839E-32 c Velocity[Y] 0.72517E-13 c Velocity[Z] 0.72529E-13 c Pressure 0.60540E-14 16 0.46974E-07 0.46974E-07 0.82246E+00 c k 0.26371E-06 2 0.26424E-07 0.78030E-09 0.11635E+01 c omega 0.13153E+02 1 0.71806E-09 0.96451E-01 0.16168E-02 c TempK 0.94800E+02 1 0.65389E-07 0.14548E-01 0.13334E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.5114e-14 7.1424e-14 -8.8998e-18 -2.3316e-18 v Velocity[Y] -0.00011972 0.00011272 -1.9818e-10 -2.8863e-12 v Velocity[Z] -0.00011263 0.00011972 -9.0277e-11 -1.3857e-12 v ǁVelocityǁ 2.9399e-10 0.00012828 1.1736e-05 8.8824e-06 v Pressure -0.0016051 0.024807 0.0014367 -4.4124e-20 v k 4.2635e-10 0.00089018 0.00056776 0.00072743 v omega 11.543 1.0313e+05 2664 496.76 v TempK 288 342.15 294.44 291.34 v Density 1.205 1.205 1.205 1.205 v TurbVisc 4.9956e-15 9.2938e-05 5.3941e-05 7.0774e-05 v CourantNb 3.2855e-09 0.00018555 1.3885e-05 9.0918e-06 v FourierNb 0.084197 0.6281 0.18121 0.1519 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9616 4.9616 0.00057638 -5.9743e-07 v volume_forces[Z] -4.9616 4.9616 -0.00057629 7.0607e-07 v ǁvolume_forcesǁ 1.0523e-08 4.9626 0.58252 0.29936 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.64 291.48 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014552 5.1492e-05 2.8681e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.084205 0.6281 0.18122 0.15191 INSTANT 0.920628000E+00 TIME STEP NUMBER 956 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.43555E-05 0.21868E-02 Friction velocity uk : 0.43559E-05 0.21867E-02 Dimensionless distance yplus : 0.29005E-04 0.14549E-01 Friction thermal sca. tstar : -0.11986E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.20371E-04 0.10218E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.43555E-05 0.21868E-02 Friction velocity uk : 0.43559E-05 0.21867E-02 Dimensionless distance yplus : 0.29005E-04 0.14549E-01 Friction thermal sca. tstar : -0.11986E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.20371E-04 0.10218E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.39218E-08 3 0.81199E-07 0.14468E-12 0.74518E+00 c Velocity[X] 0.31736E-32 c Velocity[Y] 0.72336E-13 c Velocity[Z] 0.72348E-13 c Pressure 0.60435E-14 16 0.46892E-07 0.46892E-07 0.82156E+00 c k 0.26342E-06 2 0.26386E-07 0.77720E-09 0.11625E+01 c omega 0.13153E+02 1 0.71642E-09 0.96090E-01 0.16138E-02 c TempK 0.94801E+02 1 0.65292E-07 0.14525E-01 0.13324E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.5072e-14 7.1391e-14 -8.8959e-18 -2.3307e-18 v Velocity[Y] -0.00011969 0.00011269 -1.9568e-10 -2.8835e-12 v Velocity[Z] -0.00011261 0.0001197 -9.2756e-11 -1.3854e-12 v ǁVelocityǁ 2.9701e-10 0.00012826 1.1739e-05 8.8876e-06 v Pressure -0.0016068 0.024819 0.0014376 -1.9709e-20 v k 4.2515e-10 0.00088928 0.00056709 0.0007266 v omega 11.532 1.0313e+05 2664 496.75 v TempK 288 342.15 294.44 291.34 v Density 1.205 1.205 1.205 1.205 v TurbVisc 4.9815e-15 9.2929e-05 5.3926e-05 7.0756e-05 v CourantNb 3.2873e-09 0.0001855 1.3886e-05 9.0949e-06 v FourierNb 0.084135 0.6281 0.18118 0.15187 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9617 4.9617 0.00057656 -5.9764e-07 v volume_forces[Z] -4.9617 4.9617 -0.00057647 7.0631e-07 v ǁvolume_forcesǁ 1.0628e-08 4.9626 0.58269 0.29951 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.65 291.48 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014549 5.1481e-05 2.8675e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.084143 0.6281 0.1812 0.15188 INSTANT 0.921591000E+00 TIME STEP NUMBER 957 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.44662E-05 0.21863E-02 Friction velocity uk : 0.44666E-05 0.21863E-02 Dimensionless distance yplus : 0.29743E-04 0.14546E-01 Friction thermal sca. tstar : -0.11939E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.20889E-04 0.10216E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.44662E-05 0.21863E-02 Friction velocity uk : 0.44666E-05 0.21863E-02 Dimensionless distance yplus : 0.29743E-04 0.14546E-01 Friction thermal sca. tstar : -0.11939E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.20889E-04 0.10216E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.39232E-08 3 0.81037E-07 0.14432E-12 0.74414E+00 c Velocity[X] 0.31634E-32 c Velocity[Y] 0.72155E-13 c Velocity[Z] 0.72167E-13 c Pressure 0.60341E-14 16 0.46819E-07 0.46819E-07 0.82066E+00 c k 0.26313E-06 2 0.26348E-07 0.77412E-09 0.11614E+01 c omega 0.13153E+02 1 0.71479E-09 0.95731E-01 0.16108E-02 c TempK 0.94801E+02 1 0.65195E-07 0.14502E-01 0.13313E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.5031e-14 7.1359e-14 -8.892e-18 -2.3298e-18 v Velocity[Y] -0.00011967 0.00011267 -1.9318e-10 -2.8807e-12 v Velocity[Z] -0.00011258 0.00011968 -9.5233e-11 -1.3851e-12 v ǁVelocityǁ 3.0016e-10 0.00012824 1.1743e-05 8.8928e-06 v Pressure -0.0016084 0.024832 0.0014385 1.2717e-19 v k 4.2396e-10 0.00088839 0.00056642 0.00072577 v omega 11.522 1.0313e+05 2664 496.74 v TempK 288 342.15 294.44 291.34 v Density 1.205 1.205 1.205 1.205 v TurbVisc 4.9676e-15 9.292e-05 5.3911e-05 7.0738e-05 v CourantNb 3.2891e-09 0.00018544 1.3886e-05 9.098e-06 v FourierNb 0.084073 0.6281 0.18115 0.15184 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9617 4.9617 0.00057674 -5.9786e-07 v volume_forces[Z] -4.9617 4.9617 -0.00057665 7.0654e-07 v ǁvolume_forcesǁ 1.0737e-08 4.9627 0.58287 0.29967 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.65 291.48 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014546 5.1471e-05 2.8668e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.084082 0.6281 0.18117 0.15185 INSTANT 0.922554000E+00 TIME STEP NUMBER 958 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.45745E-05 0.21858E-02 Friction velocity uk : 0.45749E-05 0.21858E-02 Dimensionless distance yplus : 0.30464E-04 0.14543E-01 Friction thermal sca. tstar : -0.11893E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.21396E-04 0.10214E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.45745E-05 0.21858E-02 Friction velocity uk : 0.45749E-05 0.21858E-02 Dimensionless distance yplus : 0.30464E-04 0.14543E-01 Friction thermal sca. tstar : -0.11893E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.21396E-04 0.10214E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.39246E-08 3 0.80882E-07 0.14396E-12 0.74310E+00 c Velocity[X] 0.31532E-32 c Velocity[Y] 0.71974E-13 c Velocity[Z] 0.71987E-13 c Pressure 0.60253E-14 16 0.46750E-07 0.46750E-07 0.81976E+00 c k 0.26284E-06 2 0.26310E-07 0.77105E-09 0.11604E+01 c omega 0.13153E+02 1 0.71316E-09 0.95373E-01 0.16078E-02 c TempK 0.94802E+02 1 0.65098E-07 0.14480E-01 0.13303E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.4989e-14 7.1326e-14 -8.8881e-18 -2.3289e-18 v Velocity[Y] -0.00011965 0.00011265 -1.9069e-10 -2.8779e-12 v Velocity[Z] -0.00011256 0.00011966 -9.7709e-11 -1.3849e-12 v ǁVelocityǁ 3.0341e-10 0.00012821 1.1746e-05 8.8981e-06 v Pressure -0.0016101 0.024845 0.0014393 6.0793e-21 v k 4.2277e-10 0.0008875 0.00056576 0.00072494 v omega 11.511 1.0313e+05 2664 496.73 v TempK 288 342.15 294.44 291.35 v Density 1.205 1.205 1.205 1.205 v TurbVisc 4.9537e-15 9.2911e-05 5.3896e-05 7.072e-05 v CourantNb 3.2909e-09 0.00018539 1.3887e-05 9.1012e-06 v FourierNb 0.084012 0.6281 0.18112 0.15181 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9617 4.9617 0.00057691 -5.9807e-07 v volume_forces[Z] -4.9617 4.9617 -0.00057683 7.0677e-07 v ǁvolume_forcesǁ 1.0851e-08 4.9627 0.58305 0.29982 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.65 291.49 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014543 5.146e-05 2.8662e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.08402 0.6281 0.18114 0.15182 INSTANT 0.923517000E+00 TIME STEP NUMBER 959 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.46805E-05 0.21854E-02 Friction velocity uk : 0.46809E-05 0.21854E-02 Dimensionless distance yplus : 0.31169E-04 0.14539E-01 Friction thermal sca. tstar : -0.11848E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.21891E-04 0.10212E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.46805E-05 0.21854E-02 Friction velocity uk : 0.46809E-05 0.21854E-02 Dimensionless distance yplus : 0.31169E-04 0.14539E-01 Friction thermal sca. tstar : -0.11848E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.21891E-04 0.10212E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.39260E-08 3 0.80723E-07 0.14360E-12 0.74205E+00 c Velocity[X] 0.31431E-32 c Velocity[Y] 0.71794E-13 c Velocity[Z] 0.71806E-13 c Pressure 0.60190E-14 16 0.46701E-07 0.46701E-07 0.81886E+00 c k 0.26255E-06 2 0.26273E-07 0.76799E-09 0.11594E+01 c omega 0.13153E+02 1 0.71153E-09 0.95018E-01 0.16048E-02 c TempK 0.94802E+02 1 0.65001E-07 0.14457E-01 0.13292E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.4948e-14 7.1293e-14 -8.8842e-18 -2.328e-18 v Velocity[Y] -0.00011963 0.00011263 -1.8819e-10 -2.8751e-12 v Velocity[Z] -0.00011254 0.00011963 -1.0018e-10 -1.3846e-12 v ǁVelocityǁ 3.0678e-10 0.00012819 1.1749e-05 8.9033e-06 v Pressure -0.0016117 0.024857 0.0014402 -5.638e-20 v k 4.2159e-10 0.00088661 0.00056509 0.00072412 v omega 11.501 1.0313e+05 2664 496.72 v TempK 288 342.15 294.45 291.35 v Density 1.205 1.205 1.205 1.205 v TurbVisc 4.9398e-15 9.2902e-05 5.3881e-05 7.0702e-05 v CourantNb 3.2927e-09 0.00018533 1.3887e-05 9.1043e-06 v FourierNb 0.083951 0.6281 0.1811 0.15178 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9618 4.9618 0.00057709 -5.9828e-07 v volume_forces[Z] -4.9618 4.9618 -0.00057701 7.07e-07 v ǁvolume_forcesǁ 1.0968e-08 4.9628 0.58322 0.29998 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.65 291.49 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014539 5.1449e-05 2.8656e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.083959 0.6281 0.18111 0.15179 INSTANT 0.924480000E+00 TIME STEP NUMBER 960 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.47844E-05 0.21849E-02 Friction velocity uk : 0.47847E-05 0.21849E-02 Dimensionless distance yplus : 0.31861E-04 0.14536E-01 Friction thermal sca. tstar : -0.11805E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.22377E-04 0.10209E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.47844E-05 0.21849E-02 Friction velocity uk : 0.47847E-05 0.21849E-02 Dimensionless distance yplus : 0.31861E-04 0.14536E-01 Friction thermal sca. tstar : -0.11805E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.22377E-04 0.10209E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.39274E-08 3 0.80565E-07 0.14324E-12 0.74101E+00 c Velocity[X] 0.31330E-32 c Velocity[Y] 0.71613E-13 c Velocity[Z] 0.71626E-13 c Pressure 0.60068E-14 16 0.46606E-07 0.46606E-07 0.81797E+00 c k 0.26226E-06 2 0.26235E-07 0.76496E-09 0.11584E+01 c omega 0.13153E+02 1 0.70991E-09 0.94663E-01 0.16018E-02 c TempK 0.94803E+02 1 0.64905E-07 0.14434E-01 0.13282E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.4907e-14 7.1261e-14 -8.8803e-18 -2.3271e-18 v Velocity[Y] -0.00011961 0.00011261 -1.857e-10 -2.8723e-12 v Velocity[Z] -0.00011252 0.00011961 -1.0266e-10 -1.3843e-12 v ǁVelocityǁ 3.1025e-10 0.00012816 1.1753e-05 8.9085e-06 v Pressure -0.0016134 0.02487 0.001441 9.972e-20 v k 4.2041e-10 0.00088572 0.00056443 0.00072329 v omega 11.491 1.0313e+05 2664 496.71 v TempK 288 342.15 294.45 291.35 v Density 1.205 1.205 1.205 1.205 v TurbVisc 4.926e-15 9.2892e-05 5.3866e-05 7.0683e-05 v CourantNb 3.2945e-09 0.00018528 1.3888e-05 9.1074e-06 v FourierNb 0.083889 0.6281 0.18107 0.15175 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9618 4.9618 0.00057727 -5.985e-07 v volume_forces[Z] -4.9618 4.9618 -0.00057718 7.0723e-07 v ǁvolume_forcesǁ 1.109e-08 4.9628 0.5834 0.30013 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.65 291.49 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014536 5.1439e-05 2.8649e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.083898 0.6281 0.18108 0.15176 INSTANT 0.925443000E+00 TIME STEP NUMBER 961 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.48863E-05 0.21845E-02 Friction velocity uk : 0.48866E-05 0.21844E-02 Dimensionless distance yplus : 0.32540E-04 0.14533E-01 Friction thermal sca. tstar : -0.11762E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.22854E-04 0.10207E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.48863E-05 0.21845E-02 Friction velocity uk : 0.48866E-05 0.21844E-02 Dimensionless distance yplus : 0.32540E-04 0.14533E-01 Friction thermal sca. tstar : -0.11762E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.22854E-04 0.10207E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.39288E-08 3 0.80407E-07 0.14288E-12 0.73996E+00 c Velocity[X] 0.31230E-32 c Velocity[Y] 0.71433E-13 c Velocity[Z] 0.71446E-13 c Pressure 0.59984E-14 16 0.46540E-07 0.46540E-07 0.81707E+00 c k 0.26198E-06 2 0.26198E-07 0.76193E-09 0.11573E+01 c omega 0.13153E+02 1 0.70830E-09 0.94311E-01 0.15988E-02 c TempK 0.94803E+02 1 0.64809E-07 0.14412E-01 0.13271E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.4866e-14 7.1228e-14 -8.8764e-18 -2.3262e-18 v Velocity[Y] -0.00011959 0.00011258 -1.832e-10 -2.8696e-12 v Velocity[Z] -0.00011249 0.00011959 -1.0513e-10 -1.384e-12 v ǁVelocityǁ 3.1383e-10 0.00012814 1.1756e-05 8.9137e-06 v Pressure -0.001615 0.024882 0.0014419 -1.4982e-19 v k 4.1924e-10 0.00088484 0.00056377 0.00072247 v omega 11.48 1.0313e+05 2664 496.7 v TempK 288 342.15 294.45 291.35 v Density 1.205 1.205 1.205 1.205 v TurbVisc 4.9122e-15 9.2883e-05 5.3851e-05 7.0665e-05 v CourantNb 3.2963e-09 0.00018522 1.3888e-05 9.1105e-06 v FourierNb 0.083828 0.6281 0.18104 0.15172 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9618 4.9619 0.00057745 -5.9871e-07 v volume_forces[Z] -4.9618 4.9619 -0.00057736 7.0746e-07 v ǁvolume_forcesǁ 1.1216e-08 4.9628 0.58357 0.30029 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.66 291.49 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014533 5.1428e-05 2.8643e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.083837 0.6281 0.18105 0.15173 INSTANT 0.926406000E+00 TIME STEP NUMBER 962 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.49863E-05 0.21840E-02 Friction velocity uk : 0.49866E-05 0.21840E-02 Dimensionless distance yplus : 0.33205E-04 0.14530E-01 Friction thermal sca. tstar : -0.11721E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.23321E-04 0.10205E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.49863E-05 0.21840E-02 Friction velocity uk : 0.49866E-05 0.21840E-02 Dimensionless distance yplus : 0.33205E-04 0.14530E-01 Friction thermal sca. tstar : -0.11721E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.23321E-04 0.10205E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.39302E-08 3 0.80249E-07 0.14252E-12 0.73892E+00 c Velocity[X] 0.31130E-32 c Velocity[Y] 0.71253E-13 c Velocity[Z] 0.71266E-13 c Pressure 0.59884E-14 16 0.46462E-07 0.46462E-07 0.81618E+00 c k 0.26169E-06 2 0.26161E-07 0.75892E-09 0.11563E+01 c omega 0.13153E+02 1 0.70669E-09 0.93960E-01 0.15958E-02 c TempK 0.94804E+02 1 0.64713E-07 0.14389E-01 0.13261E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.4825e-14 7.1196e-14 -8.8725e-18 -2.3253e-18 v Velocity[Y] -0.00011956 0.00011256 -1.8071e-10 -2.8668e-12 v Velocity[Z] -0.00011247 0.00011957 -1.076e-10 -1.3837e-12 v ǁVelocityǁ 3.1751e-10 0.00012812 1.1759e-05 8.9189e-06 v Pressure -0.0016167 0.024894 0.0014427 5.7263e-20 v k 4.1807e-10 0.00088395 0.00056311 0.00072165 v omega 11.47 1.0313e+05 2664 496.69 v TempK 288 342.15 294.45 291.35 v Density 1.205 1.205 1.205 1.205 v TurbVisc 4.8985e-15 9.2874e-05 5.3836e-05 7.0647e-05 v CourantNb 3.2981e-09 0.00018517 1.3889e-05 9.1136e-06 v FourierNb 0.083768 0.6281 0.18101 0.15169 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9619 4.9619 0.00057763 -5.9892e-07 v volume_forces[Z] -4.9619 4.9619 -0.00057754 7.0769e-07 v ǁvolume_forcesǁ 1.1345e-08 4.9629 0.58375 0.30044 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.66 291.49 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.01453 5.1418e-05 2.8637e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.083776 0.6281 0.18102 0.1517 INSTANT 0.927369000E+00 TIME STEP NUMBER 963 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.50846E-05 0.21836E-02 Friction velocity uk : 0.50849E-05 0.21835E-02 Dimensionless distance yplus : 0.33860E-04 0.14527E-01 Friction thermal sca. tstar : -0.11680E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.23781E-04 0.10203E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.50846E-05 0.21836E-02 Friction velocity uk : 0.50849E-05 0.21835E-02 Dimensionless distance yplus : 0.33860E-04 0.14527E-01 Friction thermal sca. tstar : -0.11680E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.23781E-04 0.10203E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.39316E-08 3 0.80094E-07 0.14216E-12 0.73788E+00 c Velocity[X] 0.31030E-32 c Velocity[Y] 0.71073E-13 c Velocity[Z] 0.71086E-13 c Pressure 0.59801E-14 16 0.46397E-07 0.46397E-07 0.81529E+00 c k 0.26140E-06 2 0.26123E-07 0.75593E-09 0.11553E+01 c omega 0.13153E+02 1 0.70509E-09 0.93610E-01 0.15928E-02 c TempK 0.94804E+02 1 0.64617E-07 0.14367E-01 0.13250E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.4784e-14 7.1163e-14 -8.8686e-18 -2.3244e-18 v Velocity[Y] -0.00011954 0.00011254 -1.7822e-10 -2.864e-12 v Velocity[Z] -0.00011245 0.00011955 -1.1007e-10 -1.3834e-12 v ǁVelocityǁ 3.213e-10 0.00012809 1.1762e-05 8.9241e-06 v Pressure -0.0016183 0.024907 0.0014436 3.373e-20 v k 4.1691e-10 0.00088307 0.00056245 0.00072083 v omega 11.46 1.0313e+05 2663.9 496.68 v TempK 288 342.15 294.45 291.36 v Density 1.205 1.205 1.205 1.205 v TurbVisc 4.8848e-15 9.2865e-05 5.382e-05 7.0629e-05 v CourantNb 3.2998e-09 0.00018511 1.389e-05 9.1167e-06 v FourierNb 0.083707 0.6281 0.18098 0.15166 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9619 4.9619 0.0005778 -5.9914e-07 v volume_forces[Z] -4.9619 4.9619 -0.00057772 7.0792e-07 v ǁvolume_forcesǁ 1.1478e-08 4.9629 0.58392 0.3006 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.66 291.5 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014527 5.1407e-05 2.863e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.083715 0.6281 0.181 0.15167 INSTANT 0.928332000E+00 TIME STEP NUMBER 964 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.51812E-05 0.21831E-02 Friction velocity uk : 0.51814E-05 0.21831E-02 Dimensionless distance yplus : 0.34503E-04 0.14524E-01 Friction thermal sca. tstar : -0.11641E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.24232E-04 0.10201E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.51812E-05 0.21831E-02 Friction velocity uk : 0.51814E-05 0.21831E-02 Dimensionless distance yplus : 0.34503E-04 0.14524E-01 Friction thermal sca. tstar : -0.11641E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.24232E-04 0.10201E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.39330E-08 3 0.79937E-07 0.14180E-12 0.73683E+00 c Velocity[X] 0.30931E-32 c Velocity[Y] 0.70894E-13 c Velocity[Z] 0.70906E-13 c Pressure 0.59702E-14 16 0.46320E-07 0.46320E-07 0.81441E+00 c k 0.26112E-06 2 0.26086E-07 0.75295E-09 0.11543E+01 c omega 0.13153E+02 1 0.70349E-09 0.93263E-01 0.15899E-02 c TempK 0.94805E+02 1 0.64522E-07 0.14344E-01 0.13240E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.4743e-14 7.1131e-14 -8.8647e-18 -2.3235e-18 v Velocity[Y] -0.00011952 0.00011252 -1.7573e-10 -2.8613e-12 v Velocity[Z] -0.00011243 0.00011952 -1.1253e-10 -1.3831e-12 v ǁVelocityǁ 3.2518e-10 0.00012807 1.1766e-05 8.9292e-06 v Pressure -0.0016199 0.024919 0.0014444 -5.2066e-20 v k 4.1575e-10 0.00088219 0.00056179 0.00072001 v omega 11.449 1.0313e+05 2663.9 496.67 v TempK 288 342.15 294.46 291.36 v Density 1.205 1.205 1.205 1.205 v TurbVisc 4.8712e-15 9.2856e-05 5.3805e-05 7.0611e-05 v CourantNb 3.3016e-09 0.00018506 1.389e-05 9.1198e-06 v FourierNb 0.083646 0.6281 0.18095 0.15163 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.962 4.962 0.00057798 -5.9935e-07 v volume_forces[Z] -4.962 4.962 -0.0005779 7.0815e-07 v ǁvolume_forcesǁ 1.1615e-08 4.9629 0.5841 0.30075 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.66 291.5 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014524 5.1396e-05 2.8624e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.083654 0.6281 0.18097 0.15164 INSTANT 0.929295000E+00 TIME STEP NUMBER 965 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.52762E-05 0.21826E-02 Friction velocity uk : 0.52764E-05 0.21826E-02 Dimensionless distance yplus : 0.35135E-04 0.14521E-01 Friction thermal sca. tstar : -0.11603E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.24677E-04 0.10199E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.52762E-05 0.21826E-02 Friction velocity uk : 0.52764E-05 0.21826E-02 Dimensionless distance yplus : 0.35135E-04 0.14521E-01 Friction thermal sca. tstar : -0.11603E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.24677E-04 0.10199E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.39344E-08 3 0.79782E-07 0.14144E-12 0.73579E+00 c Velocity[X] 0.30832E-32 c Velocity[Y] 0.70714E-13 c Velocity[Z] 0.70727E-13 c Pressure 0.59612E-14 16 0.46249E-07 0.46249E-07 0.81352E+00 c k 0.26083E-06 2 0.26049E-07 0.74998E-09 0.11533E+01 c omega 0.13153E+02 1 0.70189E-09 0.92916E-01 0.15869E-02 c TempK 0.94805E+02 1 0.64427E-07 0.14322E-01 0.13230E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.4702e-14 7.1098e-14 -8.8609e-18 -2.3226e-18 v Velocity[Y] -0.0001195 0.0001125 -1.7323e-10 -2.8586e-12 v Velocity[Z] -0.0001124 0.0001195 -1.15e-10 -1.3828e-12 v ǁVelocityǁ 3.2916e-10 0.00012805 1.1769e-05 8.9344e-06 v Pressure -0.0016216 0.024932 0.0014453 3.8927e-20 v k 4.1459e-10 0.00088131 0.00056114 0.0007192 v omega 11.439 1.0313e+05 2663.9 496.67 v TempK 288 342.15 294.46 291.36 v Density 1.205 1.205 1.205 1.205 v TurbVisc 4.8577e-15 9.2847e-05 5.379e-05 7.0593e-05 v CourantNb 3.3034e-09 0.000185 1.3891e-05 9.1228e-06 v FourierNb 0.083586 0.6281 0.18092 0.1516 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.962 4.962 0.00057816 -5.9956e-07 v volume_forces[Z] -4.962 4.962 -0.00057807 7.0838e-07 v ǁvolume_forcesǁ 1.1755e-08 4.963 0.58428 0.30091 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.66 291.5 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014521 5.1386e-05 2.8618e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.083594 0.6281 0.18094 0.15161 INSTANT 0.930258000E+00 TIME STEP NUMBER 966 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.53697E-05 0.21822E-02 Friction velocity uk : 0.53700E-05 0.21822E-02 Dimensionless distance yplus : 0.35758E-04 0.14518E-01 Friction thermal sca. tstar : -0.11565E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.25114E-04 0.10197E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.53697E-05 0.21822E-02 Friction velocity uk : 0.53700E-05 0.21822E-02 Dimensionless distance yplus : 0.35758E-04 0.14518E-01 Friction thermal sca. tstar : -0.11565E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.25114E-04 0.10197E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.39357E-08 3 0.79629E-07 0.14108E-12 0.73475E+00 c Velocity[X] 0.30734E-32 c Velocity[Y] 0.70535E-13 c Velocity[Z] 0.70548E-13 c Pressure 0.59540E-14 16 0.46193E-07 0.46193E-07 0.81264E+00 c k 0.26055E-06 2 0.26012E-07 0.74703E-09 0.11523E+01 c omega 0.13153E+02 1 0.70030E-09 0.92572E-01 0.15840E-02 c TempK 0.94806E+02 1 0.64332E-07 0.14300E-01 0.13219E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.4661e-14 7.1066e-14 -8.857e-18 -2.3217e-18 v Velocity[Y] -0.00011948 0.00011247 -1.7074e-10 -2.8559e-12 v Velocity[Z] -0.00011238 0.00011948 -1.1746e-10 -1.3825e-12 v ǁVelocityǁ 3.3323e-10 0.00012802 1.1772e-05 8.9396e-06 v Pressure -0.0016232 0.024944 0.0014461 -4.0006e-20 v k 4.1344e-10 0.00088043 0.00056048 0.00071838 v omega 11.429 1.0313e+05 2663.9 496.66 v TempK 288 342.15 294.46 291.36 v Density 1.205 1.205 1.205 1.205 v TurbVisc 4.8442e-15 9.2838e-05 5.3775e-05 7.0575e-05 v CourantNb 3.3051e-09 0.00018495 1.3891e-05 9.1259e-06 v FourierNb 0.083525 0.6281 0.1809 0.15157 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.962 4.962 0.00057833 -5.9977e-07 v volume_forces[Z] -4.962 4.962 -0.00057825 7.086e-07 v ǁvolume_forcesǁ 1.1899e-08 4.963 0.58445 0.30106 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.67 291.5 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014518 5.1375e-05 2.8612e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.083534 0.6281 0.18091 0.15158 INSTANT 0.931221000E+00 TIME STEP NUMBER 967 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.54618E-05 0.21817E-02 Friction velocity uk : 0.54621E-05 0.21817E-02 Dimensionless distance yplus : 0.36371E-04 0.14515E-01 Friction thermal sca. tstar : -0.11529E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.25545E-04 0.10195E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.54618E-05 0.21817E-02 Friction velocity uk : 0.54621E-05 0.21817E-02 Dimensionless distance yplus : 0.36371E-04 0.14515E-01 Friction thermal sca. tstar : -0.11529E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.25545E-04 0.10195E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.39371E-08 3 0.79473E-07 0.14072E-12 0.73371E+00 c Velocity[X] 0.30636E-32 c Velocity[Y] 0.70356E-13 c Velocity[Z] 0.70369E-13 c Pressure 0.59432E-14 16 0.46109E-07 0.46109E-07 0.81176E+00 c k 0.26026E-06 2 0.25975E-07 0.74410E-09 0.11513E+01 c omega 0.13153E+02 1 0.69872E-09 0.92229E-01 0.15810E-02 c TempK 0.94806E+02 1 0.64237E-07 0.14277E-01 0.13209E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.462e-14 7.1034e-14 -8.8531e-18 -2.3208e-18 v Velocity[Y] -0.00011945 0.00011245 -1.6825e-10 -2.8532e-12 v Velocity[Z] -0.00011236 0.00011946 -1.1992e-10 -1.3822e-12 v ǁVelocityǁ 3.3738e-10 0.000128 1.1775e-05 8.9447e-06 v Pressure -0.0016249 0.024957 0.001447 -1.2747e-20 v k 4.1229e-10 0.00087956 0.00055983 0.00071757 v omega 11.419 1.0313e+05 2663.9 496.65 v TempK 288 342.16 294.46 291.36 v Density 1.205 1.205 1.205 1.205 v TurbVisc 4.8307e-15 9.2829e-05 5.376e-05 7.0557e-05 v CourantNb 3.3069e-09 0.00018489 1.3892e-05 9.129e-06 v FourierNb 0.083465 0.6281 0.18087 0.15154 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9621 4.9621 0.00057851 -5.9998e-07 v volume_forces[Z] -4.9621 4.9621 -0.00057843 7.0883e-07 v ǁvolume_forcesǁ 1.2046e-08 4.963 0.58463 0.30121 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.67 291.5 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014515 5.1365e-05 2.8605e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.083473 0.6281 0.18088 0.15155 INSTANT 0.932184000E+00 TIME STEP NUMBER 968 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.55526E-05 0.21813E-02 Friction velocity uk : 0.55529E-05 0.21813E-02 Dimensionless distance yplus : 0.36976E-04 0.14512E-01 Friction thermal sca. tstar : -0.11494E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.25969E-04 0.10193E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.55526E-05 0.21813E-02 Friction velocity uk : 0.55529E-05 0.21813E-02 Dimensionless distance yplus : 0.36976E-04 0.14512E-01 Friction thermal sca. tstar : -0.11494E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.25969E-04 0.10193E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.39385E-08 3 0.79277E-07 0.14037E-12 0.73266E+00 c Velocity[X] 0.30539E-32 c Velocity[Y] 0.70177E-13 c Velocity[Z] 0.70190E-13 c Pressure 0.59342E-14 16 0.46038E-07 0.46038E-07 0.81088E+00 c k 0.25998E-06 2 0.25938E-07 0.74117E-09 0.11503E+01 c omega 0.13153E+02 1 0.69714E-09 0.91887E-01 0.15781E-02 c TempK 0.94807E+02 1 0.64143E-07 0.14255E-01 0.13198E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.458e-14 7.1002e-14 -8.8493e-18 -2.3199e-18 v Velocity[Y] -0.00011943 0.00011243 -1.6576e-10 -2.8505e-12 v Velocity[Z] -0.00011234 0.00011944 -1.2238e-10 -1.3818e-12 v ǁVelocityǁ 3.4163e-10 0.00012797 1.1779e-05 8.9499e-06 v Pressure -0.0016265 0.024969 0.0014478 9.2072e-20 v k 4.1115e-10 0.00087868 0.00055918 0.00071676 v omega 11.408 1.0313e+05 2663.9 496.64 v TempK 288 342.16 294.46 291.36 v Density 1.205 1.205 1.205 1.205 v TurbVisc 4.8173e-15 9.282e-05 5.3745e-05 7.0539e-05 v CourantNb 3.3086e-09 0.00018484 1.3892e-05 9.132e-06 v FourierNb 0.083405 0.6281 0.18084 0.15151 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9621 4.9621 0.00057869 -6.0019e-07 v volume_forces[Z] -4.9621 4.9621 -0.0005786 7.0906e-07 v ǁvolume_forcesǁ 1.2196e-08 4.9631 0.5848 0.30137 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.67 291.5 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014512 5.1354e-05 2.8599e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.083413 0.6281 0.18085 0.15152 INSTANT 0.933147000E+00 TIME STEP NUMBER 969 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.56421E-05 0.21808E-02 Friction velocity uk : 0.56423E-05 0.21808E-02 Dimensionless distance yplus : 0.37572E-04 0.14509E-01 Friction thermal sca. tstar : -0.11459E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.26388E-04 0.10190E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.56421E-05 0.21808E-02 Friction velocity uk : 0.56423E-05 0.21808E-02 Dimensionless distance yplus : 0.37572E-04 0.14509E-01 Friction thermal sca. tstar : -0.11459E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.26388E-04 0.10190E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.39399E-08 3 0.79125E-07 0.14001E-12 0.73162E+00 c Velocity[X] 0.30442E-32 c Velocity[Y] 0.69998E-13 c Velocity[Z] 0.70011E-13 c Pressure 0.59268E-14 16 0.45981E-07 0.45981E-07 0.81000E+00 c k 0.25970E-06 2 0.25902E-07 0.73826E-09 0.11493E+01 c omega 0.13153E+02 1 0.69557E-09 0.91548E-01 0.15752E-02 c TempK 0.94807E+02 1 0.64049E-07 0.14233E-01 0.13188E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.4539e-14 7.0969e-14 -8.8454e-18 -2.319e-18 v Velocity[Y] -0.00011941 0.00011241 -1.6327e-10 -2.8479e-12 v Velocity[Z] -0.00011231 0.00011941 -1.2484e-10 -1.3815e-12 v ǁVelocityǁ 3.4596e-10 0.00012795 1.1782e-05 8.955e-06 v Pressure -0.0016282 0.024982 0.0014487 2.0787e-20 v k 4.1001e-10 0.00087781 0.00055853 0.00071595 v omega 11.398 1.0313e+05 2663.9 496.63 v TempK 288 342.16 294.47 291.37 v Density 1.205 1.205 1.205 1.205 v TurbVisc 4.804e-15 9.2811e-05 5.373e-05 7.0521e-05 v CourantNb 3.3103e-09 0.00018478 1.3893e-05 9.1351e-06 v FourierNb 0.083345 0.6281 0.18081 0.15148 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9621 4.9622 0.00057886 -6.0041e-07 v volume_forces[Z] -4.9621 4.9622 -0.00057878 7.0928e-07 v ǁvolume_forcesǁ 1.235e-08 4.9631 0.58497 0.30152 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.67 291.51 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014509 5.1343e-05 2.8593e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.083353 0.6281 0.18082 0.15149 INSTANT 0.934110000E+00 TIME STEP NUMBER 970 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.57304E-05 0.21804E-02 Friction velocity uk : 0.57306E-05 0.21804E-02 Dimensionless distance yplus : 0.38160E-04 0.14506E-01 Friction thermal sca. tstar : -0.11426E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.26801E-04 0.10188E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.57304E-05 0.21804E-02 Friction velocity uk : 0.57306E-05 0.21804E-02 Dimensionless distance yplus : 0.38160E-04 0.14506E-01 Friction thermal sca. tstar : -0.11426E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.26801E-04 0.10188E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.39413E-08 3 0.79030E-07 0.13965E-12 0.73058E+00 c Velocity[X] 0.30345E-32 c Velocity[Y] 0.69820E-13 c Velocity[Z] 0.69833E-13 c Pressure 0.59712E-14 16 0.46324E-07 0.46324E-07 0.80912E+00 c k 0.25941E-06 2 0.25865E-07 0.73537E-09 0.11483E+01 c omega 0.13153E+02 1 0.69400E-09 0.91209E-01 0.15723E-02 c TempK 0.94808E+02 1 0.63955E-07 0.14211E-01 0.13178E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.4499e-14 7.0937e-14 -8.8416e-18 -2.3181e-18 v Velocity[Y] -0.00011939 0.00011239 -1.6079e-10 -2.8452e-12 v Velocity[Z] -0.00011229 0.00011939 -1.273e-10 -1.3811e-12 v ǁVelocityǁ 3.5038e-10 0.00012793 1.1785e-05 8.9601e-06 v Pressure -0.0016298 0.024994 0.0014495 6.2067e-20 v k 4.0888e-10 0.00087694 0.00055788 0.00071514 v omega 11.388 1.0313e+05 2663.9 496.62 v TempK 288 342.16 294.47 291.37 v Density 1.205 1.205 1.205 1.205 v TurbVisc 4.7907e-15 9.2802e-05 5.3716e-05 7.0503e-05 v CourantNb 3.312e-09 0.00018473 1.3893e-05 9.1382e-06 v FourierNb 0.083285 0.6281 0.18078 0.15145 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9622 4.9622 0.00057904 -6.0062e-07 v volume_forces[Z] -4.9622 4.9622 -0.00057896 7.0951e-07 v ǁvolume_forcesǁ 1.2507e-08 4.9631 0.58515 0.30168 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.67 291.51 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014506 5.1333e-05 2.8587e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.083294 0.6281 0.1808 0.15146 INSTANT 0.935073000E+00 TIME STEP NUMBER 971 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.58175E-05 0.21799E-02 Friction velocity uk : 0.58178E-05 0.21799E-02 Dimensionless distance yplus : 0.38740E-04 0.14503E-01 Friction thermal sca. tstar : -0.11393E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.27208E-04 0.10186E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.58175E-05 0.21799E-02 Friction velocity uk : 0.58178E-05 0.21799E-02 Dimensionless distance yplus : 0.38740E-04 0.14503E-01 Friction thermal sca. tstar : -0.11393E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.27208E-04 0.10186E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.39427E-08 3 0.78871E-07 0.13930E-12 0.72954E+00 c Velocity[X] 0.30249E-32 c Velocity[Y] 0.69641E-13 c Velocity[Z] 0.69654E-13 c Pressure 0.59139E-14 16 0.45880E-07 0.45880E-07 0.80825E+00 c k 0.25913E-06 2 0.25829E-07 0.73249E-09 0.11473E+01 c omega 0.13153E+02 1 0.69243E-09 0.90872E-01 0.15694E-02 c TempK 0.94809E+02 1 0.63861E-07 0.14189E-01 0.13168E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.4458e-14 7.0905e-14 -8.8378e-18 -2.3172e-18 v Velocity[Y] -0.00011937 0.00011236 -1.583e-10 -2.8425e-12 v Velocity[Z] -0.00011227 0.00011937 -1.2976e-10 -1.3808e-12 v ǁVelocityǁ 3.5487e-10 0.0001279 1.1788e-05 8.9652e-06 v Pressure -0.0016315 0.025006 0.0014504 -1.3727e-20 v k 4.0775e-10 0.00087607 0.00055723 0.00071434 v omega 11.378 1.0313e+05 2663.9 496.61 v TempK 288 342.16 294.47 291.37 v Density 1.205 1.205 1.205 1.205 v TurbVisc 4.7774e-15 9.2793e-05 5.3701e-05 7.0485e-05 v CourantNb 3.3138e-09 0.00018467 1.3894e-05 9.1412e-06 v FourierNb 0.083226 0.6281 0.18075 0.15142 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9622 4.9622 0.00057922 -6.0083e-07 v volume_forces[Z] -4.9622 4.9622 -0.00057913 7.0974e-07 v ǁvolume_forcesǁ 1.2666e-08 4.9632 0.58532 0.30183 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.67 291.51 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014503 5.1322e-05 2.858e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.083234 0.6281 0.18077 0.15143 INSTANT 0.936036000E+00 TIME STEP NUMBER 972 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.59035E-05 0.21795E-02 Friction velocity uk : 0.59038E-05 0.21795E-02 Dimensionless distance yplus : 0.39313E-04 0.14500E-01 Friction thermal sca. tstar : -0.11361E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.27611E-04 0.10184E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.59035E-05 0.21795E-02 Friction velocity uk : 0.59038E-05 0.21795E-02 Dimensionless distance yplus : 0.39313E-04 0.14500E-01 Friction thermal sca. tstar : -0.11361E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.27611E-04 0.10184E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.39440E-08 3 0.78717E-07 0.13894E-12 0.72850E+00 c Velocity[X] 0.30154E-32 c Velocity[Y] 0.69463E-13 c Velocity[Z] 0.69477E-13 c Pressure 0.59050E-14 16 0.45810E-07 0.45810E-07 0.80737E+00 c k 0.25885E-06 2 0.25792E-07 0.72962E-09 0.11463E+01 c omega 0.13153E+02 1 0.69087E-09 0.90537E-01 0.15665E-02 c TempK 0.94809E+02 1 0.63768E-07 0.14167E-01 0.13157E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.4418e-14 7.0873e-14 -8.834e-18 -2.3163e-18 v Velocity[Y] -0.00011934 0.00011234 -1.5581e-10 -2.84e-12 v Velocity[Z] -0.00011225 0.00011935 -1.3221e-10 -1.3802e-12 v ǁVelocityǁ 3.5945e-10 0.00012788 1.1792e-05 8.9704e-06 v Pressure -0.0016331 0.025019 0.0014512 5.7361e-20 v k 4.0662e-10 0.0008752 0.00055658 0.00071353 v omega 11.368 1.0313e+05 2663.9 496.6 v TempK 288 342.16 294.47 291.37 v Density 1.205 1.205 1.205 1.205 v TurbVisc 4.7642e-15 9.2783e-05 5.3686e-05 7.0467e-05 v CourantNb 3.3155e-09 0.00018462 1.3894e-05 9.1443e-06 v FourierNb 0.083166 0.6281 0.18073 0.15139 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9622 4.9623 0.00057939 -6.0103e-07 v volume_forces[Z] -4.9622 4.9623 -0.00057931 7.0996e-07 v ǁvolume_forcesǁ 1.2829e-08 4.9632 0.5855 0.30198 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.68 291.51 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.0145 5.1312e-05 2.8574e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.083174 0.6281 0.18074 0.1514 INSTANT 0.936999000E+00 TIME STEP NUMBER 973 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.59885E-05 0.21790E-02 Friction velocity uk : 0.59887E-05 0.21790E-02 Dimensionless distance yplus : 0.39878E-04 0.14497E-01 Friction thermal sca. tstar : -0.11330E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.28008E-04 0.10182E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.59885E-05 0.21790E-02 Friction velocity uk : 0.59887E-05 0.21790E-02 Dimensionless distance yplus : 0.39878E-04 0.14497E-01 Friction thermal sca. tstar : -0.11330E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.28008E-04 0.10182E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.39454E-08 3 0.78563E-07 0.13858E-12 0.72746E+00 c Velocity[X] 0.30059E-32 c Velocity[Y] 0.69285E-13 c Velocity[Z] 0.69299E-13 c Pressure 0.58911E-14 16 0.45702E-07 0.45702E-07 0.80650E+00 c k 0.25857E-06 2 0.25756E-07 0.72677E-09 0.11453E+01 c omega 0.13153E+02 1 0.68931E-09 0.90203E-01 0.15636E-02 c TempK 0.94810E+02 1 0.63674E-07 0.14145E-01 0.13147E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.4377e-14 7.0841e-14 -8.8301e-18 -2.3154e-18 v Velocity[Y] -0.00011932 0.00011232 -1.5333e-10 -2.8372e-12 v Velocity[Z] -0.00011223 0.00011933 -1.3466e-10 -1.3797e-12 v ǁVelocityǁ 3.6409e-10 0.00012785 1.1795e-05 8.9755e-06 v Pressure -0.0016347 0.025031 0.0014521 -1.1511e-19 v k 4.055e-10 0.00087434 0.00055594 0.00071273 v omega 11.357 1.0313e+05 2663.9 496.59 v TempK 288 342.16 294.47 291.37 v Density 1.205 1.205 1.205 1.205 v TurbVisc 4.7511e-15 9.2774e-05 5.3671e-05 7.0449e-05 v CourantNb 3.3172e-09 0.00018457 1.3895e-05 9.1473e-06 v FourierNb 0.083107 0.6281 0.1807 0.15136 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9623 4.9623 0.00057957 -6.0124e-07 v volume_forces[Z] -4.9623 4.9623 -0.00057949 7.1019e-07 v ǁvolume_forcesǁ 1.2994e-08 4.9633 0.58567 0.30214 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.68 291.51 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014497 5.1301e-05 2.8568e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.083115 0.6281 0.18071 0.15137 INSTANT 0.937962000E+00 TIME STEP NUMBER 974 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.60724E-05 0.21786E-02 Friction velocity uk : 0.60726E-05 0.21786E-02 Dimensionless distance yplus : 0.40437E-04 0.14494E-01 Friction thermal sca. tstar : -0.11300E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.28400E-04 0.10180E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.60724E-05 0.21786E-02 Friction velocity uk : 0.60726E-05 0.21786E-02 Dimensionless distance yplus : 0.40437E-04 0.14494E-01 Friction thermal sca. tstar : -0.11300E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.28400E-04 0.10180E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.39468E-08 3 0.78412E-07 0.13823E-12 0.72642E+00 c Velocity[X] 0.29964E-32 c Velocity[Y] 0.69108E-13 c Velocity[Z] 0.69121E-13 c Pressure 0.58815E-14 16 0.45627E-07 0.45627E-07 0.80564E+00 c k 0.25829E-06 2 0.25719E-07 0.72393E-09 0.11443E+01 c omega 0.13153E+02 1 0.68776E-09 0.89871E-01 0.15607E-02 c TempK 0.94810E+02 1 0.63581E-07 0.14124E-01 0.13137E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.4337e-14 7.081e-14 -8.8263e-18 -2.3145e-18 v Velocity[Y] -0.0001193 0.0001123 -1.5084e-10 -2.8345e-12 v Velocity[Z] -0.0001122 0.0001193 -1.3711e-10 -1.3793e-12 v ǁVelocityǁ 3.6882e-10 0.00012783 1.1798e-05 8.9806e-06 v Pressure -0.0016364 0.025044 0.0014529 7.2657e-20 v k 4.0438e-10 0.00087347 0.00055529 0.00071193 v omega 11.347 1.0313e+05 2663.9 496.59 v TempK 288 342.16 294.48 291.37 v Density 1.205 1.205 1.205 1.205 v TurbVisc 4.738e-15 9.2765e-05 5.3656e-05 7.0431e-05 v CourantNb 3.3189e-09 0.00018451 1.3895e-05 9.1503e-06 v FourierNb 0.083048 0.6281 0.18067 0.15133 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9623 4.9623 0.00057975 -6.0145e-07 v volume_forces[Z] -4.9623 4.9623 -0.00057966 7.1041e-07 v ǁvolume_forcesǁ 1.3162e-08 4.9633 0.58585 0.30229 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.68 291.51 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014494 5.1291e-05 2.8562e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.083056 0.6281 0.18068 0.15134 INSTANT 0.938925000E+00 TIME STEP NUMBER 975 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.61554E-05 0.21781E-02 Friction velocity uk : 0.61556E-05 0.21781E-02 Dimensionless distance yplus : 0.40990E-04 0.14491E-01 Friction thermal sca. tstar : -0.11271E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.28788E-04 0.10178E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.61554E-05 0.21781E-02 Friction velocity uk : 0.61556E-05 0.21781E-02 Dimensionless distance yplus : 0.40990E-04 0.14491E-01 Friction thermal sca. tstar : -0.11271E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.28788E-04 0.10178E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.39482E-08 3 0.78259E-07 0.13787E-12 0.72538E+00 c Velocity[X] 0.29869E-32 c Velocity[Y] 0.68930E-13 c Velocity[Z] 0.68943E-13 c Pressure 0.58722E-14 16 0.45554E-07 0.45554E-07 0.80477E+00 c k 0.25801E-06 2 0.25683E-07 0.72110E-09 0.11433E+01 c omega 0.13153E+02 1 0.68622E-09 0.89540E-01 0.15578E-02 c TempK 0.94811E+02 1 0.63489E-07 0.14102E-01 0.13127E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.4297e-14 7.0778e-14 -8.8225e-18 -2.3137e-18 v Velocity[Y] -0.00011928 0.00011228 -1.4836e-10 -2.8318e-12 v Velocity[Z] -0.00011218 0.00011928 -1.3956e-10 -1.3788e-12 v ǁVelocityǁ 3.7361e-10 0.00012781 1.1801e-05 8.9856e-06 v Pressure -0.001638 0.025056 0.0014537 5.54e-20 v k 4.0327e-10 0.00087261 0.00055465 0.00071113 v omega 11.337 1.0313e+05 2663.9 496.58 v TempK 288 342.16 294.48 291.38 v Density 1.205 1.205 1.205 1.205 v TurbVisc 4.7249e-15 9.2756e-05 5.3641e-05 7.0413e-05 v CourantNb 3.3206e-09 0.00018446 1.3896e-05 9.1534e-06 v FourierNb 0.082989 0.6281 0.18064 0.1513 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9624 4.9624 0.00057992 -6.0166e-07 v volume_forces[Z] -4.9624 4.9624 -0.00057984 7.1064e-07 v ǁvolume_forcesǁ 1.3333e-08 4.9633 0.58602 0.30244 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.68 291.52 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014491 5.128e-05 2.8556e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.082997 0.6281 0.18066 0.15131 INSTANT 0.939888000E+00 TIME STEP NUMBER 976 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.62374E-05 0.21777E-02 Friction velocity uk : 0.62376E-05 0.21777E-02 Dimensionless distance yplus : 0.41536E-04 0.14488E-01 Friction thermal sca. tstar : -0.11242E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.29172E-04 0.10176E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.62374E-05 0.21777E-02 Friction velocity uk : 0.62376E-05 0.21777E-02 Dimensionless distance yplus : 0.41536E-04 0.14488E-01 Friction thermal sca. tstar : -0.11242E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.29172E-04 0.10176E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.39495E-08 3 0.78111E-07 0.13752E-12 0.72434E+00 c Velocity[X] 0.29775E-32 c Velocity[Y] 0.68753E-13 c Velocity[Z] 0.68766E-13 c Pressure 0.58732E-14 16 0.45562E-07 0.45562E-07 0.80390E+00 c k 0.25773E-06 2 0.25647E-07 0.71829E-09 0.11423E+01 c omega 0.13153E+02 1 0.68467E-09 0.89211E-01 0.15550E-02 c TempK 0.94811E+02 1 0.63396E-07 0.14080E-01 0.13116E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.4257e-14 7.0746e-14 -8.8187e-18 -2.3128e-18 v Velocity[Y] -0.00011925 0.00011226 -1.4587e-10 -2.8292e-12 v Velocity[Z] -0.00011216 0.00011926 -1.4201e-10 -1.3784e-12 v ǁVelocityǁ 3.7848e-10 0.00012778 1.1804e-05 8.9907e-06 v Pressure -0.0016397 0.025068 0.0014546 5.0987e-21 v k 4.0216e-10 0.00087175 0.00055401 0.00071033 v omega 11.327 1.0313e+05 2663.9 496.57 v TempK 288 342.16 294.48 291.38 v Density 1.205 1.205 1.205 1.205 v TurbVisc 4.7119e-15 9.2747e-05 5.3626e-05 7.0395e-05 v CourantNb 3.3223e-09 0.0001844 1.3896e-05 9.1564e-06 v FourierNb 0.08293 0.6281 0.18061 0.15127 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9624 4.9624 0.0005801 -6.0187e-07 v volume_forces[Z] -4.9624 4.9624 -0.00058001 7.1086e-07 v ǁvolume_forcesǁ 1.3506e-08 4.9634 0.58619 0.3026 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.68 291.52 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014488 5.127e-05 2.8549e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.082938 0.6281 0.18063 0.15128 INSTANT 0.940851000E+00 TIME STEP NUMBER 977 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.63186E-05 0.21772E-02 Friction velocity uk : 0.63188E-05 0.21772E-02 Dimensionless distance yplus : 0.42076E-04 0.14485E-01 Friction thermal sca. tstar : -0.11214E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.29551E-04 0.10174E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.63186E-05 0.21772E-02 Friction velocity uk : 0.63188E-05 0.21772E-02 Dimensionless distance yplus : 0.42076E-04 0.14485E-01 Friction thermal sca. tstar : -0.11214E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.29551E-04 0.10174E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.39509E-08 3 0.77975E-07 0.13716E-12 0.72330E+00 c Velocity[X] 0.29681E-32 c Velocity[Y] 0.68575E-13 c Velocity[Z] 0.68589E-13 c Pressure 0.58546E-14 16 0.45417E-07 0.45417E-07 0.80304E+00 c k 0.25745E-06 2 0.25611E-07 0.71549E-09 0.11413E+01 c omega 0.13153E+02 1 0.68314E-09 0.88883E-01 0.15521E-02 c TempK 0.94812E+02 1 0.63304E-07 0.14058E-01 0.13106E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.4217e-14 7.0714e-14 -8.8149e-18 -2.3119e-18 v Velocity[Y] -0.00011923 0.00011223 -1.4339e-10 -2.8266e-12 v Velocity[Z] -0.00011214 0.00011924 -1.4445e-10 -1.3779e-12 v ǁVelocityǁ 3.8341e-10 0.00012776 1.1808e-05 8.9958e-06 v Pressure -0.0016413 0.025081 0.0014554 -1.2266e-19 v k 4.0106e-10 0.00087089 0.00055337 0.00070954 v omega 11.317 1.0313e+05 2663.8 496.56 v TempK 288 342.16 294.48 291.38 v Density 1.205 1.205 1.205 1.205 v TurbVisc 4.699e-15 9.2738e-05 5.3611e-05 7.0377e-05 v CourantNb 3.3239e-09 0.00018435 1.3897e-05 9.1594e-06 v FourierNb 0.082871 0.6281 0.18059 0.15124 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9624 4.9624 0.00058027 -6.0208e-07 v volume_forces[Z] -4.9624 4.9624 -0.00058019 7.1108e-07 v ǁvolume_forcesǁ 1.3682e-08 4.9634 0.58637 0.30275 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.69 291.52 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014485 5.1259e-05 2.8543e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.082879 0.6281 0.1806 0.15125 INSTANT 0.941814000E+00 TIME STEP NUMBER 978 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.63988E-05 0.21768E-02 Friction velocity uk : 0.63990E-05 0.21768E-02 Dimensionless distance yplus : 0.42610E-04 0.14482E-01 Friction thermal sca. tstar : -0.11187E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.29927E-04 0.10172E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.63988E-05 0.21768E-02 Friction velocity uk : 0.63990E-05 0.21768E-02 Dimensionless distance yplus : 0.42610E-04 0.14482E-01 Friction thermal sca. tstar : -0.11187E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.29927E-04 0.10172E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.39523E-08 3 0.77825E-07 0.13681E-12 0.72226E+00 c Velocity[X] 0.29587E-32 c Velocity[Y] 0.68398E-13 c Velocity[Z] 0.68412E-13 c Pressure 0.58455E-14 16 0.45346E-07 0.45346E-07 0.80218E+00 c k 0.25717E-06 2 0.25575E-07 0.71271E-09 0.11403E+01 c omega 0.13153E+02 1 0.68160E-09 0.88557E-01 0.15492E-02 c TempK 0.94812E+02 1 0.63212E-07 0.14037E-01 0.13096E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.4177e-14 7.0683e-14 -8.8111e-18 -2.311e-18 v Velocity[Y] -0.00011921 0.00011221 -1.4091e-10 -2.824e-12 v Velocity[Z] -0.00011212 0.00011922 -1.4689e-10 -1.3774e-12 v ǁVelocityǁ 3.8841e-10 0.00012773 1.1811e-05 9.0009e-06 v Pressure -0.001643 0.025093 0.0014563 -1.765e-21 v k 3.9996e-10 0.00087003 0.00055273 0.00070874 v omega 11.307 1.0313e+05 2663.8 496.55 v TempK 288 342.16 294.48 291.38 v Density 1.205 1.205 1.205 1.205 v TurbVisc 4.6861e-15 9.2729e-05 5.3596e-05 7.0359e-05 v CourantNb 3.3256e-09 0.0001843 1.3897e-05 9.1624e-06 v FourierNb 0.082812 0.6281 0.18056 0.15121 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9625 4.9625 0.00058045 -6.0228e-07 v volume_forces[Z] -4.9625 4.9625 -0.00058037 7.1131e-07 v ǁvolume_forcesǁ 1.386e-08 4.9634 0.58654 0.3029 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.69 291.52 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014482 5.1249e-05 2.8537e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.08282 0.6281 0.18057 0.15122 INSTANT 0.942777000E+00 TIME STEP NUMBER 979 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.64783E-05 0.21764E-02 Friction velocity uk : 0.64784E-05 0.21763E-02 Dimensionless distance yplus : 0.43139E-04 0.14479E-01 Friction thermal sca. tstar : -0.11161E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.30298E-04 0.10169E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.64783E-05 0.21764E-02 Friction velocity uk : 0.64784E-05 0.21763E-02 Dimensionless distance yplus : 0.43139E-04 0.14479E-01 Friction thermal sca. tstar : -0.11161E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.30298E-04 0.10169E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.39537E-08 3 0.77658E-07 0.13646E-12 0.72122E+00 c Velocity[X] 0.29493E-32 c Velocity[Y] 0.68221E-13 c Velocity[Z] 0.68235E-13 c Pressure 0.58371E-14 16 0.45281E-07 0.45281E-07 0.80132E+00 c k 0.25689E-06 2 0.25539E-07 0.70994E-09 0.11393E+01 c omega 0.13153E+02 1 0.68008E-09 0.88232E-01 0.15464E-02 c TempK 0.94813E+02 1 0.63120E-07 0.14015E-01 0.13086E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.4137e-14 7.0651e-14 -8.8074e-18 -2.3101e-18 v Velocity[Y] -0.00011919 0.00011219 -1.3843e-10 -2.8214e-12 v Velocity[Z] -0.00011209 0.00011919 -1.4933e-10 -1.377e-12 v ǁVelocityǁ 3.9347e-10 0.00012771 1.1814e-05 9.0059e-06 v Pressure -0.0016446 0.025106 0.0014571 -1.1864e-19 v k 3.9886e-10 0.00086918 0.00055209 0.00070795 v omega 11.297 1.0313e+05 2663.8 496.54 v TempK 288 342.16 294.48 291.38 v Density 1.205 1.205 1.205 1.205 v TurbVisc 4.6732e-15 9.272e-05 5.3582e-05 7.0341e-05 v CourantNb 3.3273e-09 0.00018424 1.3898e-05 9.1654e-06 v FourierNb 0.082753 0.6281 0.18053 0.15118 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9625 4.9625 0.00058062 -6.0249e-07 v volume_forces[Z] -4.9625 4.9625 -0.00058054 7.1153e-07 v ǁvolume_forcesǁ 1.4041e-08 4.9635 0.58671 0.30306 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.69 291.52 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014479 5.1238e-05 2.8531e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.082762 0.6281 0.18054 0.15119 INSTANT 0.943740000E+00 TIME STEP NUMBER 980 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.65569E-05 0.21759E-02 Friction velocity uk : 0.65571E-05 0.21759E-02 Dimensionless distance yplus : 0.43663E-04 0.14476E-01 Friction thermal sca. tstar : -0.11136E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.30666E-04 0.10167E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.65569E-05 0.21759E-02 Friction velocity uk : 0.65571E-05 0.21759E-02 Dimensionless distance yplus : 0.43663E-04 0.14476E-01 Friction thermal sca. tstar : -0.11136E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.30666E-04 0.10167E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.39550E-08 3 0.77511E-07 0.13610E-12 0.72018E+00 c Velocity[X] 0.29400E-32 c Velocity[Y] 0.68045E-13 c Velocity[Z] 0.68058E-13 c Pressure 0.58288E-14 16 0.45215E-07 0.45215E-07 0.80046E+00 c k 0.25662E-06 2 0.25503E-07 0.70718E-09 0.11384E+01 c omega 0.13153E+02 1 0.67855E-09 0.87909E-01 0.15436E-02 c TempK 0.94813E+02 1 0.63028E-07 0.13994E-01 0.13076E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.4097e-14 7.0619e-14 -8.8036e-18 -2.3093e-18 v Velocity[Y] -0.00011917 0.00011217 -1.3595e-10 -2.8188e-12 v Velocity[Z] -0.00011207 0.00011917 -1.5177e-10 -1.3766e-12 v ǁVelocityǁ 3.986e-10 0.00012768 1.1817e-05 9.011e-06 v Pressure -0.0016462 0.025118 0.001458 -1.1806e-19 v k 3.9777e-10 0.00086832 0.00055146 0.00070716 v omega 11.287 1.0313e+05 2663.8 496.53 v TempK 288 342.16 294.49 291.39 v Density 1.205 1.205 1.205 1.205 v TurbVisc 4.6604e-15 9.2711e-05 5.3567e-05 7.0324e-05 v CourantNb 3.3289e-09 0.00018419 1.3898e-05 9.1685e-06 v FourierNb 0.082695 0.6281 0.1805 0.15115 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9625 4.9626 0.0005808 -6.027e-07 v volume_forces[Z] -4.9625 4.9626 -0.00058072 7.1175e-07 v ǁvolume_forcesǁ 1.4224e-08 4.9635 0.58689 0.30321 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.69 291.53 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014476 5.1228e-05 2.8525e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.082703 0.6281 0.18051 0.15116 INSTANT 0.944703000E+00 TIME STEP NUMBER 981 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.66347E-05 0.21755E-02 Friction velocity uk : 0.66349E-05 0.21754E-02 Dimensionless distance yplus : 0.44181E-04 0.14474E-01 Friction thermal sca. tstar : -0.11111E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.31030E-04 0.10165E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.66347E-05 0.21755E-02 Friction velocity uk : 0.66349E-05 0.21754E-02 Dimensionless distance yplus : 0.44181E-04 0.14474E-01 Friction thermal sca. tstar : -0.11111E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.31030E-04 0.10165E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.39564E-08 3 0.77364E-07 0.13575E-12 0.71914E+00 c Velocity[X] 0.29308E-32 c Velocity[Y] 0.67868E-13 c Velocity[Z] 0.67882E-13 c Pressure 0.58198E-14 16 0.45145E-07 0.45145E-07 0.79960E+00 c k 0.25634E-06 2 0.25468E-07 0.70443E-09 0.11374E+01 c omega 0.13153E+02 1 0.67703E-09 0.87587E-01 0.15407E-02 c TempK 0.94814E+02 1 0.62937E-07 0.13972E-01 0.13066E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.4057e-14 7.0588e-14 -8.7998e-18 -2.3084e-18 v Velocity[Y] -0.00011914 0.00011215 -1.3347e-10 -2.8163e-12 v Velocity[Z] -0.00011205 0.00011915 -1.5421e-10 -1.3761e-12 v ǁVelocityǁ 4.0378e-10 0.00012766 1.182e-05 9.016e-06 v Pressure -0.0016479 0.02513 0.0014588 -5.638e-20 v k 3.9668e-10 0.00086747 0.00055082 0.00070637 v omega 11.277 1.0313e+05 2663.8 496.52 v TempK 288 342.16 294.49 291.39 v Density 1.205 1.205 1.205 1.205 v TurbVisc 4.6476e-15 9.2702e-05 5.3552e-05 7.0306e-05 v CourantNb 3.3306e-09 0.00018413 1.3899e-05 9.1715e-06 v FourierNb 0.082637 0.6281 0.18047 0.15112 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9626 4.9626 0.00058097 -6.0291e-07 v volume_forces[Z] -4.9626 4.9626 -0.00058089 7.1197e-07 v ǁvolume_forcesǁ 1.4409e-08 4.9635 0.58706 0.30336 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.69 291.53 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014474 5.1217e-05 2.8518e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.082645 0.6281 0.18049 0.15113 INSTANT 0.945666000E+00 TIME STEP NUMBER 982 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.67119E-05 0.21750E-02 Friction velocity uk : 0.67120E-05 0.21750E-02 Dimensionless distance yplus : 0.44695E-04 0.14471E-01 Friction thermal sca. tstar : -0.11087E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.31391E-04 0.10163E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.67119E-05 0.21750E-02 Friction velocity uk : 0.67120E-05 0.21750E-02 Dimensionless distance yplus : 0.44695E-04 0.14471E-01 Friction thermal sca. tstar : -0.11087E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.31391E-04 0.10163E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.39577E-08 3 0.77235E-07 0.13540E-12 0.71810E+00 c Velocity[X] 0.29216E-32 c Velocity[Y] 0.67692E-13 c Velocity[Z] 0.67706E-13 c Pressure 0.58900E-14 16 0.45689E-07 0.45689E-07 0.79875E+00 c k 0.25606E-06 2 0.25432E-07 0.70170E-09 0.11364E+01 c omega 0.13153E+02 1 0.67552E-09 0.87266E-01 0.15379E-02 c TempK 0.94814E+02 1 0.62846E-07 0.13951E-01 0.13056E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.4017e-14 7.0556e-14 -8.796e-18 -2.3075e-18 v Velocity[Y] -0.00011912 0.00011213 -1.3099e-10 -2.8137e-12 v Velocity[Z] -0.00011203 0.00011913 -1.5665e-10 -1.3756e-12 v ǁVelocityǁ 4.0903e-10 0.00012764 1.1823e-05 9.021e-06 v Pressure -0.0016495 0.025143 0.0014596 2.8631e-20 v k 3.9559e-10 0.00086662 0.00055019 0.00070558 v omega 11.267 1.0313e+05 2663.8 496.52 v TempK 288 342.16 294.49 291.39 v Density 1.205 1.205 1.205 1.205 v TurbVisc 4.6349e-15 9.2693e-05 5.3537e-05 7.0288e-05 v CourantNb 3.3322e-09 0.00018408 1.39e-05 9.1745e-06 v FourierNb 0.082578 0.6281 0.18045 0.15109 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9626 4.9626 0.00058115 -6.0311e-07 v volume_forces[Z] -4.9626 4.9626 -0.00058107 7.122e-07 v ǁvolume_forcesǁ 1.4597e-08 4.9636 0.58723 0.30351 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.7 291.53 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014471 5.1207e-05 2.8512e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.082587 0.6281 0.18046 0.1511 INSTANT 0.946629000E+00 TIME STEP NUMBER 983 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.67882E-05 0.21746E-02 Friction velocity uk : 0.67884E-05 0.21745E-02 Dimensionless distance yplus : 0.45203E-04 0.14468E-01 Friction thermal sca. tstar : -0.11063E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.31748E-04 0.10161E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.67882E-05 0.21746E-02 Friction velocity uk : 0.67884E-05 0.21745E-02 Dimensionless distance yplus : 0.45203E-04 0.14468E-01 Friction thermal sca. tstar : -0.11063E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.31748E-04 0.10161E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.39591E-08 3 0.77067E-07 0.13505E-12 0.71706E+00 c Velocity[X] 0.29125E-32 c Velocity[Y] 0.67516E-13 c Velocity[Z] 0.67530E-13 c Pressure 0.58030E-14 16 0.45014E-07 0.45014E-07 0.79790E+00 c k 0.25579E-06 2 0.25396E-07 0.69898E-09 0.11354E+01 c omega 0.13153E+02 1 0.67401E-09 0.86947E-01 0.15351E-02 c TempK 0.94815E+02 1 0.62755E-07 0.13930E-01 0.13046E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.3977e-14 7.0525e-14 -8.7923e-18 -2.3066e-18 v Velocity[Y] -0.0001191 0.0001121 -1.2852e-10 -2.821e-12 v Velocity[Z] -0.00011201 0.0001191 -1.5908e-10 -1.3772e-12 v ǁVelocityǁ 4.143e-10 0.00012761 1.1827e-05 9.026e-06 v Pressure -0.0016512 0.025155 0.0014605 3.6868e-20 v k 3.9451e-10 0.00086577 0.00054956 0.00070479 v omega 11.257 1.0313e+05 2663.8 496.51 v TempK 288 342.16 294.49 291.39 v Density 1.205 1.205 1.205 1.205 v TurbVisc 4.6222e-15 9.2685e-05 5.3522e-05 7.027e-05 v CourantNb 3.3338e-09 0.00018403 1.39e-05 9.1775e-06 v FourierNb 0.08252 0.6281 0.18042 0.15106 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9626 4.9627 0.00058132 -6.0332e-07 v volume_forces[Z] -4.9626 4.9627 -0.00058124 7.1242e-07 v ǁvolume_forcesǁ 1.4786e-08 4.9636 0.5874 0.30367 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.7 291.53 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014468 5.1196e-05 2.8506e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.082529 0.6281 0.18043 0.15107 INSTANT 0.947592000E+00 TIME STEP NUMBER 984 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.68635E-05 0.21741E-02 Friction velocity uk : 0.68637E-05 0.21741E-02 Dimensionless distance yplus : 0.45705E-04 0.14465E-01 Friction thermal sca. tstar : -0.11069E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.32100E-04 0.10159E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.68635E-05 0.21741E-02 Friction velocity uk : 0.68637E-05 0.21741E-02 Dimensionless distance yplus : 0.45705E-04 0.14465E-01 Friction thermal sca. tstar : -0.11069E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.32100E-04 0.10159E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.39605E-08 3 0.76923E-07 0.13469E-12 0.71602E+00 c Velocity[X] 0.29034E-32 c Velocity[Y] 0.67340E-13 c Velocity[Z] 0.67354E-13 c Pressure 0.57941E-14 16 0.44945E-07 0.44945E-07 0.79705E+00 c k 0.25551E-06 2 0.25361E-07 0.69628E-09 0.11344E+01 c omega 0.13153E+02 1 0.67251E-09 0.86630E-01 0.15323E-02 c TempK 0.94815E+02 1 0.62664E-07 0.13908E-01 0.13036E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.3938e-14 7.0493e-14 -8.7885e-18 -2.3058e-18 v Velocity[Y] -0.00011908 0.00011208 -1.2605e-10 -2.8186e-12 v Velocity[Z] -0.00011198 0.00011908 -1.6152e-10 -1.3763e-12 v ǁVelocityǁ 4.1967e-10 0.00012759 1.183e-05 9.0311e-06 v Pressure -0.0016528 0.025167 0.0014613 5.187e-20 v k 3.9344e-10 0.00086492 0.00054893 0.00070401 v omega 11.247 1.0313e+05 2663.8 496.5 v TempK 288 342.16 294.49 291.39 v Density 1.205 1.205 1.205 1.205 v TurbVisc 4.6096e-15 9.2676e-05 5.3508e-05 7.0252e-05 v CourantNb 3.3355e-09 0.00018397 1.3901e-05 9.1804e-06 v FourierNb 0.082463 0.6281 0.18039 0.15103 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9627 4.9627 0.0005815 -6.0352e-07 v volume_forces[Z] -4.9627 4.9627 -0.00058142 7.1264e-07 v ǁvolume_forcesǁ 1.4977e-08 4.9636 0.58758 0.30382 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.7 291.53 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014465 5.1186e-05 2.85e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.082471 0.6281 0.1804 0.15104 INSTANT 0.948555000E+00 TIME STEP NUMBER 985 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.69387E-05 0.21737E-02 Friction velocity uk : 0.69388E-05 0.21737E-02 Dimensionless distance yplus : 0.46205E-04 0.14462E-01 Friction thermal sca. tstar : -0.11123E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.32451E-04 0.10157E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.69387E-05 0.21737E-02 Friction velocity uk : 0.69388E-05 0.21737E-02 Dimensionless distance yplus : 0.46205E-04 0.14462E-01 Friction thermal sca. tstar : -0.11123E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.32451E-04 0.10157E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.39618E-08 3 0.76784E-07 0.13434E-12 0.71499E+00 c Velocity[X] 0.28943E-32 c Velocity[Y] 0.67164E-13 c Velocity[Z] 0.67178E-13 c Pressure 0.58030E-14 16 0.45013E-07 0.45013E-07 0.79620E+00 c k 0.25524E-06 2 0.25326E-07 0.69358E-09 0.11335E+01 c omega 0.13153E+02 1 0.67101E-09 0.86314E-01 0.15295E-02 c TempK 0.94816E+02 1 0.62574E-07 0.13887E-01 0.13025E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.3898e-14 7.0462e-14 -8.7848e-18 -2.3049e-18 v Velocity[Y] -0.00011905 0.00011206 -1.2357e-10 -2.816e-12 v Velocity[Z] -0.00011196 0.00011906 -1.6395e-10 -1.376e-12 v ǁVelocityǁ 4.2509e-10 0.00012756 1.1833e-05 9.0361e-06 v Pressure -0.0016544 0.025179 0.0014622 7.2559e-21 v k 3.9237e-10 0.00086407 0.0005483 0.00070322 v omega 11.237 1.0313e+05 2663.8 496.49 v TempK 288 342.16 294.5 291.39 v Density 1.205 1.205 1.205 1.205 v TurbVisc 4.597e-15 9.2667e-05 5.3493e-05 7.0235e-05 v CourantNb 3.3371e-09 0.00018392 1.3901e-05 9.1834e-06 v FourierNb 0.082405 0.6281 0.18036 0.151 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9627 4.9627 0.00058167 -6.0373e-07 v volume_forces[Z] -4.9627 4.9627 -0.00058159 7.1286e-07 v ǁvolume_forcesǁ 1.5171e-08 4.9637 0.58775 0.30397 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.7 291.53 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014462 5.1175e-05 2.8494e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.082413 0.6281 0.18038 0.15101 INSTANT 0.949518000E+00 TIME STEP NUMBER 986 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.70131E-05 0.21732E-02 Friction velocity uk : 0.70133E-05 0.21732E-02 Dimensionless distance yplus : 0.46701E-04 0.14459E-01 Friction thermal sca. tstar : -0.11177E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.32799E-04 0.10155E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.70131E-05 0.21732E-02 Friction velocity uk : 0.70133E-05 0.21732E-02 Dimensionless distance yplus : 0.46701E-04 0.14459E-01 Friction thermal sca. tstar : -0.11177E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.32799E-04 0.10155E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.39632E-08 3 0.76652E-07 0.13399E-12 0.71395E+00 c Velocity[X] 0.28852E-32 c Velocity[Y] 0.66989E-13 c Velocity[Z] 0.67003E-13 c Pressure 0.58030E-14 16 0.45012E-07 0.45012E-07 0.79535E+00 c k 0.25497E-06 2 0.25290E-07 0.69090E-09 0.11325E+01 c omega 0.13153E+02 1 0.66951E-09 0.85999E-01 0.15267E-02 c TempK 0.94816E+02 1 0.62483E-07 0.13866E-01 0.13015E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.3859e-14 7.0431e-14 -8.781e-18 -2.304e-18 v Velocity[Y] -0.00011903 0.00011204 -1.211e-10 -2.8135e-12 v Velocity[Z] -0.00011194 0.00011904 -1.6637e-10 -1.3755e-12 v ǁVelocityǁ 4.3056e-10 0.00012754 1.1836e-05 9.0411e-06 v Pressure -0.0016561 0.025192 0.001463 -2.8435e-20 v k 3.913e-10 0.00086323 0.00054767 0.00070244 v omega 11.227 1.0313e+05 2663.8 496.48 v TempK 288 342.16 294.5 291.4 v Density 1.205 1.205 1.205 1.205 v TurbVisc 4.5845e-15 9.2658e-05 5.3478e-05 7.0217e-05 v CourantNb 3.3387e-09 0.00018387 1.3902e-05 9.1864e-06 v FourierNb 0.082347 0.6281 0.18033 0.15097 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9627 4.9628 0.00058185 -6.0393e-07 v volume_forces[Z] -4.9627 4.9628 -0.00058177 7.1308e-07 v ǁvolume_forcesǁ 1.5367e-08 4.9637 0.58792 0.30412 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.7 291.54 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014459 5.1165e-05 2.8488e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.082355 0.6281 0.18035 0.15098 INSTANT 0.950481000E+00 TIME STEP NUMBER 987 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.70869E-05 0.21728E-02 Friction velocity uk : 0.70870E-05 0.21728E-02 Dimensionless distance yplus : 0.47192E-04 0.14456E-01 Friction thermal sca. tstar : -0.11233E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.33144E-04 0.10153E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.70869E-05 0.21728E-02 Friction velocity uk : 0.70870E-05 0.21728E-02 Dimensionless distance yplus : 0.47192E-04 0.14456E-01 Friction thermal sca. tstar : -0.11233E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.33144E-04 0.10153E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.39645E-08 3 0.76502E-07 0.13364E-12 0.71291E+00 c Velocity[X] 0.28763E-32 c Velocity[Y] 0.66813E-13 c Velocity[Z] 0.66827E-13 c Pressure 0.57709E-14 16 0.44763E-07 0.44763E-07 0.79450E+00 c k 0.25469E-06 2 0.25255E-07 0.68823E-09 0.11315E+01 c omega 0.13153E+02 1 0.66802E-09 0.85686E-01 0.15239E-02 c TempK 0.94817E+02 1 0.62393E-07 0.13845E-01 0.13005E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.3819e-14 7.04e-14 -8.7773e-18 -2.3032e-18 v Velocity[Y] -0.00011901 0.00011202 -1.1863e-10 -2.811e-12 v Velocity[Z] -0.00011192 0.00011902 -1.688e-10 -1.3751e-12 v ǁVelocityǁ 4.3608e-10 0.00012751 1.1839e-05 9.046e-06 v Pressure -0.0016577 0.025204 0.0014638 1.7473e-19 v k 3.9023e-10 0.00086239 0.00054704 0.00070166 v omega 11.217 1.0313e+05 2663.8 496.47 v TempK 288 342.16 294.5 291.4 v Density 1.205 1.205 1.205 1.205 v TurbVisc 4.572e-15 9.2649e-05 5.3464e-05 7.0199e-05 v CourantNb 3.3403e-09 0.00018381 1.3902e-05 9.1894e-06 v FourierNb 0.08229 0.6281 0.18031 0.15094 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9628 4.9628 0.00058202 -6.0414e-07 v volume_forces[Z] -4.9628 4.9628 -0.00058194 7.133e-07 v ǁvolume_forcesǁ 1.5565e-08 4.9637 0.58809 0.30428 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.71 291.54 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014456 5.1155e-05 2.8482e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.082298 0.6281 0.18032 0.15095 INSTANT 0.951444000E+00 TIME STEP NUMBER 988 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.71600E-05 0.21724E-02 Friction velocity uk : 0.71602E-05 0.21723E-02 Dimensionless distance yplus : 0.47679E-04 0.14453E-01 Friction thermal sca. tstar : -0.11289E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.33486E-04 0.10151E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.71600E-05 0.21724E-02 Friction velocity uk : 0.71602E-05 0.21723E-02 Dimensionless distance yplus : 0.47679E-04 0.14453E-01 Friction thermal sca. tstar : -0.11289E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.33486E-04 0.10151E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.39659E-08 3 0.76347E-07 0.13329E-12 0.71187E+00 c Velocity[X] 0.28674E-32 c Velocity[Y] 0.66638E-13 c Velocity[Z] 0.66652E-13 c Pressure 0.57603E-14 16 0.44681E-07 0.44681E-07 0.79366E+00 c k 0.25442E-06 2 0.25220E-07 0.68558E-09 0.11306E+01 c omega 0.13153E+02 1 0.66653E-09 0.85374E-01 0.15211E-02 c TempK 0.94817E+02 1 0.62303E-07 0.13824E-01 0.12996E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.378e-14 7.0368e-14 -8.7736e-18 -2.3023e-18 v Velocity[Y] -0.00011899 0.000112 -1.1615e-10 -2.8084e-12 v Velocity[Z] -0.0001119 0.00011899 -1.7122e-10 -1.3746e-12 v ǁVelocityǁ 4.4165e-10 0.00012749 1.1842e-05 9.051e-06 v Pressure -0.0016594 0.025216 0.0014647 -3.677e-20 v k 3.8917e-10 0.00086154 0.00054641 0.00070088 v omega 11.207 1.0313e+05 2663.8 496.46 v TempK 288 342.16 294.5 291.4 v Density 1.205 1.205 1.205 1.205 v TurbVisc 4.5596e-15 9.264e-05 5.3449e-05 7.0181e-05 v CourantNb 3.3419e-09 0.00018376 1.3903e-05 9.1924e-06 v FourierNb 0.082232 0.6281 0.18028 0.15091 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9628 4.9628 0.00058219 -6.0434e-07 v volume_forces[Z] -4.9628 4.9628 -0.00058211 7.1352e-07 v ǁvolume_forcesǁ 1.5764e-08 4.9638 0.58827 0.30443 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.71 291.54 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014453 5.1144e-05 2.8475e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.08224 0.6281 0.18029 0.15092 INSTANT 0.952407000E+00 TIME STEP NUMBER 989 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.72325E-05 0.21719E-02 Friction velocity uk : 0.72327E-05 0.21719E-02 Dimensionless distance yplus : 0.48162E-04 0.14450E-01 Friction thermal sca. tstar : -0.11346E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.33826E-04 0.10149E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.72325E-05 0.21719E-02 Friction velocity uk : 0.72327E-05 0.21719E-02 Dimensionless distance yplus : 0.48162E-04 0.14450E-01 Friction thermal sca. tstar : -0.11346E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.33826E-04 0.10149E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.39672E-08 3 0.76199E-07 0.13294E-12 0.71084E+00 c Velocity[X] 0.28584E-32 c Velocity[Y] 0.66463E-13 c Velocity[Z] 0.66478E-13 c Pressure 0.57594E-14 16 0.44673E-07 0.44673E-07 0.79282E+00 c k 0.25415E-06 2 0.25185E-07 0.68294E-09 0.11296E+01 c omega 0.13153E+02 1 0.66505E-09 0.85064E-01 0.15184E-02 c TempK 0.94818E+02 1 0.62214E-07 0.13803E-01 0.12986E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.374e-14 7.0337e-14 -8.7699e-18 -2.3014e-18 v Velocity[Y] -0.00011896 0.00011198 -1.1368e-10 -2.806e-12 v Velocity[Z] -0.00011188 0.00011897 -1.7365e-10 -1.3741e-12 v ǁVelocityǁ 4.4728e-10 0.00012747 1.1845e-05 9.056e-06 v Pressure -0.001661 0.025229 0.0014655 -7.8442e-22 v k 3.8812e-10 0.0008607 0.00054579 0.0007001 v omega 11.198 1.0313e+05 2663.8 496.46 v TempK 288 342.16 294.5 291.4 v Density 1.205 1.205 1.205 1.205 v TurbVisc 4.5472e-15 9.2631e-05 5.3434e-05 7.0164e-05 v CourantNb 3.3435e-09 0.00018371 1.3903e-05 9.1953e-06 v FourierNb 0.082175 0.6281 0.18025 0.15088 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9629 4.9629 0.00058237 -6.0455e-07 v volume_forces[Z] -4.9629 4.9629 -0.00058229 7.1374e-07 v ǁvolume_forcesǁ 1.5966e-08 4.9638 0.58844 0.30458 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.71 291.54 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.01445 5.1134e-05 2.8469e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.082183 0.6281 0.18026 0.15089 INSTANT 0.953370000E+00 TIME STEP NUMBER 990 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.73045E-05 0.21715E-02 Friction velocity uk : 0.73046E-05 0.21715E-02 Dimensionless distance yplus : 0.48641E-04 0.14447E-01 Friction thermal sca. tstar : -0.11404E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.34162E-04 0.10147E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.73045E-05 0.21715E-02 Friction velocity uk : 0.73046E-05 0.21715E-02 Dimensionless distance yplus : 0.48641E-04 0.14447E-01 Friction thermal sca. tstar : -0.11404E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.34162E-04 0.10147E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.39686E-08 3 0.76051E-07 0.13259E-12 0.70980E+00 c Velocity[X] 0.28495E-32 c Velocity[Y] 0.66289E-13 c Velocity[Z] 0.66303E-13 c Pressure 0.57428E-14 16 0.44544E-07 0.44544E-07 0.79198E+00 c k 0.25388E-06 2 0.25150E-07 0.68031E-09 0.11286E+01 c omega 0.13153E+02 1 0.66358E-09 0.84755E-01 0.15156E-02 c TempK 0.94818E+02 1 0.62124E-07 0.13782E-01 0.12976E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.3701e-14 7.0306e-14 -8.7661e-18 -2.3006e-18 v Velocity[Y] -0.00011894 0.00011195 -1.1121e-10 -2.8035e-12 v Velocity[Z] -0.00011185 0.00011895 -1.7607e-10 -1.3736e-12 v ǁVelocityǁ 4.5294e-10 0.00012744 1.1848e-05 9.061e-06 v Pressure -0.0016626 0.025241 0.0014663 1.2806e-19 v k 3.8706e-10 0.00085986 0.00054517 0.00069933 v omega 11.188 1.0313e+05 2663.8 496.45 v TempK 288 342.16 294.51 291.4 v Density 1.205 1.205 1.205 1.205 v TurbVisc 4.5349e-15 9.2622e-05 5.342e-05 7.0146e-05 v CourantNb 3.3451e-09 0.00018366 1.3904e-05 9.1983e-06 v FourierNb 0.082118 0.6281 0.18022 0.15085 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9629 4.9629 0.00058254 -6.0475e-07 v volume_forces[Z] -4.9629 4.9629 -0.00058246 7.1395e-07 v ǁvolume_forcesǁ 1.6169e-08 4.9639 0.58861 0.30473 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.71 291.54 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014447 5.1123e-05 2.8463e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.082126 0.6281 0.18024 0.15086 INSTANT 0.954333000E+00 TIME STEP NUMBER 991 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.73759E-05 0.21710E-02 Friction velocity uk : 0.73760E-05 0.21710E-02 Dimensionless distance yplus : 0.49116E-04 0.14444E-01 Friction thermal sca. tstar : -0.11463E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.34496E-04 0.10145E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.73759E-05 0.21710E-02 Friction velocity uk : 0.73760E-05 0.21710E-02 Dimensionless distance yplus : 0.49116E-04 0.14444E-01 Friction thermal sca. tstar : -0.11463E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.34496E-04 0.10145E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.39699E-08 3 0.75910E-07 0.13224E-12 0.70877E+00 c Velocity[X] 0.28406E-32 c Velocity[Y] 0.66114E-13 c Velocity[Z] 0.66129E-13 c Pressure 0.57351E-14 16 0.44484E-07 0.44484E-07 0.79114E+00 c k 0.25360E-06 2 0.25115E-07 0.67769E-09 0.11277E+01 c omega 0.13153E+02 1 0.66210E-09 0.84447E-01 0.15129E-02 c TempK 0.94819E+02 1 0.62035E-07 0.13761E-01 0.12966E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.3662e-14 7.0275e-14 -8.7624e-18 -2.2997e-18 v Velocity[Y] -0.00011892 0.00011193 -1.0874e-10 -2.801e-12 v Velocity[Z] -0.00011183 0.00011893 -1.7848e-10 -1.3731e-12 v ǁVelocityǁ 4.5866e-10 0.00012742 1.1851e-05 9.0659e-06 v Pressure -0.0016643 0.025253 0.0014672 -8.7267e-21 v k 3.8601e-10 0.00085903 0.00054454 0.00069855 v omega 11.178 1.0313e+05 2663.8 496.44 v TempK 288 342.16 294.51 291.4 v Density 1.205 1.205 1.205 1.205 v TurbVisc 4.5226e-15 9.2613e-05 5.3405e-05 7.0128e-05 v CourantNb 3.3467e-09 0.0001836 1.3904e-05 9.2012e-06 v FourierNb 0.082061 0.6281 0.1802 0.15082 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9629 4.9629 0.00058272 -6.0495e-07 v volume_forces[Z] -4.9629 4.9629 -0.00058264 7.1417e-07 v ǁvolume_forcesǁ 1.6374e-08 4.9639 0.58878 0.30488 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.71 291.54 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014444 5.1113e-05 2.8457e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.082069 0.6281 0.18021 0.15083 INSTANT 0.955296000E+00 TIME STEP NUMBER 992 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.74467E-05 0.21706E-02 Friction velocity uk : 0.74469E-05 0.21706E-02 Dimensionless distance yplus : 0.49588E-04 0.14441E-01 Friction thermal sca. tstar : -0.11522E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.34827E-04 0.10143E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.74467E-05 0.21706E-02 Friction velocity uk : 0.74469E-05 0.21706E-02 Dimensionless distance yplus : 0.49588E-04 0.14441E-01 Friction thermal sca. tstar : -0.11522E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.34827E-04 0.10143E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.39713E-08 3 0.75768E-07 0.13189E-12 0.70773E+00 c Velocity[X] 0.28318E-32 c Velocity[Y] 0.65940E-13 c Velocity[Z] 0.65954E-13 c Pressure 0.57261E-14 16 0.44413E-07 0.44413E-07 0.79030E+00 c k 0.25333E-06 2 0.25080E-07 0.67508E-09 0.11267E+01 c omega 0.13153E+02 1 0.66063E-09 0.84141E-01 0.15101E-02 c TempK 0.94819E+02 1 0.61946E-07 0.13740E-01 0.12956E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.3623e-14 7.0244e-14 -8.7587e-18 -2.2989e-18 v Velocity[Y] -0.0001189 0.00011191 -1.0628e-10 -2.7986e-12 v Velocity[Z] -0.00011181 0.0001189 -1.809e-10 -1.3725e-12 v ǁVelocityǁ 4.6442e-10 0.00012739 1.1855e-05 9.0709e-06 v Pressure -0.0016659 0.025265 0.001468 6.9421e-20 v k 3.8497e-10 0.00085819 0.00054392 0.00069778 v omega 11.168 1.0313e+05 2663.7 496.43 v TempK 288 342.16 294.51 291.41 v Density 1.205 1.205 1.205 1.205 v TurbVisc 4.5103e-15 9.2604e-05 5.339e-05 7.0111e-05 v CourantNb 3.3482e-09 0.00018355 1.3904e-05 9.2042e-06 v FourierNb 0.082004 0.6281 0.18017 0.15079 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.963 4.963 0.00058289 -6.0516e-07 v volume_forces[Z] -4.963 4.963 -0.00058281 7.1439e-07 v ǁvolume_forcesǁ 1.6581e-08 4.9639 0.58895 0.30504 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.72 291.55 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014441 5.1103e-05 2.8451e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.082012 0.6281 0.18018 0.1508 INSTANT 0.956259000E+00 TIME STEP NUMBER 993 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.75171E-05 0.21702E-02 Friction velocity uk : 0.75172E-05 0.21701E-02 Dimensionless distance yplus : 0.50056E-04 0.14438E-01 Friction thermal sca. tstar : -0.11583E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.35156E-04 0.10141E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.75171E-05 0.21702E-02 Friction velocity uk : 0.75172E-05 0.21701E-02 Dimensionless distance yplus : 0.50056E-04 0.14438E-01 Friction thermal sca. tstar : -0.11583E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.35156E-04 0.10141E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.39726E-08 3 0.75626E-07 0.13155E-12 0.70670E+00 c Velocity[X] 0.28230E-32 c Velocity[Y] 0.65766E-13 c Velocity[Z] 0.65780E-13 c Pressure 0.57211E-14 16 0.44375E-07 0.44375E-07 0.78947E+00 c k 0.25306E-06 2 0.25045E-07 0.67249E-09 0.11257E+01 c omega 0.13153E+02 1 0.65917E-09 0.83836E-01 0.15074E-02 c TempK 0.94820E+02 1 0.61857E-07 0.13719E-01 0.12946E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.3584e-14 7.0213e-14 -8.755e-18 -2.298e-18 v Velocity[Y] -0.00011887 0.00011189 -1.0381e-10 -2.7962e-12 v Velocity[Z] -0.00011179 0.00011888 -1.8331e-10 -1.372e-12 v ǁVelocityǁ 4.7023e-10 0.00012737 1.1858e-05 9.0758e-06 v Pressure -0.0016676 0.025278 0.0014689 -1.6865e-20 v k 3.8393e-10 0.00085736 0.0005433 0.00069701 v omega 11.158 1.0313e+05 2663.7 496.42 v TempK 288 342.17 294.51 291.41 v Density 1.205 1.205 1.205 1.205 v TurbVisc 4.4981e-15 9.2595e-05 5.3376e-05 7.0093e-05 v CourantNb 3.3498e-09 0.0001835 1.3905e-05 9.2071e-06 v FourierNb 0.081947 0.6281 0.18014 0.15076 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.963 4.963 0.00058306 -6.0536e-07 v volume_forces[Z] -4.963 4.963 -0.00058298 7.1461e-07 v ǁvolume_forcesǁ 1.6789e-08 4.964 0.58912 0.30519 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.72 291.55 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014438 5.1092e-05 2.8445e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.081955 0.6281 0.18015 0.15077 INSTANT 0.957222000E+00 TIME STEP NUMBER 994 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.75869E-05 0.21697E-02 Friction velocity uk : 0.75870E-05 0.21697E-02 Dimensionless distance yplus : 0.50521E-04 0.14435E-01 Friction thermal sca. tstar : -0.11644E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.35483E-04 0.10138E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.75869E-05 0.21697E-02 Friction velocity uk : 0.75870E-05 0.21697E-02 Dimensionless distance yplus : 0.50521E-04 0.14435E-01 Friction thermal sca. tstar : -0.11644E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.35483E-04 0.10138E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.39739E-08 3 0.75497E-07 0.13120E-12 0.70566E+00 c Velocity[X] 0.28143E-32 c Velocity[Y] 0.65592E-13 c Velocity[Z] 0.65607E-13 c Pressure 0.57118E-14 16 0.44302E-07 0.44302E-07 0.78863E+00 c k 0.25279E-06 2 0.25011E-07 0.66991E-09 0.11248E+01 c omega 0.13153E+02 1 0.65771E-09 0.83533E-01 0.15047E-02 c TempK 0.94821E+02 1 0.61769E-07 0.13699E-01 0.12936E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.3545e-14 7.0182e-14 -8.7513e-18 -2.2971e-18 v Velocity[Y] -0.00011885 0.00011187 -1.0145e-10 -2.8897e-12 v Velocity[Z] -0.00011177 0.00011886 -1.856e-10 -1.2498e-12 v ǁVelocityǁ 4.7559e-10 0.00012734 1.1861e-05 9.0807e-06 v Pressure -0.0016692 0.02529 0.0014697 1.0825e-19 v k 3.8289e-10 0.00085652 0.00054268 0.00069624 v omega 11.149 1.0313e+05 2663.7 496.41 v TempK 288 342.17 294.51 291.41 v Density 1.205 1.205 1.205 1.205 v TurbVisc 4.4859e-15 9.2586e-05 5.3361e-05 7.0075e-05 v CourantNb 3.3514e-09 0.00018344 1.3905e-05 9.2101e-06 v FourierNb 0.08189 0.6281 0.18011 0.15073 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.963 4.963 0.00058324 -6.0556e-07 v volume_forces[Z] -4.963 4.963 -0.00058316 7.1482e-07 v ǁvolume_forcesǁ 1.6999e-08 4.964 0.58929 0.30534 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.72 291.55 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014435 5.1082e-05 2.8439e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.081899 0.6281 0.18013 0.15074 INSTANT 0.958185000E+00 TIME STEP NUMBER 995 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.76504E-05 0.21693E-02 Friction velocity uk : 0.76505E-05 0.21693E-02 Dimensionless distance yplus : 0.50944E-04 0.14432E-01 Friction thermal sca. tstar : -0.11706E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.35780E-04 0.10136E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.76504E-05 0.21693E-02 Friction velocity uk : 0.76505E-05 0.21693E-02 Dimensionless distance yplus : 0.50944E-04 0.14432E-01 Friction thermal sca. tstar : -0.11706E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.35780E-04 0.10136E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.39753E-08 3 0.75340E-07 0.13085E-12 0.70463E+00 c Velocity[X] 0.28056E-32 c Velocity[Y] 0.65419E-13 c Velocity[Z] 0.65433E-13 c Pressure 0.57018E-14 16 0.44223E-07 0.44223E-07 0.78780E+00 c k 0.25252E-06 2 0.24976E-07 0.66734E-09 0.11238E+01 c omega 0.13153E+02 1 0.65626E-09 0.83230E-01 0.15019E-02 c TempK 0.94821E+02 1 0.61681E-07 0.13678E-01 0.12926E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.3506e-14 7.0152e-14 -8.7477e-18 -2.2963e-18 v Velocity[Y] -0.00011883 0.00011185 -9.8978e-11 -2.8832e-12 v Velocity[Z] -0.00011174 0.00011883 -1.8801e-10 -1.2452e-12 v ǁVelocityǁ 4.8165e-10 0.00012732 1.1864e-05 9.0856e-06 v Pressure -0.0016708 0.025302 0.0014705 3.5299e-20 v k 3.8186e-10 0.00085569 0.00054207 0.00069547 v omega 11.139 1.0313e+05 2663.7 496.4 v TempK 288 342.17 294.52 291.41 v Density 1.205 1.205 1.205 1.205 v TurbVisc 4.4738e-15 9.2578e-05 5.3346e-05 7.0058e-05 v CourantNb 3.3529e-09 0.00018339 1.3906e-05 9.213e-06 v FourierNb 0.081834 0.6281 0.18009 0.1507 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9631 4.9631 0.00058341 -6.0576e-07 v volume_forces[Z] -4.9631 4.9631 -0.00058333 7.1504e-07 v ǁvolume_forcesǁ 1.7192e-08 4.964 0.58947 0.30549 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.72 291.55 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014432 5.1071e-05 2.8433e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.081842 0.6281 0.1801 0.15071 INSTANT 0.959148000E+00 TIME STEP NUMBER 996 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.77213E-05 0.21688E-02 Friction velocity uk : 0.77214E-05 0.21688E-02 Dimensionless distance yplus : 0.51416E-04 0.14430E-01 Friction thermal sca. tstar : -0.11769E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.36111E-04 0.10134E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.77213E-05 0.21688E-02 Friction velocity uk : 0.77214E-05 0.21688E-02 Dimensionless distance yplus : 0.51416E-04 0.14430E-01 Friction thermal sca. tstar : -0.11769E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.36111E-04 0.10134E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.39766E-08 3 0.75199E-07 0.13050E-12 0.70359E+00 c Velocity[X] 0.27969E-32 c Velocity[Y] 0.65245E-13 c Velocity[Z] 0.65260E-13 c Pressure 0.56952E-14 16 0.44172E-07 0.44172E-07 0.78697E+00 c k 0.25225E-06 2 0.24942E-07 0.66479E-09 0.11229E+01 c omega 0.13153E+02 1 0.65481E-09 0.82930E-01 0.14992E-02 c TempK 0.94822E+02 1 0.61593E-07 0.13657E-01 0.12916E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.3467e-14 7.0121e-14 -8.744e-18 -2.2954e-18 v Velocity[Y] -0.00011881 0.00011183 -9.6516e-11 -2.8826e-12 v Velocity[Z] -0.00011172 0.00011881 -1.9042e-10 -1.247e-12 v ǁVelocityǁ 4.8764e-10 0.00012729 1.1867e-05 9.0906e-06 v Pressure -0.0016725 0.025314 0.0014713 -2.8337e-20 v k 3.8083e-10 0.00085486 0.00054145 0.0006947 v omega 11.129 1.0313e+05 2663.7 496.4 v TempK 288 342.17 294.52 291.41 v Density 1.205 1.205 1.205 1.205 v TurbVisc 4.4617e-15 9.2569e-05 5.3332e-05 7.004e-05 v CourantNb 3.3545e-09 0.00018334 1.3906e-05 9.2159e-06 v FourierNb 0.081778 0.6281 0.18006 0.15067 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9631 4.9631 0.00058358 -6.0596e-07 v volume_forces[Z] -4.9631 4.9631 -0.0005835 7.1526e-07 v ǁvolume_forcesǁ 1.7412e-08 4.9641 0.58964 0.30564 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.72 291.55 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.01443 5.1061e-05 2.8427e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.081786 0.6281 0.18007 0.15068 INSTANT 0.960111000E+00 TIME STEP NUMBER 997 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.77904E-05 0.21684E-02 Friction velocity uk : 0.77905E-05 0.21684E-02 Dimensionless distance yplus : 0.51876E-04 0.14427E-01 Friction thermal sca. tstar : -0.11834E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.36435E-04 0.10132E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.77904E-05 0.21684E-02 Friction velocity uk : 0.77905E-05 0.21684E-02 Dimensionless distance yplus : 0.51876E-04 0.14427E-01 Friction thermal sca. tstar : -0.11834E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.36435E-04 0.10132E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.39779E-08 3 0.75059E-07 0.13016E-12 0.70256E+00 c Velocity[X] 0.27882E-32 c Velocity[Y] 0.65072E-13 c Velocity[Z] 0.65086E-13 c Pressure 0.56851E-14 16 0.44094E-07 0.44094E-07 0.78614E+00 c k 0.25199E-06 2 0.24907E-07 0.66224E-09 0.11219E+01 c omega 0.13153E+02 1 0.65336E-09 0.82630E-01 0.14965E-02 c TempK 0.94822E+02 1 0.61505E-07 0.13637E-01 0.12907E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.3428e-14 7.009e-14 -8.7403e-18 -2.2946e-18 v Velocity[Y] -0.00011878 0.0001118 -9.4054e-11 -2.8804e-12 v Velocity[Z] -0.0001117 0.00011879 -1.9282e-10 -1.2463e-12 v ǁVelocityǁ 4.9366e-10 0.00012727 1.187e-05 9.0955e-06 v Pressure -0.0016741 0.025327 0.0014722 1.2355e-20 v k 3.798e-10 0.00085404 0.00054084 0.00069393 v omega 11.119 1.0313e+05 2663.7 496.39 v TempK 288 342.17 294.52 291.41 v Density 1.205 1.205 1.205 1.205 v TurbVisc 4.4497e-15 9.256e-05 5.3317e-05 7.0023e-05 v CourantNb 3.356e-09 0.00018329 1.3907e-05 9.2189e-06 v FourierNb 0.081721 0.6281 0.18003 0.15064 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9631 4.9632 0.00058375 -6.0616e-07 v volume_forces[Z] -4.9631 4.9632 -0.00058368 7.1547e-07 v ǁvolume_forcesǁ 1.7628e-08 4.9641 0.58981 0.30579 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.72 291.55 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014427 5.1051e-05 2.842e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.081729 0.6281 0.18004 0.15065 INSTANT 0.961074000E+00 TIME STEP NUMBER 998 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.78588E-05 0.21680E-02 Friction velocity uk : 0.78589E-05 0.21679E-02 Dimensionless distance yplus : 0.52332E-04 0.14424E-01 Friction thermal sca. tstar : -0.11899E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.36754E-04 0.10130E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.78588E-05 0.21680E-02 Friction velocity uk : 0.78589E-05 0.21679E-02 Dimensionless distance yplus : 0.52332E-04 0.14424E-01 Friction thermal sca. tstar : -0.11899E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.36754E-04 0.10130E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.39793E-08 3 0.74943E-07 0.12981E-12 0.70152E+00 c Velocity[X] 0.27797E-32 c Velocity[Y] 0.64899E-13 c Velocity[Z] 0.64913E-13 c Pressure 0.57153E-14 16 0.44327E-07 0.44327E-07 0.78532E+00 c k 0.25172E-06 2 0.24873E-07 0.65971E-09 0.11210E+01 c omega 0.13153E+02 1 0.65192E-09 0.82332E-01 0.14938E-02 c TempK 0.94823E+02 1 0.61417E-07 0.13616E-01 0.12897E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.3389e-14 7.0059e-14 -8.7366e-18 -2.2937e-18 v Velocity[Y] -0.00011876 0.00011178 -9.1605e-11 -2.8902e-12 v Velocity[Z] -0.00011168 0.00011877 -1.9523e-10 -1.2497e-12 v ǁVelocityǁ 4.9968e-10 0.00012724 1.1873e-05 9.1003e-06 v Pressure -0.0016758 0.025339 0.001473 -1.3316e-19 v k 3.7878e-10 0.00085321 0.00054022 0.00069317 v omega 11.11 1.0313e+05 2663.7 496.38 v TempK 288 342.17 294.52 291.42 v Density 1.205 1.205 1.205 1.205 v TurbVisc 4.4377e-15 9.2551e-05 5.3303e-05 7.0005e-05 v CourantNb 3.3575e-09 0.00018323 1.3907e-05 9.2218e-06 v FourierNb 0.081665 0.6281 0.18 0.15062 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9632 4.9632 0.00058393 -6.0636e-07 v volume_forces[Z] -4.9632 4.9632 -0.00058385 7.1569e-07 v ǁvolume_forcesǁ 1.7846e-08 4.9641 0.58998 0.30595 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.73 291.56 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014424 5.104e-05 2.8414e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.081673 0.6281 0.18002 0.15062 INSTANT 0.962037000E+00 TIME STEP NUMBER 999 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.79264E-05 0.21675E-02 Friction velocity uk : 0.79265E-05 0.21675E-02 Dimensionless distance yplus : 0.52781E-04 0.14421E-01 Friction thermal sca. tstar : -0.11965E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.37070E-04 0.10128E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.79264E-05 0.21675E-02 Friction velocity uk : 0.79265E-05 0.21675E-02 Dimensionless distance yplus : 0.52781E-04 0.14421E-01 Friction thermal sca. tstar : -0.11965E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.37070E-04 0.10128E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.39806E-08 3 0.74781E-07 0.12947E-12 0.70049E+00 c Velocity[X] 0.27712E-32 c Velocity[Y] 0.64726E-13 c Velocity[Z] 0.64741E-13 c Pressure 0.56711E-14 16 0.43984E-07 0.43984E-07 0.78449E+00 c k 0.25145E-06 2 0.24838E-07 0.65719E-09 0.11200E+01 c omega 0.13153E+02 1 0.65048E-09 0.82035E-01 0.14911E-02 c TempK 0.94823E+02 1 0.61330E-07 0.13596E-01 0.12887E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.335e-14 7.0029e-14 -8.733e-18 -2.2929e-18 v Velocity[Y] -0.00011874 0.00011176 -8.9145e-11 -2.888e-12 v Velocity[Z] -0.00011166 0.00011874 -1.9763e-10 -1.2487e-12 v ǁVelocityǁ 5.0576e-10 0.00012722 1.1876e-05 9.1052e-06 v Pressure -0.0016774 0.025351 0.0014738 -5.6675e-20 v k 3.7776e-10 0.00085238 0.00053961 0.00069241 v omega 11.1 1.0313e+05 2663.7 496.37 v TempK 288 342.17 294.52 291.42 v Density 1.205 1.205 1.205 1.205 v TurbVisc 4.4258e-15 9.2542e-05 5.3288e-05 6.9988e-05 v CourantNb 3.359e-09 0.00018318 1.3908e-05 9.2247e-06 v FourierNb 0.081609 0.6281 0.17998 0.15059 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9632 4.9632 0.0005841 -6.0656e-07 v volume_forces[Z] -4.9632 4.9632 -0.00058402 7.1591e-07 v ǁvolume_forcesǁ 1.8063e-08 4.9642 0.59015 0.3061 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.73 291.56 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014421 5.103e-05 2.8408e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.081617 0.6281 0.17999 0.1506 INSTANT 0.963000000E+00 TIME STEP NUMBER 1000 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.79936E-05 0.21671E-02 Friction velocity uk : 0.79937E-05 0.21671E-02 Dimensionless distance yplus : 0.53230E-04 0.14418E-01 Friction thermal sca. tstar : -0.12032E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.37385E-04 0.10126E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.79936E-05 0.21671E-02 Friction velocity uk : 0.79937E-05 0.21671E-02 Dimensionless distance yplus : 0.53230E-04 0.14418E-01 Friction thermal sca. tstar : -0.12032E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.37385E-04 0.10126E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.39819E-08 3 0.74648E-07 0.12912E-12 0.69946E+00 c Velocity[X] 0.27626E-32 c Velocity[Y] 0.64553E-13 c Velocity[Z] 0.64568E-13 c Pressure 0.56977E-14 16 0.44190E-07 0.44190E-07 0.78367E+00 c k 0.25118E-06 2 0.24804E-07 0.65468E-09 0.11191E+01 c omega 0.13153E+02 1 0.64905E-09 0.81740E-01 0.14884E-02 c TempK 0.94824E+02 1 0.61242E-07 0.13575E-01 0.12877E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.3312e-14 6.9998e-14 -8.7293e-18 -2.292e-18 v Velocity[Y] -0.00011872 0.00011174 -8.6686e-11 -2.8854e-12 v Velocity[Z] -0.00011164 0.00011872 -2.0003e-10 -1.2483e-12 v ǁVelocityǁ 5.1187e-10 0.0001272 1.1879e-05 9.1101e-06 v Pressure -0.0016791 0.025363 0.0014747 -5.3929e-20 v k 3.7675e-10 0.00085156 0.000539 0.00069165 v omega 11.09 1.0313e+05 2663.7 496.36 v TempK 288 342.17 294.53 291.42 v Density 1.205 1.205 1.205 1.205 v TurbVisc 4.4139e-15 9.2533e-05 5.3274e-05 6.997e-05 v CourantNb 3.3606e-09 0.00018313 1.3908e-05 9.2276e-06 v FourierNb 0.081553 0.6281 0.17995 0.15056 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9632 4.9633 0.00058427 -6.0676e-07 v volume_forces[Z] -4.9632 4.9633 -0.00058419 7.1612e-07 v ǁvolume_forcesǁ 1.8283e-08 4.9642 0.59032 0.30625 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.73 291.56 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014418 5.102e-05 2.8402e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.081561 0.6281 0.17996 0.15057 INSTANT 0.963963000E+00 TIME STEP NUMBER 1001 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.80604E-05 0.21667E-02 Friction velocity uk : 0.80605E-05 0.21666E-02 Dimensionless distance yplus : 0.53674E-04 0.14415E-01 Friction thermal sca. tstar : -0.12101E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.37697E-04 0.10124E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.80604E-05 0.21667E-02 Friction velocity uk : 0.80605E-05 0.21666E-02 Dimensionless distance yplus : 0.53674E-04 0.14415E-01 Friction thermal sca. tstar : -0.12101E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.37697E-04 0.10124E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.39833E-08 3 0.74505E-07 0.12878E-12 0.69843E+00 c Velocity[X] 0.27541E-32 c Velocity[Y] 0.64381E-13 c Velocity[Z] 0.64396E-13 c Pressure 0.56798E-14 16 0.44051E-07 0.44051E-07 0.78285E+00 c k 0.25092E-06 2 0.24770E-07 0.65218E-09 0.11181E+01 c omega 0.13153E+02 1 0.64762E-09 0.81446E-01 0.14857E-02 c TempK 0.94824E+02 1 0.61155E-07 0.13555E-01 0.12867E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.3273e-14 6.9968e-14 -8.7256e-18 -2.2912e-18 v Velocity[Y] -0.00011869 0.00011172 -8.4229e-11 -2.883e-12 v Velocity[Z] -0.00011161 0.0001187 -2.0243e-10 -1.2477e-12 v ǁVelocityǁ 5.1801e-10 0.00012717 1.1882e-05 9.115e-06 v Pressure -0.0016807 0.025375 0.0014755 4.8928e-20 v k 3.7573e-10 0.00085074 0.00053839 0.00069089 v omega 11.081 1.0313e+05 2663.7 496.35 v TempK 288 342.17 294.53 291.42 v Density 1.205 1.205 1.205 1.205 v TurbVisc 4.402e-15 9.2524e-05 5.3259e-05 6.9952e-05 v CourantNb 3.3621e-09 0.00018308 1.3909e-05 9.2305e-06 v FourierNb 0.081497 0.6281 0.17992 0.15053 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9633 4.9633 0.00058444 -6.0696e-07 v volume_forces[Z] -4.9633 4.9633 -0.00058437 7.1633e-07 v ǁvolume_forcesǁ 1.8504e-08 4.9642 0.59049 0.3064 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.73 291.56 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014415 5.1009e-05 2.8396e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.081506 0.6281 0.17994 0.15054 INSTANT 0.964926000E+00 TIME STEP NUMBER 1002 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.81267E-05 0.21662E-02 Friction velocity uk : 0.81268E-05 0.21662E-02 Dimensionless distance yplus : 0.54115E-04 0.14412E-01 Friction thermal sca. tstar : -0.12170E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.38007E-04 0.10122E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.81267E-05 0.21662E-02 Friction velocity uk : 0.81268E-05 0.21662E-02 Dimensionless distance yplus : 0.54115E-04 0.14412E-01 Friction thermal sca. tstar : -0.12170E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.38007E-04 0.10122E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.39846E-08 3 0.74368E-07 0.12843E-12 0.69740E+00 c Velocity[X] 0.27456E-32 c Velocity[Y] 0.64209E-13 c Velocity[Z] 0.64224E-13 c Pressure 0.56696E-14 16 0.43971E-07 0.43971E-07 0.78203E+00 c k 0.25065E-06 2 0.24736E-07 0.64970E-09 0.11172E+01 c omega 0.13153E+02 1 0.64619E-09 0.81153E-01 0.14831E-02 c TempK 0.94825E+02 1 0.61068E-07 0.13534E-01 0.12858E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.3234e-14 6.9937e-14 -8.722e-18 -2.2903e-18 v Velocity[Y] -0.00011867 0.0001117 -8.1773e-11 -2.8804e-12 v Velocity[Z] -0.00011159 0.00011868 -2.0482e-10 -1.2473e-12 v ǁVelocityǁ 5.2419e-10 0.00012715 1.1885e-05 9.1198e-06 v Pressure -0.0016823 0.025388 0.0014763 6.0793e-21 v k 3.7473e-10 0.00084992 0.00053778 0.00069013 v omega 11.071 1.0313e+05 2663.7 496.35 v TempK 288 342.17 294.53 291.42 v Density 1.205 1.205 1.205 1.205 v TurbVisc 4.3902e-15 9.2516e-05 5.3245e-05 6.9935e-05 v CourantNb 3.3636e-09 0.00018302 1.3909e-05 9.2334e-06 v FourierNb 0.081442 0.6281 0.17989 0.1505 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9633 4.9633 0.00058462 -6.0716e-07 v volume_forces[Z] -4.9633 4.9633 -0.00058454 7.1655e-07 v ǁvolume_forcesǁ 1.8726e-08 4.9643 0.59066 0.30655 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.73 291.56 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014412 5.0999e-05 2.839e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.08145 0.6281 0.17991 0.15051 INSTANT 0.965889000E+00 TIME STEP NUMBER 1003 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.81926E-05 0.21658E-02 Friction velocity uk : 0.81926E-05 0.21658E-02 Dimensionless distance yplus : 0.54554E-04 0.14409E-01 Friction thermal sca. tstar : -0.12241E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.38315E-04 0.10120E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.81926E-05 0.21658E-02 Friction velocity uk : 0.81926E-05 0.21658E-02 Dimensionless distance yplus : 0.54554E-04 0.14409E-01 Friction thermal sca. tstar : -0.12241E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.38315E-04 0.10120E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.39859E-08 3 0.74223E-07 0.12809E-12 0.69636E+00 c Velocity[X] 0.27372E-32 c Velocity[Y] 0.64037E-13 c Velocity[Z] 0.64052E-13 c Pressure 0.56361E-14 16 0.43711E-07 0.43711E-07 0.78121E+00 c k 0.25039E-06 2 0.24702E-07 0.64723E-09 0.11162E+01 c omega 0.13153E+02 1 0.64477E-09 0.80862E-01 0.14804E-02 c TempK 0.94825E+02 1 0.60982E-07 0.13514E-01 0.12848E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.3196e-14 6.9907e-14 -8.7184e-18 -2.2895e-18 v Velocity[Y] -0.00011865 0.00011168 -7.9318e-11 -2.878e-12 v Velocity[Z] -0.00011157 0.00011865 -2.0722e-10 -1.2468e-12 v ǁVelocityǁ 5.304e-10 0.00012712 1.1888e-05 9.1247e-06 v Pressure -0.001684 0.0254 0.0014772 1.0982e-20 v k 3.7372e-10 0.0008491 0.00053717 0.00068937 v omega 11.061 1.0313e+05 2663.7 496.34 v TempK 288 342.17 294.53 291.43 v Density 1.205 1.205 1.205 1.205 v TurbVisc 4.3784e-15 9.2507e-05 5.323e-05 6.9917e-05 v CourantNb 3.3651e-09 0.00018297 1.391e-05 9.2363e-06 v FourierNb 0.081386 0.6281 0.17987 0.15047 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9633 4.9634 0.00058479 -6.0736e-07 v volume_forces[Z] -4.9633 4.9634 -0.00058471 7.1676e-07 v ǁvolume_forcesǁ 1.895e-08 4.9643 0.59083 0.3067 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.74 291.56 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014409 5.0989e-05 2.8384e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.081395 0.6281 0.17988 0.15048 INSTANT 0.966852000E+00 TIME STEP NUMBER 1004 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.82580E-05 0.21654E-02 Friction velocity uk : 0.82581E-05 0.21653E-02 Dimensionless distance yplus : 0.54990E-04 0.14406E-01 Friction thermal sca. tstar : -0.12313E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.38621E-04 0.10118E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.82580E-05 0.21654E-02 Friction velocity uk : 0.82581E-05 0.21653E-02 Dimensionless distance yplus : 0.54990E-04 0.14406E-01 Friction thermal sca. tstar : -0.12313E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.38621E-04 0.10118E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.39872E-08 3 0.85173E-07 0.12775E-12 0.69533E+00 c Velocity[X] 0.27288E-32 c Velocity[Y] 0.63865E-13 c Velocity[Z] 0.63880E-13 c Pressure 0.56364E-14 16 0.43713E-07 0.43713E-07 0.78039E+00 c k 0.25012E-06 2 0.24668E-07 0.64476E-09 0.11153E+01 c omega 0.13153E+02 1 0.64336E-09 0.80571E-01 0.14777E-02 c TempK 0.94826E+02 1 0.60895E-07 0.13494E-01 0.12838E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.3157e-14 6.9876e-14 -8.7147e-18 -2.2887e-18 v Velocity[Y] -0.00011862 0.00011166 -7.6864e-11 -2.8756e-12 v Velocity[Z] -0.00011155 0.00011863 -2.0961e-10 -1.2463e-12 v ǁVelocityǁ 5.3665e-10 0.0001271 1.1891e-05 9.1295e-06 v Pressure -0.0016856 0.025412 0.001478 -1.0315e-19 v k 3.7272e-10 0.00084828 0.00053657 0.00068861 v omega 11.052 1.0313e+05 2663.7 496.33 v TempK 288 342.17 294.53 291.43 v Density 1.205 1.205 1.205 1.205 v TurbVisc 4.3667e-15 9.2498e-05 5.3216e-05 6.99e-05 v CourantNb 3.3666e-09 0.00018292 1.391e-05 9.2392e-06 v FourierNb 0.081331 0.6281 0.17984 0.15044 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9634 4.9634 0.00058496 -6.0756e-07 v volume_forces[Z] -4.9634 4.9634 -0.00058488 7.1697e-07 v ǁvolume_forcesǁ 1.9174e-08 4.9643 0.591 0.30685 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.74 291.57 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014406 5.0979e-05 2.8378e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.081339 0.6281 0.17985 0.15045 INSTANT 0.967815000E+00 TIME STEP NUMBER 1005 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.83230E-05 0.21649E-02 Friction velocity uk : 0.83231E-05 0.21649E-02 Dimensionless distance yplus : 0.55423E-04 0.14403E-01 Friction thermal sca. tstar : -0.12386E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.38925E-04 0.10116E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.83230E-05 0.21649E-02 Friction velocity uk : 0.83231E-05 0.21649E-02 Dimensionless distance yplus : 0.55423E-04 0.14403E-01 Friction thermal sca. tstar : -0.12386E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.38925E-04 0.10116E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.39885E-08 3 0.73951E-07 0.12740E-12 0.69430E+00 c Velocity[X] 0.27204E-32 c Velocity[Y] 0.63694E-13 c Velocity[Z] 0.63709E-13 c Pressure 0.56264E-14 16 0.43635E-07 0.43635E-07 0.77958E+00 c k 0.24986E-06 2 0.24634E-07 0.64231E-09 0.11143E+01 c omega 0.13153E+02 1 0.64194E-09 0.80282E-01 0.14751E-02 c TempK 0.94826E+02 1 0.60809E-07 0.13474E-01 0.12829E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.3119e-14 6.9846e-14 -8.7111e-18 -2.2878e-18 v Velocity[Y] -0.0001186 0.00011164 -7.4413e-11 -2.8732e-12 v Velocity[Z] -0.00011153 0.00011861 -2.12e-10 -1.2457e-12 v ǁVelocityǁ 5.4293e-10 0.00012707 1.1894e-05 9.1344e-06 v Pressure -0.0016873 0.025424 0.0014788 1.0698e-19 v k 3.7173e-10 0.00084747 0.00053596 0.00068786 v omega 11.042 1.0313e+05 2663.7 496.32 v TempK 288 342.17 294.53 291.43 v Density 1.205 1.205 1.205 1.205 v TurbVisc 4.355e-15 9.2489e-05 5.3201e-05 6.9883e-05 v CourantNb 3.368e-09 0.00018287 1.3911e-05 9.2421e-06 v FourierNb 0.081276 0.6281 0.17981 0.15041 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9634 4.9634 0.00058513 -6.0776e-07 v volume_forces[Z] -4.9634 4.9634 -0.00058505 7.1719e-07 v ǁvolume_forcesǁ 1.94e-08 4.9644 0.59117 0.307 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.74 291.57 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014403 5.0968e-05 2.8372e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.081284 0.6281 0.17983 0.15042 INSTANT 0.968778000E+00 TIME STEP NUMBER 1006 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.83877E-05 0.21645E-02 Friction velocity uk : 0.83878E-05 0.21645E-02 Dimensionless distance yplus : 0.55853E-04 0.14401E-01 Friction thermal sca. tstar : -0.12460E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.39228E-04 0.10114E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.83877E-05 0.21645E-02 Friction velocity uk : 0.83878E-05 0.21645E-02 Dimensionless distance yplus : 0.55853E-04 0.14401E-01 Friction thermal sca. tstar : -0.12460E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.39228E-04 0.10114E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.39899E-08 3 0.73811E-07 0.12706E-12 0.69327E+00 c Velocity[X] 0.27121E-32 c Velocity[Y] 0.63522E-13 c Velocity[Z] 0.63537E-13 c Pressure 0.56116E-14 16 0.43519E-07 0.43519E-07 0.77876E+00 c k 0.24959E-06 2 0.24601E-07 0.63987E-09 0.11134E+01 c omega 0.13153E+02 1 0.64054E-09 0.79995E-01 0.14724E-02 c TempK 0.94827E+02 1 0.60723E-07 0.13454E-01 0.12819E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.3081e-14 6.9815e-14 -8.7075e-18 -2.287e-18 v Velocity[Y] -0.00011858 0.00011161 -7.1962e-11 -2.8708e-12 v Velocity[Z] -0.00011151 0.00011858 -2.1438e-10 -1.2452e-12 v ǁVelocityǁ 5.4924e-10 0.00012705 1.1897e-05 9.1392e-06 v Pressure -0.0016889 0.025436 0.0014796 -4.3535e-20 v k 3.7073e-10 0.00084665 0.00053536 0.00068711 v omega 11.033 1.0313e+05 2663.7 496.31 v TempK 288 342.17 294.54 291.43 v Density 1.205 1.205 1.205 1.205 v TurbVisc 4.3434e-15 9.248e-05 5.3187e-05 6.9865e-05 v CourantNb 3.3695e-09 0.00018282 1.3911e-05 9.2449e-06 v FourierNb 0.081221 0.6281 0.17979 0.15038 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9634 4.9635 0.0005853 -6.0796e-07 v volume_forces[Z] -4.9634 4.9635 -0.00058523 7.174e-07 v ǁvolume_forcesǁ 1.9627e-08 4.9644 0.59134 0.30715 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.74 291.57 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014401 5.0958e-05 2.8366e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.081229 0.6281 0.1798 0.15039 INSTANT 0.969741000E+00 TIME STEP NUMBER 1007 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.84519E-05 0.21641E-02 Friction velocity uk : 0.84520E-05 0.21640E-02 Dimensionless distance yplus : 0.56281E-04 0.14398E-01 Friction thermal sca. tstar : -0.12536E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.39528E-04 0.10112E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.84519E-05 0.21641E-02 Friction velocity uk : 0.84520E-05 0.21640E-02 Dimensionless distance yplus : 0.56281E-04 0.14398E-01 Friction thermal sca. tstar : -0.12536E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.39528E-04 0.10112E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.39912E-08 3 0.73680E-07 0.12672E-12 0.69224E+00 c Velocity[X] 0.27038E-32 c Velocity[Y] 0.63352E-13 c Velocity[Z] 0.63367E-13 c Pressure 0.56238E-14 16 0.43614E-07 0.43614E-07 0.77795E+00 c k 0.24933E-06 2 0.24567E-07 0.63745E-09 0.11125E+01 c omega 0.13153E+02 1 0.63913E-09 0.79709E-01 0.14698E-02 c TempK 0.94827E+02 1 0.60637E-07 0.13434E-01 0.12809E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.3042e-14 6.9785e-14 -8.7038e-18 -2.2861e-18 v Velocity[Y] -0.00011856 0.00011159 -6.9513e-11 -2.8684e-12 v Velocity[Z] -0.00011149 0.00011856 -2.1677e-10 -1.2446e-12 v ǁVelocityǁ 5.5559e-10 0.00012702 1.19e-05 9.144e-06 v Pressure -0.0016905 0.025449 0.0014805 9.8053e-22 v k 3.6975e-10 0.00084584 0.00053475 0.00068636 v omega 11.023 1.0313e+05 2663.7 496.3 v TempK 288 342.17 294.54 291.43 v Density 1.205 1.205 1.205 1.205 v TurbVisc 4.3318e-15 9.2472e-05 5.3172e-05 6.9848e-05 v CourantNb 3.371e-09 0.00018277 1.3912e-05 9.2478e-06 v FourierNb 0.081166 0.6281 0.17976 0.15035 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9635 4.9635 0.00058547 -6.0815e-07 v volume_forces[Z] -4.9635 4.9635 -0.0005854 7.1761e-07 v ǁvolume_forcesǁ 1.9855e-08 4.9644 0.59151 0.30731 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.74 291.57 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014398 5.0948e-05 2.836e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.081174 0.6281 0.17977 0.15036 INSTANT 0.970704000E+00 TIME STEP NUMBER 1008 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.85158E-05 0.21636E-02 Friction velocity uk : 0.85159E-05 0.21636E-02 Dimensionless distance yplus : 0.56707E-04 0.14395E-01 Friction thermal sca. tstar : -0.12613E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.39827E-04 0.10110E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.85158E-05 0.21636E-02 Friction velocity uk : 0.85159E-05 0.21636E-02 Dimensionless distance yplus : 0.56707E-04 0.14395E-01 Friction thermal sca. tstar : -0.12613E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.39827E-04 0.10110E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.39925E-08 3 0.73541E-07 0.12638E-12 0.69121E+00 c Velocity[X] 0.26956E-32 c Velocity[Y] 0.63181E-13 c Velocity[Z] 0.63196E-13 c Pressure 0.55954E-14 16 0.43393E-07 0.43393E-07 0.77714E+00 c k 0.24907E-06 2 0.24533E-07 0.63503E-09 0.11115E+01 c omega 0.13153E+02 1 0.63773E-09 0.79423E-01 0.14672E-02 c TempK 0.94828E+02 1 0.60552E-07 0.13413E-01 0.12800E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.3004e-14 6.9755e-14 -8.7002e-18 -2.2853e-18 v Velocity[Y] -0.00011853 0.00011157 -6.7065e-11 -2.866e-12 v Velocity[Z] -0.00011146 0.00011854 -2.1915e-10 -1.244e-12 v ǁVelocityǁ 5.6197e-10 0.000127 1.1903e-05 9.1488e-06 v Pressure -0.0016922 0.025461 0.0014813 -3.6574e-20 v k 3.6876e-10 0.00084503 0.00053415 0.00068561 v omega 11.014 1.0313e+05 2663.6 496.3 v TempK 288 342.17 294.54 291.43 v Density 1.205 1.205 1.205 1.205 v TurbVisc 4.3202e-15 9.2463e-05 5.3158e-05 6.983e-05 v CourantNb 3.3725e-09 0.00018271 1.3912e-05 9.2507e-06 v FourierNb 0.081111 0.6281 0.17973 0.15032 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9635 4.9635 0.00058565 -6.0835e-07 v volume_forces[Z] -4.9635 4.9635 -0.00058557 7.1782e-07 v ǁvolume_forcesǁ 2.0085e-08 4.9645 0.59168 0.30746 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.75 291.57 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014395 5.0937e-05 2.8354e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.081119 0.6281 0.17975 0.15033 INSTANT 0.971667000E+00 TIME STEP NUMBER 1009 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.85794E-05 0.21632E-02 Friction velocity uk : 0.85794E-05 0.21632E-02 Dimensionless distance yplus : 0.57130E-04 0.14392E-01 Friction thermal sca. tstar : -0.12691E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.40124E-04 0.10108E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.85794E-05 0.21632E-02 Friction velocity uk : 0.85794E-05 0.21632E-02 Dimensionless distance yplus : 0.57130E-04 0.14392E-01 Friction thermal sca. tstar : -0.12691E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.40124E-04 0.10108E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.39938E-08 3 0.73403E-07 0.12604E-12 0.69018E+00 c Velocity[X] 0.26874E-32 c Velocity[Y] 0.63010E-13 c Velocity[Z] 0.63025E-13 c Pressure 0.55872E-14 16 0.43330E-07 0.43330E-07 0.77634E+00 c k 0.24881E-06 2 0.24500E-07 0.63263E-09 0.11106E+01 c omega 0.13153E+02 1 0.63634E-09 0.79140E-01 0.14646E-02 c TempK 0.94828E+02 1 0.60466E-07 0.13393E-01 0.12790E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.2966e-14 6.9725e-14 -8.6966e-18 -2.2845e-18 v Velocity[Y] -0.00011851 0.00011155 -6.4619e-11 -2.8636e-12 v Velocity[Z] -0.00011144 0.00011852 -2.2153e-10 -1.2435e-12 v ǁVelocityǁ 5.6838e-10 0.00012697 1.1906e-05 9.1536e-06 v Pressure -0.0016938 0.025473 0.0014821 -1.7669e-19 v k 3.6778e-10 0.00084422 0.00053355 0.00068486 v omega 11.004 1.0313e+05 2663.6 496.29 v TempK 288 342.17 294.54 291.44 v Density 1.205 1.205 1.205 1.205 v TurbVisc 4.3087e-15 9.2454e-05 5.3144e-05 6.9813e-05 v CourantNb 3.3739e-09 0.00018266 1.3912e-05 9.2535e-06 v FourierNb 0.081056 0.6281 0.1797 0.15029 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9635 4.9636 0.00058582 -6.0855e-07 v volume_forces[Z] -4.9635 4.9636 -0.00058574 7.1803e-07 v ǁvolume_forcesǁ 2.0315e-08 4.9645 0.59185 0.30761 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.75 291.58 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014392 5.0927e-05 2.8348e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.081064 0.6281 0.17972 0.1503 INSTANT 0.972630000E+00 TIME STEP NUMBER 1010 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.86426E-05 0.21628E-02 Friction velocity uk : 0.86426E-05 0.21628E-02 Dimensionless distance yplus : 0.57550E-04 0.14389E-01 Friction thermal sca. tstar : -0.12771E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.40420E-04 0.10106E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.86426E-05 0.21628E-02 Friction velocity uk : 0.86426E-05 0.21628E-02 Dimensionless distance yplus : 0.57550E-04 0.14389E-01 Friction thermal sca. tstar : -0.12771E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.40420E-04 0.10106E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.39951E-08 3 0.73267E-07 0.12569E-12 0.68916E+00 c Velocity[X] 0.26792E-32 c Velocity[Y] 0.62840E-13 c Velocity[Z] 0.62855E-13 c Pressure 0.55795E-14 16 0.43269E-07 0.43269E-07 0.77553E+00 c k 0.24854E-06 2 0.24466E-07 0.63023E-09 0.11097E+01 c omega 0.13153E+02 1 0.63495E-09 0.78857E-01 0.14619E-02 c TempK 0.94829E+02 1 0.60381E-07 0.13374E-01 0.12780E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.2928e-14 6.9695e-14 -8.693e-18 -2.2836e-18 v Velocity[Y] -0.00011849 0.00011153 -6.2174e-11 -2.8613e-12 v Velocity[Z] -0.00011142 0.00011849 -2.239e-10 -1.2429e-12 v ǁVelocityǁ 5.7483e-10 0.00012695 1.1909e-05 9.1584e-06 v Pressure -0.0016955 0.025485 0.0014829 6.5499e-20 v k 3.668e-10 0.00084341 0.00053295 0.00068411 v omega 10.995 1.0313e+05 2663.6 496.28 v TempK 288 342.17 294.54 291.44 v Density 1.205 1.205 1.205 1.205 v TurbVisc 4.2972e-15 9.2445e-05 5.3129e-05 6.9795e-05 v CourantNb 3.3754e-09 0.00018261 1.3913e-05 9.2564e-06 v FourierNb 0.081001 0.6281 0.17968 0.15027 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9636 4.9636 0.00058599 -6.0875e-07 v volume_forces[Z] -4.9636 4.9636 -0.00058591 7.1824e-07 v ǁvolume_forcesǁ 2.0547e-08 4.9645 0.59201 0.30776 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.75 291.58 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014389 5.0917e-05 2.8342e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.08101 0.6281 0.17969 0.15027 INSTANT 0.973593000E+00 TIME STEP NUMBER 1011 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.87054E-05 0.21624E-02 Friction velocity uk : 0.87055E-05 0.21623E-02 Dimensionless distance yplus : 0.57969E-04 0.14386E-01 Friction thermal sca. tstar : -0.12852E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.40714E-04 0.10104E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.87054E-05 0.21624E-02 Friction velocity uk : 0.87055E-05 0.21623E-02 Dimensionless distance yplus : 0.57969E-04 0.14386E-01 Friction thermal sca. tstar : -0.12852E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.40714E-04 0.10104E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.39964E-08 3 0.19448E-06 0.12535E-12 0.68813E+00 c Velocity[X] 0.26710E-32 c Velocity[Y] 0.62670E-13 c Velocity[Z] 0.62685E-13 c Pressure 0.56239E-14 16 0.43613E-07 0.43613E-07 0.77472E+00 c k 0.24828E-06 2 0.24433E-07 0.62785E-09 0.11087E+01 c omega 0.13153E+02 1 0.63356E-09 0.78576E-01 0.14593E-02 c TempK 0.94829E+02 1 0.60296E-07 0.13354E-01 0.12771E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.289e-14 6.9665e-14 -8.6894e-18 -2.2828e-18 v Velocity[Y] -0.00011846 0.00011151 -5.973e-11 -2.859e-12 v Velocity[Z] -0.0001114 0.00011847 -2.2628e-10 -1.2424e-12 v ǁVelocityǁ 5.813e-10 0.00012692 1.1912e-05 9.1632e-06 v Pressure -0.0016971 0.025497 0.0014838 1.8434e-20 v k 3.6582e-10 0.0008426 0.00053235 0.00068337 v omega 10.985 1.0313e+05 2663.6 496.27 v TempK 288 342.17 294.55 291.44 v Density 1.205 1.205 1.205 1.205 v TurbVisc 4.2858e-15 9.2436e-05 5.3115e-05 6.9778e-05 v CourantNb 3.3768e-09 0.00018256 1.3913e-05 9.2592e-06 v FourierNb 0.080947 0.6281 0.17965 0.15024 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9636 4.9636 0.00058616 -6.0894e-07 v volume_forces[Z] -4.9636 4.9636 -0.00058608 7.1845e-07 v ǁvolume_forcesǁ 2.078e-08 4.9646 0.59218 0.30791 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.75 291.58 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014386 5.0907e-05 2.8336e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.080955 0.6281 0.17966 0.15025 INSTANT 0.974556000E+00 TIME STEP NUMBER 1012 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.87679E-05 0.21619E-02 Friction velocity uk : 0.87680E-05 0.21619E-02 Dimensionless distance yplus : 0.58385E-04 0.14383E-01 Friction thermal sca. tstar : -0.12935E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.41006E-04 0.10102E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.87679E-05 0.21619E-02 Friction velocity uk : 0.87680E-05 0.21619E-02 Dimensionless distance yplus : 0.58385E-04 0.14383E-01 Friction thermal sca. tstar : -0.12935E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.41006E-04 0.10102E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.39977E-08 3 0.73089E-07 0.12501E-12 0.68710E+00 c Velocity[X] 0.26629E-32 c Velocity[Y] 0.62500E-13 c Velocity[Z] 0.62515E-13 c Pressure 0.56766E-14 16 0.44021E-07 0.44021E-07 0.77392E+00 c k 0.24802E-06 2 0.24400E-07 0.62548E-09 0.11078E+01 c omega 0.13153E+02 1 0.63218E-09 0.78296E-01 0.14567E-02 c TempK 0.94830E+02 1 0.60212E-07 0.13334E-01 0.12761E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.2852e-14 6.9635e-14 -8.6858e-18 -2.282e-18 v Velocity[Y] -0.00011844 0.00011149 -5.7287e-11 -2.8554e-12 v Velocity[Z] -0.00011138 0.00011845 -2.2865e-10 -1.239e-12 v ǁVelocityǁ 5.878e-10 0.0001269 1.1915e-05 9.1679e-06 v Pressure -0.0016987 0.025509 0.0014846 9.315e-21 v k 3.6485e-10 0.0008418 0.00053176 0.00068262 v omega 10.976 1.0313e+05 2663.6 496.26 v TempK 288 342.17 294.55 291.44 v Density 1.205 1.205 1.205 1.205 v TurbVisc 4.2744e-15 9.2428e-05 5.3101e-05 6.9761e-05 v CourantNb 3.3782e-09 0.00018251 1.3914e-05 9.2621e-06 v FourierNb 0.080892 0.6281 0.17962 0.15021 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9636 4.9637 0.00058633 -6.0914e-07 v volume_forces[Z] -4.9636 4.9637 -0.00058625 7.1866e-07 v ǁvolume_forcesǁ 2.1014e-08 4.9646 0.59235 0.30806 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.75 291.58 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014383 5.0896e-05 2.833e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.080901 0.6281 0.17964 0.15022 INSTANT 0.975519000E+00 TIME STEP NUMBER 1013 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.88300E-05 0.21615E-02 Friction velocity uk : 0.88301E-05 0.21615E-02 Dimensionless distance yplus : 0.58799E-04 0.14381E-01 Friction thermal sca. tstar : -0.13019E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.41296E-04 0.10100E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.88300E-05 0.21615E-02 Friction velocity uk : 0.88301E-05 0.21615E-02 Dimensionless distance yplus : 0.58799E-04 0.14381E-01 Friction thermal sca. tstar : -0.13019E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.41296E-04 0.10100E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.39990E-08 3 0.72866E-07 0.12468E-12 0.68607E+00 c Velocity[X] 0.26548E-32 c Velocity[Y] 0.62330E-13 c Velocity[Z] 0.62345E-13 c Pressure 0.55616E-14 16 0.43129E-07 0.43129E-07 0.77312E+00 c k 0.24776E-06 2 0.24367E-07 0.62312E-09 0.11069E+01 c omega 0.13153E+02 1 0.63080E-09 0.78017E-01 0.14541E-02 c TempK 0.94830E+02 1 0.60127E-07 0.13314E-01 0.12752E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.2814e-14 6.9605e-14 -8.6822e-18 -2.2811e-18 v Velocity[Y] -0.00011842 0.00011147 -5.4847e-11 -2.853e-12 v Velocity[Z] -0.00011136 0.00011842 -2.3102e-10 -1.2385e-12 v ǁVelocityǁ 5.9434e-10 0.00012687 1.1918e-05 9.1727e-06 v Pressure -0.0017004 0.025521 0.0014854 -8.2364e-21 v k 3.6388e-10 0.00084099 0.00053116 0.00068188 v omega 10.966 1.0313e+05 2663.6 496.25 v TempK 288 342.17 294.55 291.44 v Density 1.205 1.205 1.205 1.205 v TurbVisc 4.263e-15 9.2419e-05 5.3086e-05 6.9743e-05 v CourantNb 3.3796e-09 0.00018246 1.3914e-05 9.2649e-06 v FourierNb 0.080838 0.6281 0.1796 0.15018 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9637 4.9637 0.0005865 -6.0934e-07 v volume_forces[Z] -4.9637 4.9637 -0.00058642 7.1887e-07 v ǁvolume_forcesǁ 2.1249e-08 4.9646 0.59252 0.30821 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.76 291.58 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014381 5.0886e-05 2.8324e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.080846 0.6281 0.17961 0.15019 INSTANT 0.976482000E+00 TIME STEP NUMBER 1014 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.88919E-05 0.21611E-02 Friction velocity uk : 0.88920E-05 0.21610E-02 Dimensionless distance yplus : 0.59211E-04 0.14378E-01 Friction thermal sca. tstar : -0.13105E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.41586E-04 0.10098E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.88919E-05 0.21611E-02 Friction velocity uk : 0.88920E-05 0.21610E-02 Dimensionless distance yplus : 0.59211E-04 0.14378E-01 Friction thermal sca. tstar : -0.13105E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.41586E-04 0.10098E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.40003E-08 3 0.72734E-07 0.12434E-12 0.68505E+00 c Velocity[X] 0.26468E-32 c Velocity[Y] 0.62160E-13 c Velocity[Z] 0.62176E-13 c Pressure 0.55474E-14 16 0.43019E-07 0.43019E-07 0.77232E+00 c k 0.24750E-06 2 0.24333E-07 0.62077E-09 0.11060E+01 c omega 0.13153E+02 1 0.62943E-09 0.77739E-01 0.14515E-02 c TempK 0.94831E+02 1 0.60043E-07 0.13294E-01 0.12742E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.2776e-14 6.9575e-14 -8.6787e-18 -2.2803e-18 v Velocity[Y] -0.00011839 0.00011145 -5.2408e-11 -2.8507e-12 v Velocity[Z] -0.00011133 0.0001184 -2.3338e-10 -1.2379e-12 v ǁVelocityǁ 6.009e-10 0.00012685 1.1921e-05 9.1774e-06 v Pressure -0.001702 0.025533 0.0014862 -3.1377e-21 v k 3.6292e-10 0.00084019 0.00053057 0.00068114 v omega 10.957 1.0313e+05 2663.6 496.25 v TempK 288 342.17 294.55 291.44 v Density 1.205 1.205 1.205 1.205 v TurbVisc 4.2517e-15 9.241e-05 5.3072e-05 6.9726e-05 v CourantNb 3.3811e-09 0.0001824 1.3915e-05 9.2677e-06 v FourierNb 0.080784 0.6281 0.17957 0.15015 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9637 4.9637 0.00058667 -6.0953e-07 v volume_forces[Z] -4.9637 4.9637 -0.00058659 7.1908e-07 v ǁvolume_forcesǁ 2.1485e-08 4.9647 0.59269 0.30836 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.76 291.58 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014378 5.0876e-05 2.8318e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.080792 0.6281 0.17958 0.15016 INSTANT 0.977445000E+00 TIME STEP NUMBER 1015 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.89535E-05 0.21606E-02 Friction velocity uk : 0.89536E-05 0.21606E-02 Dimensionless distance yplus : 0.59621E-04 0.14375E-01 Friction thermal sca. tstar : -0.13193E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.41874E-04 0.10096E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.89535E-05 0.21606E-02 Friction velocity uk : 0.89536E-05 0.21606E-02 Dimensionless distance yplus : 0.59621E-04 0.14375E-01 Friction thermal sca. tstar : -0.13193E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.41874E-04 0.10096E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.40016E-08 3 0.72602E-07 0.12400E-12 0.68402E+00 c Velocity[X] 0.26388E-32 c Velocity[Y] 0.61991E-13 c Velocity[Z] 0.62006E-13 c Pressure 0.55508E-14 16 0.43044E-07 0.43044E-07 0.77152E+00 c k 0.24724E-06 2 0.24300E-07 0.61843E-09 0.11050E+01 c omega 0.13153E+02 1 0.62806E-09 0.77463E-01 0.14490E-02 c TempK 0.94831E+02 1 0.59959E-07 0.13275E-01 0.12733E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.2738e-14 6.9545e-14 -8.6751e-18 -2.2795e-18 v Velocity[Y] -0.00011837 0.00011142 -4.997e-11 -2.8484e-12 v Velocity[Z] -0.00011131 0.00011838 -2.3575e-10 -1.2373e-12 v ǁVelocityǁ 6.075e-10 0.00012682 1.1924e-05 9.1822e-06 v Pressure -0.0017037 0.025545 0.0014871 1.21e-19 v k 3.6196e-10 0.00083939 0.00052997 0.0006804 v omega 10.947 1.0313e+05 2663.6 496.24 v TempK 288 342.17 294.55 291.45 v Density 1.205 1.205 1.205 1.205 v TurbVisc 4.2405e-15 9.2401e-05 5.3058e-05 6.9709e-05 v CourantNb 3.3825e-09 0.00018235 1.3915e-05 9.2706e-06 v FourierNb 0.08073 0.6281 0.17954 0.15012 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9638 4.9638 0.00058684 -6.0973e-07 v volume_forces[Z] -4.9638 4.9638 -0.00058677 7.1929e-07 v ǁvolume_forcesǁ 2.1723e-08 4.9647 0.59286 0.30851 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.76 291.59 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014375 5.0866e-05 2.8312e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.080738 0.6281 0.17956 0.15013 INSTANT 0.978408000E+00 TIME STEP NUMBER 1016 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.90148E-05 0.21602E-02 Friction velocity uk : 0.90148E-05 0.21602E-02 Dimensionless distance yplus : 0.60029E-04 0.14372E-01 Friction thermal sca. tstar : -0.13282E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.42160E-04 0.10094E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.90148E-05 0.21602E-02 Friction velocity uk : 0.90148E-05 0.21602E-02 Dimensionless distance yplus : 0.60029E-04 0.14372E-01 Friction thermal sca. tstar : -0.13282E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.42160E-04 0.10094E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.40029E-08 3 0.83650E-07 0.12366E-12 0.68300E+00 c Velocity[X] 0.26308E-32 c Velocity[Y] 0.61822E-13 c Velocity[Z] 0.61837E-13 c Pressure 0.55383E-14 16 0.42947E-07 0.42947E-07 0.77072E+00 c k 0.24698E-06 2 0.24267E-07 0.61610E-09 0.11041E+01 c omega 0.13153E+02 1 0.62669E-09 0.77188E-01 0.14464E-02 c TempK 0.94832E+02 1 0.59875E-07 0.13255E-01 0.12723E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.2701e-14 6.9515e-14 -8.6715e-18 -2.2787e-18 v Velocity[Y] -0.00011835 0.0001114 -4.7534e-11 -2.8461e-12 v Velocity[Z] -0.00011129 0.00011835 -2.3811e-10 -1.2367e-12 v ǁVelocityǁ 6.1412e-10 0.0001268 1.1927e-05 9.1869e-06 v Pressure -0.0017053 0.025558 0.0014879 1.3884e-19 v k 3.61e-10 0.00083859 0.00052938 0.00067966 v omega 10.938 1.0313e+05 2663.6 496.23 v TempK 288 342.17 294.56 291.45 v Density 1.205 1.205 1.205 1.205 v TurbVisc 4.2292e-15 9.2393e-05 5.3043e-05 6.9691e-05 v CourantNb 3.3839e-09 0.0001823 1.3916e-05 9.2734e-06 v FourierNb 0.080676 0.6281 0.17952 0.15009 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9638 4.9638 0.00058701 -6.0992e-07 v volume_forces[Z] -4.9638 4.9638 -0.00058694 7.195e-07 v ǁvolume_forcesǁ 2.1961e-08 4.9647 0.59302 0.30866 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.76 291.59 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014372 5.0856e-05 2.8306e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.080684 0.6281 0.17953 0.1501 INSTANT 0.979371000E+00 TIME STEP NUMBER 1017 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.90757E-05 0.21598E-02 Friction velocity uk : 0.90758E-05 0.21598E-02 Dimensionless distance yplus : 0.60435E-04 0.14369E-01 Friction thermal sca. tstar : -0.13373E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.42445E-04 0.10092E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.90757E-05 0.21598E-02 Friction velocity uk : 0.90758E-05 0.21598E-02 Dimensionless distance yplus : 0.60435E-04 0.14369E-01 Friction thermal sca. tstar : -0.13373E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.42445E-04 0.10092E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.40042E-08 3 0.72334E-07 0.12332E-12 0.68197E+00 c Velocity[X] 0.26228E-32 c Velocity[Y] 0.61653E-13 c Velocity[Z] 0.61669E-13 c Pressure 0.55310E-14 16 0.42890E-07 0.42890E-07 0.76993E+00 c k 0.24673E-06 2 0.24234E-07 0.61378E-09 0.11032E+01 c omega 0.13153E+02 1 0.62533E-09 0.76914E-01 0.14438E-02 c TempK 0.94832E+02 1 0.59791E-07 0.13235E-01 0.12714E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.2663e-14 6.9485e-14 -8.668e-18 -2.2778e-18 v Velocity[Y] -0.00011832 0.00011138 -4.51e-11 -2.8438e-12 v Velocity[Z] -0.00011127 0.00011833 -2.4047e-10 -1.236e-12 v ǁVelocityǁ 6.2077e-10 0.00012677 1.193e-05 9.1916e-06 v Pressure -0.0017069 0.02557 0.0014887 -9.0797e-20 v k 3.6005e-10 0.00083779 0.00052879 0.00067892 v omega 10.929 1.0313e+05 2663.6 496.22 v TempK 288 342.17 294.56 291.45 v Density 1.205 1.205 1.205 1.205 v TurbVisc 4.218e-15 9.2384e-05 5.3029e-05 6.9674e-05 v CourantNb 3.3853e-09 0.00018225 1.3916e-05 9.2762e-06 v FourierNb 0.080622 0.6281 0.17949 0.15006 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9638 4.9638 0.00058718 -6.1012e-07 v volume_forces[Z] -4.9638 4.9638 -0.00058711 7.1971e-07 v ǁvolume_forcesǁ 2.22e-08 4.9648 0.59319 0.30881 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.76 291.59 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014369 5.0845e-05 2.83e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.08063 0.6281 0.1795 0.15007 INSTANT 0.980334000E+00 TIME STEP NUMBER 1018 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.91364E-05 0.21594E-02 Friction velocity uk : 0.91364E-05 0.21593E-02 Dimensionless distance yplus : 0.60839E-04 0.14366E-01 Friction thermal sca. tstar : -0.13466E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.42729E-04 0.10090E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.91364E-05 0.21594E-02 Friction velocity uk : 0.91364E-05 0.21593E-02 Dimensionless distance yplus : 0.60839E-04 0.14366E-01 Friction thermal sca. tstar : -0.13466E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.42729E-04 0.10090E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.40055E-08 3 0.72201E-07 0.12298E-12 0.68095E+00 c Velocity[X] 0.26148E-32 c Velocity[Y] 0.61485E-13 c Velocity[Z] 0.61500E-13 c Pressure 0.55226E-14 16 0.42824E-07 0.42824E-07 0.76913E+00 c k 0.24647E-06 2 0.24202E-07 0.61148E-09 0.11023E+01 c omega 0.13153E+02 1 0.62397E-09 0.76641E-01 0.14413E-02 c TempK 0.94833E+02 1 0.59707E-07 0.13216E-01 0.12704E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.2625e-14 6.9455e-14 -8.6644e-18 -2.277e-18 v Velocity[Y] -0.0001183 0.00011136 -4.2667e-11 -2.8415e-12 v Velocity[Z] -0.00011125 0.00011831 -2.4283e-10 -1.2354e-12 v ǁVelocityǁ 6.2745e-10 0.00012675 1.1933e-05 9.1964e-06 v Pressure -0.0017086 0.025582 0.0014895 -1.0845e-19 v k 3.591e-10 0.00083699 0.0005282 0.00067819 v omega 10.919 1.0313e+05 2663.6 496.21 v TempK 288 342.17 294.56 291.45 v Density 1.205 1.205 1.205 1.205 v TurbVisc 4.2069e-15 9.2375e-05 5.3015e-05 6.9657e-05 v CourantNb 3.3867e-09 0.0001822 1.3916e-05 9.279e-06 v FourierNb 0.080569 0.6281 0.17946 0.15003 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9639 4.9639 0.00058735 -6.1031e-07 v volume_forces[Z] -4.9639 4.9639 -0.00058728 7.1992e-07 v ǁvolume_forcesǁ 2.2441e-08 4.9648 0.59336 0.30896 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.76 291.59 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014366 5.0835e-05 2.8294e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.080577 0.6281 0.17948 0.15004 INSTANT 0.981297000E+00 TIME STEP NUMBER 1019 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.91968E-05 0.21589E-02 Friction velocity uk : 0.91968E-05 0.21589E-02 Dimensionless distance yplus : 0.61241E-04 0.14364E-01 Friction thermal sca. tstar : -0.13561E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.43011E-04 0.10088E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.91968E-05 0.21589E-02 Friction velocity uk : 0.91968E-05 0.21589E-02 Dimensionless distance yplus : 0.61241E-04 0.14364E-01 Friction thermal sca. tstar : -0.13561E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.43011E-04 0.10088E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.40068E-08 3 0.72065E-07 0.12265E-12 0.67992E+00 c Velocity[X] 0.26070E-32 c Velocity[Y] 0.61316E-13 c Velocity[Z] 0.61332E-13 c Pressure 0.55077E-14 16 0.42708E-07 0.42708E-07 0.76834E+00 c k 0.24621E-06 2 0.24169E-07 0.60918E-09 0.11014E+01 c omega 0.13153E+02 1 0.62262E-09 0.76370E-01 0.14387E-02 c TempK 0.94833E+02 1 0.59624E-07 0.13196E-01 0.12695E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.2588e-14 6.9426e-14 -8.6608e-18 -2.2762e-18 v Velocity[Y] -0.00011828 0.00011134 -4.0236e-11 -2.8392e-12 v Velocity[Z] -0.00011123 0.00011828 -2.4518e-10 -1.2347e-12 v ǁVelocityǁ 6.3416e-10 0.00012672 1.1936e-05 9.2011e-06 v Pressure -0.0017102 0.025594 0.0014903 -6.2852e-20 v k 3.5815e-10 0.0008362 0.00052761 0.00067745 v omega 10.91 1.0313e+05 2663.6 496.21 v TempK 288 342.17 294.56 291.45 v Density 1.205 1.205 1.205 1.205 v TurbVisc 4.1958e-15 9.2366e-05 5.3e-05 6.964e-05 v CourantNb 3.388e-09 0.00018215 1.3917e-05 9.2818e-06 v FourierNb 0.080515 0.6281 0.17944 0.15001 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9639 4.9639 0.00058752 -6.105e-07 v volume_forces[Z] -4.9639 4.9639 -0.00058745 7.2012e-07 v ǁvolume_forcesǁ 2.2682e-08 4.9648 0.59353 0.30911 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.77 291.59 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014364 5.0825e-05 2.8288e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.080523 0.6281 0.17945 0.15002 INSTANT 0.982260000E+00 TIME STEP NUMBER 1020 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.92569E-05 0.21585E-02 Friction velocity uk : 0.92569E-05 0.21585E-02 Dimensionless distance yplus : 0.61641E-04 0.14361E-01 Friction thermal sca. tstar : -0.13658E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.43293E-04 0.10086E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.92569E-05 0.21585E-02 Friction velocity uk : 0.92569E-05 0.21585E-02 Dimensionless distance yplus : 0.61641E-04 0.14361E-01 Friction thermal sca. tstar : -0.13658E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.43293E-04 0.10086E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.40080E-08 3 0.71938E-07 0.12231E-12 0.67890E+00 c Velocity[X] 0.25991E-32 c Velocity[Y] 0.61148E-13 c Velocity[Z] 0.61164E-13 c Pressure 0.55004E-14 16 0.42652E-07 0.42652E-07 0.76755E+00 c k 0.24595E-06 2 0.24136E-07 0.60690E-09 0.11004E+01 c omega 0.13153E+02 1 0.62127E-09 0.76099E-01 0.14361E-02 c TempK 0.94834E+02 1 0.59541E-07 0.13177E-01 0.12685E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.255e-14 6.9396e-14 -8.6573e-18 -2.2754e-18 v Velocity[Y] -0.00011825 0.00011132 -3.7806e-11 -2.8369e-12 v Velocity[Z] -0.00011121 0.00011826 -2.4753e-10 -1.2341e-12 v ǁVelocityǁ 6.409e-10 0.00012669 1.1938e-05 9.2058e-06 v Pressure -0.0017119 0.025606 0.0014912 -7.2853e-20 v k 3.572e-10 0.0008354 0.00052703 0.00067672 v omega 10.901 1.0313e+05 2663.6 496.2 v TempK 288 342.18 294.56 291.45 v Density 1.205 1.205 1.205 1.205 v TurbVisc 4.1847e-15 9.2358e-05 5.2986e-05 6.9622e-05 v CourantNb 3.3894e-09 0.0001821 1.3917e-05 9.2846e-06 v FourierNb 0.080462 0.6281 0.17941 0.14998 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9639 4.9639 0.00058769 -6.107e-07 v volume_forces[Z] -4.9639 4.9639 -0.00058762 7.2033e-07 v ǁvolume_forcesǁ 2.2925e-08 4.9649 0.5937 0.30926 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.77 291.59 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014361 5.0815e-05 2.8282e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.08047 0.6281 0.17942 0.14999 INSTANT 0.983223000E+00 TIME STEP NUMBER 1021 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.93167E-05 0.21581E-02 Friction velocity uk : 0.93167E-05 0.21581E-02 Dimensionless distance yplus : 0.62039E-04 0.14358E-01 Friction thermal sca. tstar : -0.13755E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.43572E-04 0.10084E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.93167E-05 0.21581E-02 Friction velocity uk : 0.93167E-05 0.21581E-02 Dimensionless distance yplus : 0.62039E-04 0.14358E-01 Friction thermal sca. tstar : -0.13755E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.43572E-04 0.10084E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.40093E-08 3 0.71809E-07 0.12198E-12 0.67788E+00 c Velocity[X] 0.25913E-32 c Velocity[Y] 0.60980E-13 c Velocity[Z] 0.60996E-13 c Pressure 0.54966E-14 16 0.42622E-07 0.42622E-07 0.76676E+00 c k 0.24570E-06 2 0.24103E-07 0.60462E-09 0.10995E+01 c omega 0.13153E+02 1 0.61992E-09 0.75830E-01 0.14336E-02 c TempK 0.94834E+02 1 0.59458E-07 0.13157E-01 0.12676E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.2513e-14 6.9366e-14 -8.6538e-18 -2.2746e-18 v Velocity[Y] -0.00011823 0.0001113 -3.5378e-11 -2.8347e-12 v Velocity[Z] -0.00011119 0.00011824 -2.4988e-10 -1.2334e-12 v ǁVelocityǁ 6.4766e-10 0.00012667 1.1941e-05 9.2104e-06 v Pressure -0.0017135 0.025618 0.001492 2.9318e-20 v k 3.5626e-10 0.00083461 0.00052644 0.00067599 v omega 10.891 1.0313e+05 2663.6 496.19 v TempK 288 342.18 294.57 291.46 v Density 1.205 1.205 1.205 1.205 v TurbVisc 4.1737e-15 9.2349e-05 5.2972e-05 6.9605e-05 v CourantNb 3.3908e-09 0.00018205 1.3918e-05 9.2874e-06 v FourierNb 0.080408 0.6281 0.17938 0.14995 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.964 4.964 0.00058786 -6.1089e-07 v volume_forces[Z] -4.964 4.964 -0.00058779 7.2054e-07 v ǁvolume_forcesǁ 2.3168e-08 4.9649 0.59386 0.30941 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.77 291.6 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014358 5.0805e-05 2.8276e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.080416 0.6281 0.1794 0.14996 INSTANT 0.984186000E+00 TIME STEP NUMBER 1022 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.93762E-05 0.21577E-02 Friction velocity uk : 0.93763E-05 0.21576E-02 Dimensionless distance yplus : 0.62436E-04 0.14355E-01 Friction thermal sca. tstar : -0.13855E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.43851E-04 0.10082E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.93762E-05 0.21577E-02 Friction velocity uk : 0.93763E-05 0.21576E-02 Dimensionless distance yplus : 0.62436E-04 0.14355E-01 Friction thermal sca. tstar : -0.13855E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.43851E-04 0.10082E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.40106E-08 3 0.71675E-07 0.12164E-12 0.67685E+00 c Velocity[X] 0.25835E-32 c Velocity[Y] 0.60813E-13 c Velocity[Z] 0.60828E-13 c Pressure 0.54849E-14 16 0.42530E-07 0.42530E-07 0.76597E+00 c k 0.24544E-06 2 0.24071E-07 0.60236E-09 0.10986E+01 c omega 0.13153E+02 1 0.61857E-09 0.75562E-01 0.14311E-02 c TempK 0.94835E+02 1 0.59375E-07 0.13138E-01 0.12666E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.2476e-14 6.9337e-14 -8.6502e-18 -2.2737e-18 v Velocity[Y] -0.00011821 0.00011128 -3.2952e-11 -2.8325e-12 v Velocity[Z] -0.00011116 0.00011821 -2.5223e-10 -1.2328e-12 v ǁVelocityǁ 6.5444e-10 0.00012664 1.1944e-05 9.2151e-06 v Pressure -0.0017151 0.02563 0.0014928 -2.9808e-20 v k 3.5533e-10 0.00083382 0.00052585 0.00067526 v omega 10.882 1.0313e+05 2663.6 496.18 v TempK 288 342.18 294.57 291.46 v Density 1.205 1.205 1.205 1.205 v TurbVisc 4.1627e-15 9.234e-05 5.2958e-05 6.9588e-05 v CourantNb 3.3921e-09 0.000182 1.3918e-05 9.2902e-06 v FourierNb 0.080355 0.6281 0.17936 0.14992 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.964 4.964 0.00058803 -6.1109e-07 v volume_forces[Z] -4.964 4.964 -0.00058796 7.2074e-07 v ǁvolume_forcesǁ 2.3413e-08 4.9649 0.59403 0.30956 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.77 291.6 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014355 5.0794e-05 2.827e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.080363 0.6281 0.17937 0.14993 INSTANT 0.985149000E+00 TIME STEP NUMBER 1023 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.94355E-05 0.21572E-02 Friction velocity uk : 0.94356E-05 0.21572E-02 Dimensionless distance yplus : 0.62830E-04 0.14352E-01 Friction thermal sca. tstar : -0.13958E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.44128E-04 0.10080E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.94355E-05 0.21572E-02 Friction velocity uk : 0.94356E-05 0.21572E-02 Dimensionless distance yplus : 0.62830E-04 0.14352E-01 Friction thermal sca. tstar : -0.13958E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.44128E-04 0.10080E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.40119E-08 3 0.71547E-07 0.12131E-12 0.67583E+00 c Velocity[X] 0.25757E-32 c Velocity[Y] 0.60645E-13 c Velocity[Z] 0.60661E-13 c Pressure 0.54800E-14 16 0.42492E-07 0.42492E-07 0.76519E+00 c k 0.24519E-06 2 0.24038E-07 0.60010E-09 0.10977E+01 c omega 0.13153E+02 1 0.61723E-09 0.75295E-01 0.14285E-02 c TempK 0.94835E+02 1 0.59293E-07 0.13119E-01 0.12657E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.2438e-14 6.9307e-14 -8.6467e-18 -2.2729e-18 v Velocity[Y] -0.00011818 0.00011126 -3.0527e-11 -2.8303e-12 v Velocity[Z] -0.00011114 0.00011819 -2.5458e-10 -1.2322e-12 v ǁVelocityǁ 6.6126e-10 0.00012662 1.1947e-05 9.2198e-06 v Pressure -0.0017168 0.025642 0.0014936 1.9611e-20 v k 3.5439e-10 0.00083303 0.00052527 0.00067453 v omega 10.873 1.0313e+05 2663.5 496.17 v TempK 288 342.18 294.57 291.46 v Density 1.205 1.205 1.205 1.205 v TurbVisc 4.1517e-15 9.2332e-05 5.2944e-05 6.9571e-05 v CourantNb 3.3935e-09 0.00018195 1.3918e-05 9.2929e-06 v FourierNb 0.080302 0.6281 0.17933 0.14989 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.964 4.964 0.0005882 -6.1128e-07 v volume_forces[Z] -4.964 4.964 -0.00058813 7.2095e-07 v ǁvolume_forcesǁ 2.3658e-08 4.965 0.5942 0.30971 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.77 291.6 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014352 5.0784e-05 2.8264e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.08031 0.6281 0.17934 0.1499 INSTANT 0.986112000E+00 TIME STEP NUMBER 1024 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.94945E-05 0.21568E-02 Friction velocity uk : 0.94946E-05 0.21568E-02 Dimensionless distance yplus : 0.63223E-04 0.14349E-01 Friction thermal sca. tstar : -0.14063E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.44404E-04 0.10078E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.94945E-05 0.21568E-02 Friction velocity uk : 0.94946E-05 0.21568E-02 Dimensionless distance yplus : 0.63223E-04 0.14349E-01 Friction thermal sca. tstar : -0.14063E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.44404E-04 0.10078E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.40132E-08 3 0.71415E-07 0.12097E-12 0.67481E+00 c Velocity[X] 0.25680E-32 c Velocity[Y] 0.60478E-13 c Velocity[Z] 0.60494E-13 c Pressure 0.54685E-14 16 0.42403E-07 0.42403E-07 0.76440E+00 c k 0.24493E-06 2 0.24006E-07 0.59786E-09 0.10968E+01 c omega 0.13153E+02 1 0.61590E-09 0.75029E-01 0.14260E-02 c TempK 0.94836E+02 1 0.59210E-07 0.13100E-01 0.12648E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.2401e-14 6.9278e-14 -8.6432e-18 -2.2721e-18 v Velocity[Y] -0.00011816 0.00011124 -2.8104e-11 -2.8281e-12 v Velocity[Z] -0.00011112 0.00011817 -2.5692e-10 -1.2316e-12 v ǁVelocityǁ 6.681e-10 0.00012659 1.195e-05 9.2245e-06 v Pressure -0.0017184 0.025654 0.0014944 -3.9025e-20 v k 3.5346e-10 0.00083224 0.00052469 0.00067381 v omega 10.863 1.0313e+05 2663.5 496.17 v TempK 288 342.18 294.57 291.46 v Density 1.205 1.205 1.205 1.205 v TurbVisc 4.1408e-15 9.2323e-05 5.2929e-05 6.9554e-05 v CourantNb 3.3948e-09 0.00018189 1.3919e-05 9.2957e-06 v FourierNb 0.080249 0.6281 0.1793 0.14986 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9641 4.9641 0.00058837 -6.1147e-07 v volume_forces[Z] -4.9641 4.9641 -0.00058829 7.2115e-07 v ǁvolume_forcesǁ 2.3905e-08 4.965 0.59437 0.30985 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.78 291.6 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014349 5.0774e-05 2.8258e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.080257 0.6281 0.17932 0.14987 INSTANT 0.987075000E+00 TIME STEP NUMBER 1025 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.95533E-05 0.21564E-02 Friction velocity uk : 0.95533E-05 0.21564E-02 Dimensionless distance yplus : 0.63615E-04 0.14347E-01 Friction thermal sca. tstar : -0.14171E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.44679E-04 0.10076E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.95533E-05 0.21564E-02 Friction velocity uk : 0.95533E-05 0.21564E-02 Dimensionless distance yplus : 0.63615E-04 0.14347E-01 Friction thermal sca. tstar : -0.14171E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.44679E-04 0.10076E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.40144E-08 3 0.71285E-07 0.12064E-12 0.67379E+00 c Velocity[X] 0.25603E-32 c Velocity[Y] 0.60311E-13 c Velocity[Z] 0.60327E-13 c Pressure 0.54606E-14 16 0.42341E-07 0.42341E-07 0.76362E+00 c k 0.24468E-06 2 0.23973E-07 0.59563E-09 0.10959E+01 c omega 0.13153E+02 1 0.61456E-09 0.74765E-01 0.14235E-02 c TempK 0.94836E+02 1 0.59128E-07 0.13080E-01 0.12638E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.2364e-14 6.9248e-14 -8.6396e-18 -2.2713e-18 v Velocity[Y] -0.00011814 0.00011121 -2.5683e-11 -2.8259e-12 v Velocity[Z] -0.0001111 0.00011814 -2.5926e-10 -1.2309e-12 v ǁVelocityǁ 6.7497e-10 0.00012657 1.1953e-05 9.2291e-06 v Pressure -0.00172 0.025666 0.0014952 1.5777e-19 v k 3.5254e-10 0.00083145 0.0005241 0.00067308 v omega 10.854 1.0313e+05 2663.5 496.16 v TempK 288 342.18 294.57 291.46 v Density 1.205 1.205 1.205 1.205 v TurbVisc 4.13e-15 9.2314e-05 5.2915e-05 6.9536e-05 v CourantNb 3.3962e-09 0.00018184 1.3919e-05 9.2985e-06 v FourierNb 0.080196 0.6281 0.17928 0.14983 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9641 4.9641 0.00058854 -6.1166e-07 v volume_forces[Z] -4.9641 4.9641 -0.00058846 7.2136e-07 v ǁvolume_forcesǁ 2.4152e-08 4.965 0.59453 0.31 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.78 291.6 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014347 5.0764e-05 2.8252e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.080204 0.6281 0.17929 0.14984 INSTANT 0.988038000E+00 TIME STEP NUMBER 1026 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.96118E-05 0.21560E-02 Friction velocity uk : 0.96119E-05 0.21559E-02 Dimensionless distance yplus : 0.64004E-04 0.14344E-01 Friction thermal sca. tstar : -0.14281E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.44953E-04 0.10074E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.96118E-05 0.21560E-02 Friction velocity uk : 0.96119E-05 0.21559E-02 Dimensionless distance yplus : 0.64004E-04 0.14344E-01 Friction thermal sca. tstar : -0.14281E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.44953E-04 0.10074E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.40157E-08 3 0.71157E-07 0.12030E-12 0.67277E+00 c Velocity[X] 0.25526E-32 c Velocity[Y] 0.60145E-13 c Velocity[Z] 0.60160E-13 c Pressure 0.54530E-14 16 0.42282E-07 0.42282E-07 0.76284E+00 c k 0.24442E-06 2 0.23941E-07 0.59341E-09 0.10950E+01 c omega 0.13153E+02 1 0.61324E-09 0.74501E-01 0.14210E-02 c TempK 0.94837E+02 1 0.59046E-07 0.13061E-01 0.12629E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.2327e-14 6.9219e-14 -8.6361e-18 -2.2705e-18 v Velocity[Y] -0.00011811 0.00011119 -2.3263e-11 -2.8237e-12 v Velocity[Z] -0.00011108 0.00011812 -2.616e-10 -1.2303e-12 v ǁVelocityǁ 6.8186e-10 0.00012654 1.1956e-05 9.2337e-06 v Pressure -0.0017217 0.025678 0.0014961 5.9812e-20 v k 3.5161e-10 0.00083067 0.00052352 0.00067235 v omega 10.845 1.0313e+05 2663.5 496.15 v TempK 288 342.18 294.57 291.46 v Density 1.205 1.205 1.205 1.205 v TurbVisc 4.1191e-15 9.2306e-05 5.2901e-05 6.9519e-05 v CourantNb 3.3975e-09 0.00018179 1.392e-05 9.3012e-06 v FourierNb 0.080143 0.6281 0.17925 0.14981 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9641 4.9641 0.00058871 -6.1185e-07 v volume_forces[Z] -4.9641 4.9641 -0.00058863 7.2156e-07 v ǁvolume_forcesǁ 2.44e-08 4.9651 0.5947 0.31015 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.78 291.6 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014344 5.0754e-05 2.8246e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.080152 0.6281 0.17927 0.14981 INSTANT 0.989001000E+00 TIME STEP NUMBER 1027 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.96701E-05 0.21555E-02 Friction velocity uk : 0.96701E-05 0.21555E-02 Dimensionless distance yplus : 0.64392E-04 0.14341E-01 Friction thermal sca. tstar : -0.14393E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.45225E-04 0.10072E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.96701E-05 0.21555E-02 Friction velocity uk : 0.96701E-05 0.21555E-02 Dimensionless distance yplus : 0.64392E-04 0.14341E-01 Friction thermal sca. tstar : -0.14393E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.45225E-04 0.10072E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.40170E-08 3 0.71029E-07 0.11997E-12 0.67175E+00 c Velocity[X] 0.25449E-32 c Velocity[Y] 0.59978E-13 c Velocity[Z] 0.59994E-13 c Pressure 0.54493E-14 16 0.42253E-07 0.42253E-07 0.76206E+00 c k 0.24417E-06 2 0.23908E-07 0.59119E-09 0.10941E+01 c omega 0.13153E+02 1 0.61191E-09 0.74239E-01 0.14185E-02 c TempK 0.94838E+02 1 0.58964E-07 0.13042E-01 0.12620E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.2289e-14 6.9189e-14 -8.6326e-18 -2.2697e-18 v Velocity[Y] -0.00011809 0.00011117 -2.0845e-11 -2.8216e-12 v Velocity[Z] -0.00011106 0.0001181 -2.6393e-10 -1.2296e-12 v ǁVelocityǁ 6.8877e-10 0.00012652 1.1959e-05 9.2384e-06 v Pressure -0.0017233 0.02569 0.0014969 -1.5532e-19 v k 3.5069e-10 0.00082988 0.00052294 0.00067163 v omega 10.836 1.0313e+05 2663.5 496.14 v TempK 288 342.18 294.58 291.47 v Density 1.205 1.205 1.205 1.205 v TurbVisc 4.1083e-15 9.2297e-05 5.2887e-05 6.9502e-05 v CourantNb 3.3988e-09 0.00018174 1.392e-05 9.304e-06 v FourierNb 0.080091 0.6281 0.17922 0.14978 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9642 4.9642 0.00058888 -6.1205e-07 v volume_forces[Z] -4.9642 4.9642 -0.0005888 7.2177e-07 v ǁvolume_forcesǁ 2.4649e-08 4.9651 0.59487 0.3103 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.78 291.61 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014341 5.0744e-05 2.824e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.080099 0.6281 0.17924 0.14979 INSTANT 0.989964000E+00 TIME STEP NUMBER 1028 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.97281E-05 0.21551E-02 Friction velocity uk : 0.97282E-05 0.21551E-02 Dimensionless distance yplus : 0.64779E-04 0.14338E-01 Friction thermal sca. tstar : -0.14509E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.45496E-04 0.10070E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.97281E-05 0.21551E-02 Friction velocity uk : 0.97282E-05 0.21551E-02 Dimensionless distance yplus : 0.64779E-04 0.14338E-01 Friction thermal sca. tstar : -0.14509E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.45496E-04 0.10070E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.40182E-08 3 0.70899E-07 0.11964E-12 0.67073E+00 c Velocity[X] 0.25373E-32 c Velocity[Y] 0.59812E-13 c Velocity[Z] 0.59828E-13 c Pressure 0.54376E-14 16 0.42162E-07 0.42162E-07 0.76128E+00 c k 0.24392E-06 2 0.23876E-07 0.58899E-09 0.10932E+01 c omega 0.13153E+02 1 0.61059E-09 0.73978E-01 0.14160E-02 c TempK 0.94838E+02 1 0.58883E-07 0.13023E-01 0.12610E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.2252e-14 6.916e-14 -8.6291e-18 -2.2689e-18 v Velocity[Y] -0.00011807 0.00011115 -1.8429e-11 -2.8194e-12 v Velocity[Z] -0.00011104 0.00011807 -2.6626e-10 -1.229e-12 v ǁVelocityǁ 6.9571e-10 0.00012649 1.1961e-05 9.243e-06 v Pressure -0.001725 0.025702 0.0014977 1.5865e-19 v k 3.4977e-10 0.0008291 0.00052237 0.00067091 v omega 10.827 1.0313e+05 2663.5 496.13 v TempK 288 342.18 294.58 291.47 v Density 1.205 1.205 1.205 1.205 v TurbVisc 4.0976e-15 9.2288e-05 5.2873e-05 6.9485e-05 v CourantNb 3.4001e-09 0.00018169 1.392e-05 9.3067e-06 v FourierNb 0.080038 0.6281 0.1792 0.14975 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9642 4.9642 0.00058904 -6.1224e-07 v volume_forces[Z] -4.9642 4.9642 -0.00058897 7.2197e-07 v ǁvolume_forcesǁ 2.4899e-08 4.9651 0.59503 0.31045 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.78 291.61 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014338 5.0734e-05 2.8234e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.080046 0.6281 0.17921 0.14976 INSTANT 0.990927000E+00 TIME STEP NUMBER 1029 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.97859E-05 0.21547E-02 Friction velocity uk : 0.97860E-05 0.21547E-02 Dimensionless distance yplus : 0.65164E-04 0.14335E-01 Friction thermal sca. tstar : -0.14627E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.45767E-04 0.10068E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.97859E-05 0.21547E-02 Friction velocity uk : 0.97860E-05 0.21547E-02 Dimensionless distance yplus : 0.65164E-04 0.14335E-01 Friction thermal sca. tstar : -0.14627E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.45767E-04 0.10068E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.40195E-08 3 0.70772E-07 0.11931E-12 0.66971E+00 c Velocity[X] 0.25297E-32 c Velocity[Y] 0.59646E-13 c Velocity[Z] 0.59662E-13 c Pressure 0.54296E-14 16 0.42099E-07 0.42099E-07 0.76051E+00 c k 0.24366E-06 2 0.23844E-07 0.58680E-09 0.10923E+01 c omega 0.13153E+02 1 0.60927E-09 0.73718E-01 0.14135E-02 c TempK 0.94839E+02 1 0.58801E-07 0.13004E-01 0.12601E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.2215e-14 6.9131e-14 -8.6256e-18 -2.2681e-18 v Velocity[Y] -0.00011804 0.00011113 -1.6015e-11 -2.8172e-12 v Velocity[Z] -0.00011101 0.00011805 -2.6859e-10 -1.2284e-12 v ǁVelocityǁ 7.0268e-10 0.00012646 1.1964e-05 9.2476e-06 v Pressure -0.0017266 0.025714 0.0014985 1.6865e-20 v k 3.4886e-10 0.00082832 0.00052179 0.00067019 v omega 10.817 1.0313e+05 2663.5 496.13 v TempK 288 342.18 294.58 291.47 v Density 1.205 1.205 1.205 1.205 v TurbVisc 4.0869e-15 9.228e-05 5.2859e-05 6.9468e-05 v CourantNb 3.4015e-09 0.00018164 1.3921e-05 9.3095e-06 v FourierNb 0.079986 0.6281 0.17917 0.14972 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9642 4.9642 0.00058921 -6.1243e-07 v volume_forces[Z] -4.9642 4.9642 -0.00058914 7.2218e-07 v ǁvolume_forcesǁ 2.515e-08 4.9652 0.5952 0.3106 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.79 291.61 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014335 5.0723e-05 2.8229e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.079994 0.6281 0.17919 0.14973 INSTANT 0.991890000E+00 TIME STEP NUMBER 1030 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.98435E-05 0.21543E-02 Friction velocity uk : 0.98435E-05 0.21543E-02 Dimensionless distance yplus : 0.65547E-04 0.14333E-01 Friction thermal sca. tstar : -0.14748E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.46036E-04 0.10066E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.98435E-05 0.21543E-02 Friction velocity uk : 0.98435E-05 0.21543E-02 Dimensionless distance yplus : 0.65547E-04 0.14333E-01 Friction thermal sca. tstar : -0.14748E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.46036E-04 0.10066E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.40208E-08 3 0.70642E-07 0.11898E-12 0.66869E+00 c Velocity[X] 0.25221E-32 c Velocity[Y] 0.59480E-13 c Velocity[Z] 0.59496E-13 c Pressure 0.54218E-14 16 0.42038E-07 0.42038E-07 0.75973E+00 c k 0.24341E-06 2 0.23812E-07 0.58462E-09 0.10914E+01 c omega 0.13153E+02 1 0.60796E-09 0.73459E-01 0.14110E-02 c TempK 0.94839E+02 1 0.58720E-07 0.12985E-01 0.12592E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.2178e-14 6.9102e-14 -8.6221e-18 -2.2673e-18 v Velocity[Y] -0.00011802 0.00011111 -1.3602e-11 -2.8151e-12 v Velocity[Z] -0.00011099 0.00011802 -2.7092e-10 -1.2277e-12 v ǁVelocityǁ 7.0967e-10 0.00012644 1.1967e-05 9.2522e-06 v Pressure -0.0017282 0.025726 0.0014993 -1.2472e-19 v k 3.4795e-10 0.00082754 0.00052121 0.00066947 v omega 10.808 1.0313e+05 2663.5 496.12 v TempK 288 342.18 294.58 291.47 v Density 1.205 1.205 1.205 1.205 v TurbVisc 4.0762e-15 9.2271e-05 5.2845e-05 6.9451e-05 v CourantNb 3.4028e-09 0.00018159 1.3921e-05 9.3122e-06 v FourierNb 0.079934 0.6281 0.17915 0.14969 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9643 4.9643 0.00058938 -6.1262e-07 v volume_forces[Z] -4.9643 4.9643 -0.00058931 7.2238e-07 v ǁvolume_forcesǁ 2.5402e-08 4.9652 0.59537 0.31075 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.79 291.61 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014333 5.0713e-05 2.8223e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.079942 0.6281 0.17916 0.1497 INSTANT 0.992853000E+00 TIME STEP NUMBER 1031 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.99008E-05 0.21539E-02 Friction velocity uk : 0.99008E-05 0.21538E-02 Dimensionless distance yplus : 0.65929E-04 0.14330E-01 Friction thermal sca. tstar : -0.14872E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.46304E-04 0.10064E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.99008E-05 0.21539E-02 Friction velocity uk : 0.99008E-05 0.21538E-02 Dimensionless distance yplus : 0.65929E-04 0.14330E-01 Friction thermal sca. tstar : -0.14872E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.46304E-04 0.10064E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.40220E-08 3 0.70515E-07 0.11865E-12 0.66768E+00 c Velocity[X] 0.25146E-32 c Velocity[Y] 0.59315E-13 c Velocity[Z] 0.59331E-13 c Pressure 0.54142E-14 16 0.41979E-07 0.41979E-07 0.75896E+00 c k 0.24316E-06 2 0.23780E-07 0.58244E-09 0.10905E+01 c omega 0.13153E+02 1 0.60665E-09 0.73201E-01 0.14085E-02 c TempK 0.94840E+02 1 0.58639E-07 0.12966E-01 0.12583E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.2142e-14 6.9072e-14 -8.6186e-18 -2.2665e-18 v Velocity[Y] -0.00011799 0.00011109 -1.1191e-11 -2.813e-12 v Velocity[Z] -0.00011097 0.000118 -2.7324e-10 -1.227e-12 v ǁVelocityǁ 7.1668e-10 0.00012641 1.197e-05 9.2568e-06 v Pressure -0.0017299 0.025738 0.0015001 8.158e-20 v k 3.4704e-10 0.00082676 0.00052064 0.00066875 v omega 10.799 1.0313e+05 2663.5 496.11 v TempK 288 342.18 294.58 291.47 v Density 1.205 1.205 1.205 1.205 v TurbVisc 4.0655e-15 9.2262e-05 5.283e-05 6.9434e-05 v CourantNb 3.4041e-09 0.00018154 1.3922e-05 9.3149e-06 v FourierNb 0.079881 0.6281 0.17912 0.14966 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9643 4.9643 0.00058955 -6.1281e-07 v volume_forces[Z] -4.9643 4.9643 -0.00058948 7.2258e-07 v ǁvolume_forcesǁ 2.5654e-08 4.9652 0.59553 0.3109 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.79 291.61 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.01433 5.0703e-05 2.8217e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.07989 0.6281 0.17913 0.14967 INSTANT 0.993816000E+00 TIME STEP NUMBER 1032 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.99579E-05 0.21534E-02 Friction velocity uk : 0.99580E-05 0.21534E-02 Dimensionless distance yplus : 0.66309E-04 0.14327E-01 Friction thermal sca. tstar : -0.14999E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.46571E-04 0.10062E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.99579E-05 0.21534E-02 Friction velocity uk : 0.99580E-05 0.21534E-02 Dimensionless distance yplus : 0.66309E-04 0.14327E-01 Friction thermal sca. tstar : -0.14999E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.46571E-04 0.10062E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.40233E-08 3 0.70389E-07 0.11832E-12 0.66666E+00 c Velocity[X] 0.25071E-32 c Velocity[Y] 0.59150E-13 c Velocity[Z] 0.59166E-13 c Pressure 0.54066E-14 16 0.41920E-07 0.41920E-07 0.75819E+00 c k 0.24291E-06 2 0.23748E-07 0.58028E-09 0.10896E+01 c omega 0.13153E+02 1 0.60535E-09 0.72945E-01 0.14061E-02 c TempK 0.94840E+02 1 0.58558E-07 0.12947E-01 0.12573E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.2105e-14 6.9043e-14 -8.6151e-18 -2.2657e-18 v Velocity[Y] -0.00011797 0.00011107 -8.782e-12 -2.8108e-12 v Velocity[Z] -0.00011095 0.00011798 -2.7556e-10 -1.2263e-12 v ǁVelocityǁ 7.2372e-10 0.00012639 1.1973e-05 9.2614e-06 v Pressure -0.0017315 0.02575 0.0015009 1.5492e-20 v k 3.4614e-10 0.00082598 0.00052006 0.00066804 v omega 10.79 1.0313e+05 2663.5 496.1 v TempK 288 342.18 294.59 291.47 v Density 1.205 1.205 1.205 1.205 v TurbVisc 4.0549e-15 9.2254e-05 5.2816e-05 6.9417e-05 v CourantNb 3.4053e-09 0.00018149 1.3922e-05 9.3176e-06 v FourierNb 0.079829 0.6281 0.17909 0.14963 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9643 4.9643 0.00058972 -6.13e-07 v volume_forces[Z] -4.9643 4.9643 -0.00058964 7.2278e-07 v ǁvolume_forcesǁ 2.5908e-08 4.9653 0.5957 0.31105 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.79 291.61 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014327 5.0693e-05 2.8211e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.079838 0.6281 0.17911 0.14964 INSTANT 0.994779000E+00 TIME STEP NUMBER 1033 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10015E-04 0.21530E-02 Friction velocity uk : 0.10015E-04 0.21530E-02 Dimensionless distance yplus : 0.66688E-04 0.14324E-01 Friction thermal sca. tstar : -0.15129E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.46837E-04 0.10060E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10015E-04 0.21530E-02 Friction velocity uk : 0.10015E-04 0.21530E-02 Dimensionless distance yplus : 0.66688E-04 0.14324E-01 Friction thermal sca. tstar : -0.15129E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.46837E-04 0.10060E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.40245E-08 3 0.70265E-07 0.11799E-12 0.66564E+00 c Velocity[X] 0.24996E-32 c Velocity[Y] 0.58985E-13 c Velocity[Z] 0.59001E-13 c Pressure 0.53995E-14 16 0.41864E-07 0.41864E-07 0.75742E+00 c k 0.24266E-06 2 0.23716E-07 0.57813E-09 0.10887E+01 c omega 0.13153E+02 1 0.60404E-09 0.72689E-01 0.14036E-02 c TempK 0.94841E+02 1 0.58478E-07 0.12928E-01 0.12564E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.2068e-14 6.9014e-14 -8.6117e-18 -2.2649e-18 v Velocity[Y] -0.00011795 0.00011105 -6.3748e-12 -2.8087e-12 v Velocity[Z] -0.00011093 0.00011795 -2.7788e-10 -1.2257e-12 v ǁVelocityǁ 7.3078e-10 0.00012636 1.1975e-05 9.266e-06 v Pressure -0.0017331 0.025762 0.0015018 4.2163e-20 v k 3.4524e-10 0.00082521 0.00051949 0.00066732 v omega 10.781 1.0313e+05 2663.5 496.09 v TempK 288 342.18 294.59 291.48 v Density 1.205 1.205 1.205 1.205 v TurbVisc 4.0444e-15 9.2245e-05 5.2802e-05 6.9399e-05 v CourantNb 3.4066e-09 0.00018144 1.3922e-05 9.3204e-06 v FourierNb 0.079777 0.6281 0.17907 0.14961 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9644 4.9644 0.00058989 -6.1319e-07 v volume_forces[Z] -4.9644 4.9644 -0.00058981 7.2299e-07 v ǁvolume_forcesǁ 2.6162e-08 4.9653 0.59586 0.31119 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.79 291.62 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014324 5.0683e-05 2.8205e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.079786 0.6281 0.17908 0.14962 INSTANT 0.995742000E+00 TIME STEP NUMBER 1034 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10071E-04 0.21526E-02 Friction velocity uk : 0.10072E-04 0.21526E-02 Dimensionless distance yplus : 0.67065E-04 0.14321E-01 Friction thermal sca. tstar : -0.15263E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.47102E-04 0.10058E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10071E-04 0.21526E-02 Friction velocity uk : 0.10072E-04 0.21526E-02 Dimensionless distance yplus : 0.67065E-04 0.14321E-01 Friction thermal sca. tstar : -0.15263E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.47102E-04 0.10058E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.40258E-08 3 0.70136E-07 0.11766E-12 0.66463E+00 c Velocity[X] 0.24922E-32 c Velocity[Y] 0.58820E-13 c Velocity[Z] 0.58836E-13 c Pressure 0.53918E-14 16 0.41804E-07 0.41804E-07 0.75665E+00 c k 0.24241E-06 2 0.23684E-07 0.57599E-09 0.10878E+01 c omega 0.13153E+02 1 0.60275E-09 0.72435E-01 0.14011E-02 c TempK 0.94841E+02 1 0.58397E-07 0.12910E-01 0.12555E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.2031e-14 6.8985e-14 -8.6082e-18 -2.2641e-18 v Velocity[Y] -0.00011792 0.00011103 -3.9696e-12 -2.8066e-12 v Velocity[Z] -0.00011091 0.00011793 -2.802e-10 -1.2249e-12 v ǁVelocityǁ 7.3786e-10 0.00012634 1.1978e-05 9.2705e-06 v Pressure -0.0017348 0.025774 0.0015026 -1.1433e-19 v k 3.4434e-10 0.00082443 0.00051892 0.00066661 v omega 10.772 1.0313e+05 2663.5 496.09 v TempK 288 342.18 294.59 291.48 v Density 1.205 1.205 1.205 1.205 v TurbVisc 4.0338e-15 9.2236e-05 5.2788e-05 6.9382e-05 v CourantNb 3.4079e-09 0.00018139 1.3923e-05 9.3231e-06 v FourierNb 0.079726 0.6281 0.17904 0.14958 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9644 4.9644 0.00059005 -6.1338e-07 v volume_forces[Z] -4.9644 4.9644 -0.00058998 7.2319e-07 v ǁvolume_forcesǁ 2.6418e-08 4.9653 0.59603 0.31134 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.79 291.62 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014321 5.0673e-05 2.8199e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.079734 0.6281 0.17905 0.14959 INSTANT 0.996705000E+00 TIME STEP NUMBER 1035 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10128E-04 0.21522E-02 Friction velocity uk : 0.10128E-04 0.21522E-02 Dimensionless distance yplus : 0.67441E-04 0.14319E-01 Friction thermal sca. tstar : -0.15400E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.47366E-04 0.10057E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10128E-04 0.21522E-02 Friction velocity uk : 0.10128E-04 0.21522E-02 Dimensionless distance yplus : 0.67441E-04 0.14319E-01 Friction thermal sca. tstar : -0.15400E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.47366E-04 0.10057E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.40270E-08 3 0.70013E-07 0.11733E-12 0.66361E+00 c Velocity[X] 0.24847E-32 c Velocity[Y] 0.58655E-13 c Velocity[Z] 0.58672E-13 c Pressure 0.53968E-14 16 0.41843E-07 0.41843E-07 0.75588E+00 c k 0.24216E-06 2 0.23652E-07 0.57385E-09 0.10869E+01 c omega 0.13153E+02 1 0.60145E-09 0.72181E-01 0.13987E-02 c TempK 0.94842E+02 1 0.58317E-07 0.12891E-01 0.12546E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.1995e-14 6.8956e-14 -8.6047e-18 -2.2633e-18 v Velocity[Y] -0.0001179 0.00011101 -1.566e-12 -2.8045e-12 v Velocity[Z] -0.00011089 0.00011791 -2.8251e-10 -1.2243e-12 v ǁVelocityǁ 7.4497e-10 0.00012631 1.1981e-05 9.2751e-06 v Pressure -0.0017364 0.025786 0.0015034 -1.863e-20 v k 3.4344e-10 0.00082366 0.00051835 0.0006659 v omega 10.763 1.0313e+05 2663.5 496.08 v TempK 288 342.18 294.59 291.48 v Density 1.205 1.205 1.205 1.205 v TurbVisc 4.0233e-15 9.2228e-05 5.2774e-05 6.9365e-05 v CourantNb 3.4092e-09 0.00018134 1.3923e-05 9.3258e-06 v FourierNb 0.079674 0.6281 0.17901 0.14955 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9644 4.9644 0.00059022 -6.1357e-07 v volume_forces[Z] -4.9644 4.9644 -0.00059015 7.2339e-07 v ǁvolume_forcesǁ 2.6674e-08 4.9654 0.59619 0.31149 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.8 291.62 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014319 5.0663e-05 2.8193e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.079682 0.6281 0.17903 0.14956 INSTANT 0.997668000E+00 TIME STEP NUMBER 1036 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10184E-04 0.21518E-02 Friction velocity uk : 0.10184E-04 0.21517E-02 Dimensionless distance yplus : 0.67816E-04 0.14316E-01 Friction thermal sca. tstar : -0.15541E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.47629E-04 0.10055E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10184E-04 0.21518E-02 Friction velocity uk : 0.10184E-04 0.21517E-02 Dimensionless distance yplus : 0.67816E-04 0.14316E-01 Friction thermal sca. tstar : -0.15541E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.47629E-04 0.10055E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.40283E-08 3 0.69885E-07 0.11700E-12 0.66260E+00 c Velocity[X] 0.24773E-32 c Velocity[Y] 0.58491E-13 c Velocity[Z] 0.58507E-13 c Pressure 0.53771E-14 16 0.41689E-07 0.41689E-07 0.75511E+00 c k 0.24191E-06 2 0.23621E-07 0.57173E-09 0.10860E+01 c omega 0.13153E+02 1 0.60016E-09 0.71929E-01 0.13962E-02 c TempK 0.94842E+02 1 0.58237E-07 0.12872E-01 0.12536E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.1958e-14 6.8927e-14 -8.6012e-18 -2.2625e-18 v Velocity[Y] -0.00011788 0.00011099 8.3567e-13 -2.8025e-12 v Velocity[Z] -0.00011087 0.00011788 -2.8482e-10 -1.2236e-12 v ǁVelocityǁ 7.5209e-10 0.00012628 1.1984e-05 9.2796e-06 v Pressure -0.0017381 0.025798 0.0015042 -7.8442e-21 v k 3.4255e-10 0.00082289 0.00051778 0.00066519 v omega 10.753 1.0313e+05 2663.5 496.07 v TempK 288 342.18 294.59 291.48 v Density 1.205 1.205 1.205 1.205 v TurbVisc 4.0129e-15 9.2219e-05 5.276e-05 6.9348e-05 v CourantNb 3.4104e-09 0.00018129 1.3923e-05 9.3285e-06 v FourierNb 0.079622 0.6281 0.17899 0.14952 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9645 4.9645 0.00059039 -6.1376e-07 v volume_forces[Z] -4.9645 4.9645 -0.00059032 7.2359e-07 v ǁvolume_forcesǁ 2.693e-08 4.9654 0.59636 0.31164 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.8 291.62 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014316 5.0653e-05 2.8187e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.079631 0.6281 0.179 0.14953 INSTANT 0.998631000E+00 TIME STEP NUMBER 1037 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10240E-04 0.21514E-02 Friction velocity uk : 0.10240E-04 0.21513E-02 Dimensionless distance yplus : 0.68189E-04 0.14313E-01 Friction thermal sca. tstar : -0.15686E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.47891E-04 0.10053E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10240E-04 0.21514E-02 Friction velocity uk : 0.10240E-04 0.21513E-02 Dimensionless distance yplus : 0.68189E-04 0.14313E-01 Friction thermal sca. tstar : -0.15686E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.47891E-04 0.10053E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.40295E-08 3 0.69762E-07 0.11667E-12 0.66158E+00 c Velocity[X] 0.24700E-32 c Velocity[Y] 0.58327E-13 c Velocity[Z] 0.58343E-13 c Pressure 0.53696E-14 16 0.41631E-07 0.41631E-07 0.75435E+00 c k 0.24166E-06 2 0.23589E-07 0.56962E-09 0.10851E+01 c omega 0.13153E+02 1 0.59888E-09 0.71678E-01 0.13938E-02 c TempK 0.94843E+02 1 0.58157E-07 0.12853E-01 0.12527E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.1922e-14 6.8898e-14 -8.5978e-18 -2.2617e-18 v Velocity[Y] -0.00011785 0.00011096 3.2355e-12 -2.8004e-12 v Velocity[Z] -0.00011084 0.00011786 -2.8713e-10 -1.2229e-12 v ǁVelocityǁ 7.5924e-10 0.00012626 1.1987e-05 9.2842e-06 v Pressure -0.0017397 0.02581 0.001505 -1.559e-20 v k 3.4166e-10 0.00082212 0.00051721 0.00066448 v omega 10.744 1.0313e+05 2663.5 496.06 v TempK 288 342.18 294.6 291.48 v Density 1.205 1.205 1.205 1.205 v TurbVisc 4.0025e-15 9.2211e-05 5.2746e-05 6.9331e-05 v CourantNb 3.4117e-09 0.00018124 1.3924e-05 9.3312e-06 v FourierNb 0.079571 0.6281 0.17896 0.14949 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9645 4.9645 0.00059056 -6.1394e-07 v volume_forces[Z] -4.9645 4.9645 -0.00059048 7.2379e-07 v ǁvolume_forcesǁ 2.7188e-08 4.9654 0.59653 0.31179 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.8 291.62 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014313 5.0643e-05 2.8181e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.079579 0.6281 0.17898 0.1495 INSTANT 0.999594000E+00 TIME STEP NUMBER 1038 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10296E-04 0.21509E-02 Friction velocity uk : 0.10296E-04 0.21509E-02 Dimensionless distance yplus : 0.68561E-04 0.14310E-01 Friction thermal sca. tstar : -0.15835E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.48153E-04 0.10051E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10296E-04 0.21509E-02 Friction velocity uk : 0.10296E-04 0.21509E-02 Dimensionless distance yplus : 0.68561E-04 0.14310E-01 Friction thermal sca. tstar : -0.15835E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.48153E-04 0.10051E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.40307E-08 3 0.69637E-07 0.11634E-12 0.66057E+00 c Velocity[X] 0.24626E-32 c Velocity[Y] 0.58163E-13 c Velocity[Z] 0.58180E-13 c Pressure 0.53611E-14 16 0.41565E-07 0.41565E-07 0.75359E+00 c k 0.24141E-06 2 0.23558E-07 0.56751E-09 0.10842E+01 c omega 0.13153E+02 1 0.59759E-09 0.71428E-01 0.13914E-02 c TempK 0.94843E+02 1 0.58077E-07 0.12835E-01 0.12518E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.1885e-14 6.8869e-14 -8.5943e-18 -2.2609e-18 v Velocity[Y] -0.00011783 0.00011094 5.6332e-12 -2.7984e-12 v Velocity[Z] -0.00011082 0.00011783 -2.8943e-10 -1.2222e-12 v ǁVelocityǁ 7.6642e-10 0.00012623 1.1989e-05 9.2887e-06 v Pressure -0.0017413 0.025822 0.0015058 8.7561e-20 v k 3.4078e-10 0.00082135 0.00051664 0.00066377 v omega 10.735 1.0313e+05 2663.5 496.05 v TempK 288 342.18 294.6 291.48 v Density 1.205 1.205 1.205 1.205 v TurbVisc 3.9921e-15 9.2202e-05 5.2732e-05 6.9314e-05 v CourantNb 3.4129e-09 0.00018119 1.3924e-05 9.3339e-06 v FourierNb 0.07952 0.6281 0.17894 0.14947 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9645 4.9645 0.00059072 -6.1413e-07 v volume_forces[Z] -4.9645 4.9645 -0.00059065 7.2399e-07 v ǁvolume_forcesǁ 2.7447e-08 4.9655 0.59669 0.31194 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.8 291.62 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.01431 5.0633e-05 2.8176e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.079528 0.6281 0.17895 0.14947 INSTANT 0.100055700E+01 TIME STEP NUMBER 1039 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10352E-04 0.21505E-02 Friction velocity uk : 0.10352E-04 0.21505E-02 Dimensionless distance yplus : 0.68931E-04 0.14308E-01 Friction thermal sca. tstar : -0.15988E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.48413E-04 0.10049E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10352E-04 0.21505E-02 Friction velocity uk : 0.10352E-04 0.21505E-02 Dimensionless distance yplus : 0.68931E-04 0.14308E-01 Friction thermal sca. tstar : -0.15988E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.48413E-04 0.10049E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.40320E-08 3 0.69513E-07 0.11602E-12 0.65956E+00 c Velocity[X] 0.24553E-32 c Velocity[Y] 0.58000E-13 c Velocity[Z] 0.58016E-13 c Pressure 0.53536E-14 16 0.41506E-07 0.41506E-07 0.75283E+00 c k 0.24116E-06 2 0.23526E-07 0.56542E-09 0.10833E+01 c omega 0.13153E+02 1 0.59632E-09 0.71179E-01 0.13889E-02 c TempK 0.94844E+02 1 0.57998E-07 0.12816E-01 0.12509E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.1849e-14 6.8841e-14 -8.5909e-18 -2.2601e-18 v Velocity[Y] -0.0001178 0.00011092 8.0292e-12 -2.7963e-12 v Velocity[Z] -0.0001108 0.00011781 -2.9173e-10 -1.2215e-12 v ǁVelocityǁ 7.7361e-10 0.00012621 1.1992e-05 9.2932e-06 v Pressure -0.001743 0.025834 0.0015066 -8.7071e-20 v k 3.3989e-10 0.00082058 0.00051608 0.00066306 v omega 10.726 1.0313e+05 2663.5 496.05 v TempK 288 342.18 294.6 291.49 v Density 1.205 1.205 1.205 1.205 v TurbVisc 3.9817e-15 9.2193e-05 5.2718e-05 6.9297e-05 v CourantNb 3.4141e-09 0.00018114 1.3925e-05 9.3365e-06 v FourierNb 0.079468 0.6281 0.17891 0.14944 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9646 4.9646 0.00059089 -6.1432e-07 v volume_forces[Z] -4.9646 4.9646 -0.00059082 7.2419e-07 v ǁvolume_forcesǁ 2.7706e-08 4.9655 0.59686 0.31208 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.8 291.63 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014308 5.0623e-05 2.817e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.079477 0.6281 0.17892 0.14945 INSTANT 0.100152000E+01 TIME STEP NUMBER 1040 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10407E-04 0.21501E-02 Friction velocity uk : 0.10407E-04 0.21501E-02 Dimensionless distance yplus : 0.69300E-04 0.14305E-01 Friction thermal sca. tstar : -0.16146E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.48672E-04 0.10047E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10407E-04 0.21501E-02 Friction velocity uk : 0.10407E-04 0.21501E-02 Dimensionless distance yplus : 0.69300E-04 0.14305E-01 Friction thermal sca. tstar : -0.16146E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.48672E-04 0.10047E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.40332E-08 3 0.69389E-07 0.11569E-12 0.65855E+00 c Velocity[X] 0.24481E-32 c Velocity[Y] 0.57837E-13 c Velocity[Z] 0.57853E-13 c Pressure 0.53467E-14 16 0.41452E-07 0.41452E-07 0.75207E+00 c k 0.24091E-06 2 0.23495E-07 0.56333E-09 0.10825E+01 c omega 0.13153E+02 1 0.59504E-09 0.70931E-01 0.13865E-02 c TempK 0.94844E+02 1 0.57918E-07 0.12798E-01 0.12500E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.1812e-14 6.8812e-14 -8.5874e-18 -2.2593e-18 v Velocity[Y] -0.00011778 0.0001109 1.0423e-11 -2.7943e-12 v Velocity[Z] -0.00011078 0.00011779 -2.9403e-10 -1.2207e-12 v ǁVelocityǁ 7.8083e-10 0.00012618 1.1995e-05 9.2977e-06 v Pressure -0.0017446 0.025846 0.0015074 -1.9022e-20 v k 3.3901e-10 0.00081982 0.00051551 0.00066236 v omega 10.717 1.0313e+05 2663.4 496.04 v TempK 288 342.18 294.6 291.49 v Density 1.205 1.205 1.205 1.205 v TurbVisc 3.9714e-15 9.2185e-05 5.2704e-05 6.928e-05 v CourantNb 3.4154e-09 0.00018109 1.3925e-05 9.3392e-06 v FourierNb 0.079417 0.6281 0.17888 0.14941 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9646 4.9646 0.00059106 -6.1451e-07 v volume_forces[Z] -4.9646 4.9646 -0.00059099 7.2439e-07 v ǁvolume_forcesǁ 2.7966e-08 4.9655 0.59702 0.31223 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.81 291.63 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014305 5.0613e-05 2.8164e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.079425 0.6281 0.1789 0.14942 INSTANT 0.100248300E+01 TIME STEP NUMBER 1041 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10462E-04 0.21497E-02 Friction velocity uk : 0.10462E-04 0.21497E-02 Dimensionless distance yplus : 0.69668E-04 0.14302E-01 Friction thermal sca. tstar : -0.16308E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.48930E-04 0.10045E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10462E-04 0.21497E-02 Friction velocity uk : 0.10462E-04 0.21497E-02 Dimensionless distance yplus : 0.69668E-04 0.14302E-01 Friction thermal sca. tstar : -0.16308E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.48930E-04 0.10045E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.40345E-08 3 0.69265E-07 0.11536E-12 0.65754E+00 c Velocity[X] 0.24408E-32 c Velocity[Y] 0.57674E-13 c Velocity[Z] 0.57690E-13 c Pressure 0.53386E-14 16 0.41389E-07 0.41389E-07 0.75131E+00 c k 0.24067E-06 2 0.23463E-07 0.56126E-09 0.10816E+01 c omega 0.13153E+02 1 0.59377E-09 0.70684E-01 0.13841E-02 c TempK 0.94845E+02 1 0.57839E-07 0.12779E-01 0.12491E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.1776e-14 6.8783e-14 -8.584e-18 -2.2585e-18 v Velocity[Y] -0.00011776 0.00011088 1.2815e-11 -2.7923e-12 v Velocity[Z] -0.00011076 0.00011776 -2.9633e-10 -1.22e-12 v ǁVelocityǁ 7.8807e-10 0.00012615 1.1998e-05 9.3022e-06 v Pressure -0.0017462 0.025858 0.0015082 -4.2163e-20 v k 3.3814e-10 0.00081905 0.00051495 0.00066165 v omega 10.708 1.0313e+05 2663.4 496.03 v TempK 288 342.18 294.6 291.49 v Density 1.205 1.205 1.205 1.205 v TurbVisc 3.9611e-15 9.2176e-05 5.269e-05 6.9264e-05 v CourantNb 3.4166e-09 0.00018104 1.3925e-05 9.3419e-06 v FourierNb 0.079366 0.6281 0.17886 0.14938 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9646 4.9646 0.00059123 -6.1469e-07 v volume_forces[Z] -4.9646 4.9646 -0.00059115 7.2459e-07 v ǁvolume_forcesǁ 2.8227e-08 4.9656 0.59719 0.31238 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.81 291.63 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014302 5.0603e-05 2.8158e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.079374 0.6281 0.17887 0.14939 INSTANT 0.100344600E+01 TIME STEP NUMBER 1042 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10517E-04 0.21493E-02 Friction velocity uk : 0.10517E-04 0.21493E-02 Dimensionless distance yplus : 0.70035E-04 0.14299E-01 Friction thermal sca. tstar : -0.16475E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.49188E-04 0.10043E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10517E-04 0.21493E-02 Friction velocity uk : 0.10517E-04 0.21493E-02 Dimensionless distance yplus : 0.70035E-04 0.14299E-01 Friction thermal sca. tstar : -0.16475E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.49188E-04 0.10043E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.40357E-08 3 0.69146E-07 0.11504E-12 0.65652E+00 c Velocity[X] 0.24336E-32 c Velocity[Y] 0.57511E-13 c Velocity[Z] 0.57528E-13 c Pressure 0.53454E-14 16 0.41441E-07 0.41441E-07 0.75055E+00 c k 0.24042E-06 2 0.23432E-07 0.55919E-09 0.10807E+01 c omega 0.13153E+02 1 0.59250E-09 0.70439E-01 0.13817E-02 c TempK 0.94845E+02 1 0.57760E-07 0.12761E-01 0.12482E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.174e-14 6.8754e-14 -8.5806e-18 -2.2577e-18 v Velocity[Y] -0.00011773 0.00011086 1.5205e-11 -2.7903e-12 v Velocity[Z] -0.00011074 0.00011774 -2.9862e-10 -1.2193e-12 v ǁVelocityǁ 7.9533e-10 0.00012613 1.2e-05 9.3067e-06 v Pressure -0.0017479 0.02587 0.001509 -3.3142e-20 v k 3.3727e-10 0.00081829 0.00051438 0.00066095 v omega 10.699 1.0313e+05 2663.4 496.02 v TempK 288 342.18 294.6 291.49 v Density 1.205 1.205 1.205 1.205 v TurbVisc 3.9509e-15 9.2168e-05 5.2676e-05 6.9247e-05 v CourantNb 3.4178e-09 0.00018099 1.3926e-05 9.3445e-06 v FourierNb 0.079315 0.6281 0.17883 0.14935 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9647 4.9647 0.00059139 -6.1488e-07 v volume_forces[Z] -4.9647 4.9647 -0.00059132 7.2479e-07 v ǁvolume_forcesǁ 2.8489e-08 4.9656 0.59735 0.31253 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.81 291.63 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014299 5.0592e-05 2.8152e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.079323 0.6281 0.17885 0.14936 INSTANT 0.100440900E+01 TIME STEP NUMBER 1043 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10572E-04 0.21489E-02 Friction velocity uk : 0.10572E-04 0.21488E-02 Dimensionless distance yplus : 0.70400E-04 0.14297E-01 Friction thermal sca. tstar : -0.16648E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.49445E-04 0.10041E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10572E-04 0.21489E-02 Friction velocity uk : 0.10572E-04 0.21488E-02 Dimensionless distance yplus : 0.70400E-04 0.14297E-01 Friction thermal sca. tstar : -0.16648E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.49445E-04 0.10041E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.40369E-08 3 0.69020E-07 0.11471E-12 0.65552E+00 c Velocity[X] 0.24264E-32 c Velocity[Y] 0.57349E-13 c Velocity[Z] 0.57365E-13 c Pressure 0.53279E-14 16 0.41305E-07 0.41305E-07 0.74980E+00 c k 0.24017E-06 2 0.23401E-07 0.55714E-09 0.10798E+01 c omega 0.13153E+02 1 0.59124E-09 0.70194E-01 0.13793E-02 c TempK 0.94846E+02 1 0.57682E-07 0.12742E-01 0.12473E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.1703e-14 6.8726e-14 -8.5771e-18 -2.2569e-18 v Velocity[Y] -0.00011771 0.00011084 1.7593e-11 -2.7883e-12 v Velocity[Z] -0.00011072 0.00011771 -3.0091e-10 -1.2186e-12 v ǁVelocityǁ 8.0261e-10 0.0001261 1.2003e-05 9.3112e-06 v Pressure -0.0017495 0.025881 0.0015099 9.364e-20 v k 3.364e-10 0.00081752 0.00051382 0.00066025 v omega 10.69 1.0313e+05 2663.4 496.02 v TempK 288 342.18 294.61 291.49 v Density 1.205 1.205 1.205 1.205 v TurbVisc 3.9407e-15 9.2159e-05 5.2662e-05 6.923e-05 v CourantNb 3.419e-09 0.00018094 1.3926e-05 9.3472e-06 v FourierNb 0.079264 0.6281 0.17881 0.14932 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9647 4.9647 0.00059156 -6.1507e-07 v volume_forces[Z] -4.9647 4.9647 -0.00059149 7.2499e-07 v ǁvolume_forcesǁ 2.8751e-08 4.9656 0.59752 0.31268 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.81 291.63 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014297 5.0582e-05 2.8146e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.079273 0.6281 0.17882 0.14933 INSTANT 0.100537200E+01 TIME STEP NUMBER 1044 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10627E-04 0.21485E-02 Friction velocity uk : 0.10627E-04 0.21484E-02 Dimensionless distance yplus : 0.70764E-04 0.14294E-01 Friction thermal sca. tstar : -0.16826E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.49700E-04 0.10039E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10627E-04 0.21485E-02 Friction velocity uk : 0.10627E-04 0.21484E-02 Dimensionless distance yplus : 0.70764E-04 0.14294E-01 Friction thermal sca. tstar : -0.16826E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.49700E-04 0.10039E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.40381E-08 3 0.68898E-07 0.11439E-12 0.65451E+00 c Velocity[X] 0.24193E-32 c Velocity[Y] 0.57187E-13 c Velocity[Z] 0.57203E-13 c Pressure 0.53206E-14 16 0.41249E-07 0.41249E-07 0.74904E+00 c k 0.23993E-06 2 0.23370E-07 0.55509E-09 0.10789E+01 c omega 0.13153E+02 1 0.58998E-09 0.69950E-01 0.13769E-02 c TempK 0.94846E+02 1 0.57603E-07 0.12724E-01 0.12464E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.1667e-14 6.8697e-14 -8.5737e-18 -2.2561e-18 v Velocity[Y] -0.00011768 0.00011082 1.9979e-11 -2.7863e-12 v Velocity[Z] -0.0001107 0.00011769 -3.032e-10 -1.2178e-12 v ǁVelocityǁ 8.0991e-10 0.00012607 1.2006e-05 9.3156e-06 v Pressure -0.0017511 0.025893 0.0015107 -2.1768e-20 v k 3.3553e-10 0.00081676 0.00051326 0.00065955 v omega 10.681 1.0313e+05 2663.4 496.01 v TempK 288 342.18 294.61 291.5 v Density 1.205 1.205 1.205 1.205 v TurbVisc 3.9305e-15 9.2151e-05 5.2648e-05 6.9213e-05 v CourantNb 3.4202e-09 0.00018089 1.3926e-05 9.3498e-06 v FourierNb 0.079214 0.6281 0.17878 0.1493 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9647 4.9647 0.00059173 -6.1525e-07 v volume_forces[Z] -4.9647 4.9647 -0.00059166 7.2518e-07 v ǁvolume_forcesǁ 2.9014e-08 4.9657 0.59768 0.31282 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.81 291.63 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014294 5.0572e-05 2.814e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.079222 0.6281 0.17879 0.14931 INSTANT 0.100633500E+01 TIME STEP NUMBER 1045 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10682E-04 0.21480E-02 Friction velocity uk : 0.10682E-04 0.21480E-02 Dimensionless distance yplus : 0.71127E-04 0.14291E-01 Friction thermal sca. tstar : -0.17009E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.49955E-04 0.10037E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10682E-04 0.21480E-02 Friction velocity uk : 0.10682E-04 0.21480E-02 Dimensionless distance yplus : 0.71127E-04 0.14291E-01 Friction thermal sca. tstar : -0.17009E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.49955E-04 0.10037E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.40394E-08 3 0.68775E-07 0.11407E-12 0.65350E+00 c Velocity[X] 0.24121E-32 c Velocity[Y] 0.57025E-13 c Velocity[Z] 0.57041E-13 c Pressure 0.53089E-14 16 0.41158E-07 0.41158E-07 0.74829E+00 c k 0.23968E-06 2 0.23339E-07 0.55305E-09 0.10781E+01 c omega 0.13153E+02 1 0.58872E-09 0.69708E-01 0.13745E-02 c TempK 0.94847E+02 1 0.57525E-07 0.12706E-01 0.12455E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.1631e-14 6.8668e-14 -8.5703e-18 -2.2553e-18 v Velocity[Y] -0.00011766 0.0001108 2.2364e-11 -2.7844e-12 v Velocity[Z] -0.00011068 0.00011766 -3.0548e-10 -1.2171e-12 v ǁVelocityǁ 8.1724e-10 0.00012605 1.2008e-05 9.3201e-06 v Pressure -0.0017528 0.025905 0.0015115 -5.3047e-20 v k 3.3466e-10 0.000816 0.0005127 0.00065885 v omega 10.672 1.0313e+05 2663.4 496 v TempK 288 342.18 294.61 291.5 v Density 1.205 1.205 1.205 1.205 v TurbVisc 3.9204e-15 9.2142e-05 5.2634e-05 6.9196e-05 v CourantNb 3.4214e-09 0.00018084 1.3927e-05 9.3525e-06 v FourierNb 0.079163 0.6281 0.17875 0.14927 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9647 4.9648 0.00059189 -6.1544e-07 v volume_forces[Z] -4.9647 4.9648 -0.00059182 7.2538e-07 v ǁvolume_forcesǁ 2.9278e-08 4.9657 0.59784 0.31297 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.81 291.64 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014291 5.0562e-05 2.8135e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.079171 0.6281 0.17877 0.14928 INSTANT 0.100729800E+01 TIME STEP NUMBER 1046 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10736E-04 0.21476E-02 Friction velocity uk : 0.10736E-04 0.21476E-02 Dimensionless distance yplus : 0.71489E-04 0.14288E-01 Friction thermal sca. tstar : -0.17199E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.50209E-04 0.10035E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10736E-04 0.21476E-02 Friction velocity uk : 0.10736E-04 0.21476E-02 Dimensionless distance yplus : 0.71489E-04 0.14288E-01 Friction thermal sca. tstar : -0.17199E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.50209E-04 0.10035E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.40406E-08 3 0.68657E-07 0.11374E-12 0.65249E+00 c Velocity[X] 0.24050E-32 c Velocity[Y] 0.56863E-13 c Velocity[Z] 0.56880E-13 c Pressure 0.53028E-14 16 0.41110E-07 0.41110E-07 0.74754E+00 c k 0.23944E-06 2 0.23308E-07 0.55102E-09 0.10772E+01 c omega 0.13153E+02 1 0.58747E-09 0.69466E-01 0.13721E-02 c TempK 0.94847E+02 1 0.57446E-07 0.12687E-01 0.12446E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.1595e-14 6.864e-14 -8.5669e-18 -2.2545e-18 v Velocity[Y] -0.00011763 0.00011078 2.4746e-11 -2.7824e-12 v Velocity[Z] -0.00011065 0.00011764 -3.0776e-10 -1.2163e-12 v ǁVelocityǁ 8.2458e-10 0.00012602 1.2011e-05 9.3246e-06 v Pressure -0.0017544 0.025917 0.0015123 -2.1905e-19 v k 3.338e-10 0.00081525 0.00051214 0.00065815 v omega 10.663 1.0313e+05 2663.4 495.99 v TempK 288 342.18 294.61 291.5 v Density 1.205 1.205 1.205 1.205 v TurbVisc 3.9103e-15 9.2133e-05 5.2621e-05 6.9179e-05 v CourantNb 3.4226e-09 0.00018079 1.3927e-05 9.3551e-06 v FourierNb 0.079113 0.6281 0.17873 0.14924 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9648 4.9648 0.00059206 -6.1563e-07 v volume_forces[Z] -4.9648 4.9648 -0.00059199 7.2558e-07 v ǁvolume_forcesǁ 2.9543e-08 4.9657 0.59801 0.31312 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.82 291.64 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014288 5.0552e-05 2.8129e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.079121 0.6281 0.17874 0.14925 INSTANT 0.100826100E+01 TIME STEP NUMBER 1047 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10790E-04 0.21472E-02 Friction velocity uk : 0.10790E-04 0.21472E-02 Dimensionless distance yplus : 0.71850E-04 0.14286E-01 Friction thermal sca. tstar : -0.17395E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.50463E-04 0.10033E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10790E-04 0.21472E-02 Friction velocity uk : 0.10790E-04 0.21472E-02 Dimensionless distance yplus : 0.71850E-04 0.14286E-01 Friction thermal sca. tstar : -0.17395E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.50463E-04 0.10033E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.40418E-08 3 0.68530E-07 0.11342E-12 0.65148E+00 c Velocity[X] 0.23980E-32 c Velocity[Y] 0.56702E-13 c Velocity[Z] 0.56718E-13 c Pressure 0.52938E-14 16 0.41040E-07 0.41040E-07 0.74679E+00 c k 0.23919E-06 2 0.23277E-07 0.54900E-09 0.10763E+01 c omega 0.13153E+02 1 0.58622E-09 0.69226E-01 0.13698E-02 c TempK 0.94848E+02 1 0.57368E-07 0.12669E-01 0.12436E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.1559e-14 6.8611e-14 -8.5635e-18 -2.2538e-18 v Velocity[Y] -0.00011761 0.00011076 2.7126e-11 -2.7804e-12 v Velocity[Z] -0.00011063 0.00011762 -3.1004e-10 -1.2155e-12 v ǁVelocityǁ 8.3195e-10 0.000126 1.2014e-05 9.329e-06 v Pressure -0.001756 0.025929 0.0015131 1.2894e-19 v k 3.3295e-10 0.00081449 0.00051158 0.00065745 v omega 10.655 1.0313e+05 2663.4 495.99 v TempK 288 342.18 294.61 291.5 v Density 1.205 1.205 1.205 1.205 v TurbVisc 3.9003e-15 9.2125e-05 5.2607e-05 6.9162e-05 v CourantNb 3.4237e-09 0.00018074 1.3927e-05 9.3577e-06 v FourierNb 0.079062 0.6281 0.1787 0.14921 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9648 4.9648 0.00059223 -6.1581e-07 v volume_forces[Z] -4.9648 4.9648 -0.00059216 7.2578e-07 v ǁvolume_forcesǁ 2.9809e-08 4.9658 0.59817 0.31327 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.82 291.64 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014286 5.0542e-05 2.8123e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.079071 0.6281 0.17872 0.14922 INSTANT 0.100922400E+01 TIME STEP NUMBER 1048 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10844E-04 0.21468E-02 Friction velocity uk : 0.10844E-04 0.21468E-02 Dimensionless distance yplus : 0.72209E-04 0.14283E-01 Friction thermal sca. tstar : -0.17598E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.50715E-04 0.10031E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10844E-04 0.21468E-02 Friction velocity uk : 0.10844E-04 0.21468E-02 Dimensionless distance yplus : 0.72209E-04 0.14283E-01 Friction thermal sca. tstar : -0.17598E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.50715E-04 0.10031E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.40430E-08 3 0.68410E-07 0.11310E-12 0.65048E+00 c Velocity[X] 0.23909E-32 c Velocity[Y] 0.56541E-13 c Velocity[Z] 0.56557E-13 c Pressure 0.52867E-14 16 0.40984E-07 0.40984E-07 0.74604E+00 c k 0.23895E-06 2 0.23246E-07 0.54699E-09 0.10754E+01 c omega 0.13153E+02 1 0.58497E-09 0.68986E-01 0.13674E-02 c TempK 0.94848E+02 1 0.57290E-07 0.12651E-01 0.12427E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.1523e-14 6.8583e-14 -8.5601e-18 -2.253e-18 v Velocity[Y] -0.00011758 0.00011074 2.9503e-11 -2.7785e-12 v Velocity[Z] -0.00011061 0.00011759 -3.1232e-10 -1.2148e-12 v ǁVelocityǁ 8.3933e-10 0.00012597 1.2017e-05 9.3334e-06 v Pressure -0.0017577 0.025941 0.0015139 1.0315e-19 v k 3.3209e-10 0.00081373 0.00051103 0.00065676 v omega 10.646 1.0313e+05 2663.4 495.98 v TempK 288 342.19 294.62 291.5 v Density 1.205 1.205 1.205 1.205 v TurbVisc 3.8902e-15 9.2116e-05 5.2593e-05 6.9145e-05 v CourantNb 3.4249e-09 0.0001807 1.3928e-05 9.3604e-06 v FourierNb 0.079012 0.6281 0.17868 0.14918 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9648 4.9649 0.00059239 -6.16e-07 v volume_forces[Z] -4.9648 4.9649 -0.00059232 7.2597e-07 v ǁvolume_forcesǁ 3.0075e-08 4.9658 0.59834 0.31341 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.82 291.64 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014283 5.0532e-05 2.8117e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.07902 0.6281 0.17869 0.14919 INSTANT 0.101018700E+01 TIME STEP NUMBER 1049 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10898E-04 0.21464E-02 Friction velocity uk : 0.10898E-04 0.21464E-02 Dimensionless distance yplus : 0.72567E-04 0.14280E-01 Friction thermal sca. tstar : -0.17808E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.50967E-04 0.10029E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10898E-04 0.21464E-02 Friction velocity uk : 0.10898E-04 0.21464E-02 Dimensionless distance yplus : 0.72567E-04 0.14280E-01 Friction thermal sca. tstar : -0.17808E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.50967E-04 0.10029E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.40442E-08 3 0.68300E-07 0.11278E-12 0.64947E+00 c Velocity[X] 0.23838E-32 c Velocity[Y] 0.56380E-13 c Velocity[Z] 0.56397E-13 c Pressure 0.52871E-14 16 0.40987E-07 0.40987E-07 0.74529E+00 c k 0.23871E-06 2 0.23215E-07 0.54499E-09 0.10746E+01 c omega 0.13153E+02 1 0.58373E-09 0.68748E-01 0.13650E-02 c TempK 0.94849E+02 1 0.57213E-07 0.12633E-01 0.12419E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.1487e-14 6.8555e-14 -8.5567e-18 -2.2522e-18 v Velocity[Y] -0.00011756 0.00011072 3.1879e-11 -2.7766e-12 v Velocity[Z] -0.00011059 0.00011757 -3.1459e-10 -1.214e-12 v ǁVelocityǁ 8.4674e-10 0.00012594 1.2019e-05 9.3378e-06 v Pressure -0.0017593 0.025953 0.0015147 7.9423e-20 v k 3.3124e-10 0.00081298 0.00051047 0.00065606 v omega 10.637 1.0313e+05 2663.4 495.97 v TempK 288 342.19 294.62 291.5 v Density 1.205 1.205 1.205 1.205 v TurbVisc 3.8802e-15 9.2108e-05 5.2579e-05 6.9128e-05 v CourantNb 3.4261e-09 0.00018065 1.3928e-05 9.363e-06 v FourierNb 0.078962 0.6281 0.17865 0.14916 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9649 4.9649 0.00059256 -6.1618e-07 v volume_forces[Z] -4.9649 4.9649 -0.00059249 7.2617e-07 v ǁvolume_forcesǁ 3.0342e-08 4.9658 0.5985 0.31356 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.82 291.64 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.01428 5.0522e-05 2.8111e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.07897 0.6281 0.17867 0.14917 INSTANT 0.101115000E+01 TIME STEP NUMBER 1050 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10951E-04 0.21460E-02 Friction velocity uk : 0.10951E-04 0.21460E-02 Dimensionless distance yplus : 0.72925E-04 0.14277E-01 Friction thermal sca. tstar : -0.18026E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.51218E-04 0.10028E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10951E-04 0.21460E-02 Friction velocity uk : 0.10951E-04 0.21460E-02 Dimensionless distance yplus : 0.72925E-04 0.14277E-01 Friction thermal sca. tstar : -0.18026E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.51218E-04 0.10028E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.40454E-08 3 0.68167E-07 0.11246E-12 0.64847E+00 c Velocity[X] 0.23769E-32 c Velocity[Y] 0.56219E-13 c Velocity[Z] 0.56236E-13 c Pressure 0.52719E-14 16 0.40869E-07 0.40869E-07 0.74455E+00 c k 0.23846E-06 2 0.23184E-07 0.54300E-09 0.10737E+01 c omega 0.13153E+02 1 0.58249E-09 0.68511E-01 0.13627E-02 c TempK 0.94849E+02 1 0.57135E-07 0.12615E-01 0.12410E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.1451e-14 6.8526e-14 -8.5533e-18 -2.2514e-18 v Velocity[Y] -0.00011754 0.0001107 3.4253e-11 -2.7747e-12 v Velocity[Z] -0.00011057 0.00011754 -3.1686e-10 -1.2132e-12 v ǁVelocityǁ 8.5417e-10 0.00012592 1.2022e-05 9.3422e-06 v Pressure -0.001761 0.025965 0.0015155 3.0789e-20 v k 3.3039e-10 0.00081223 0.00050992 0.00065537 v omega 10.628 1.0313e+05 2663.4 495.96 v TempK 288 342.19 294.62 291.51 v Density 1.205 1.205 1.205 1.205 v TurbVisc 3.8703e-15 9.2099e-05 5.2565e-05 6.9112e-05 v CourantNb 3.4272e-09 0.0001806 1.3928e-05 9.3656e-06 v FourierNb 0.078912 0.6281 0.17863 0.14913 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9649 4.9649 0.00059272 -6.1637e-07 v volume_forces[Z] -4.9649 4.9649 -0.00059265 7.2637e-07 v ǁvolume_forcesǁ 3.061e-08 4.9658 0.59866 0.31371 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.82 291.64 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014277 5.0512e-05 2.8105e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.07892 0.6281 0.17864 0.14914 INSTANT 0.101211300E+01 TIME STEP NUMBER 1051 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11005E-04 0.21456E-02 Friction velocity uk : 0.11005E-04 0.21455E-02 Dimensionless distance yplus : 0.73281E-04 0.14275E-01 Friction thermal sca. tstar : -0.18252E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.51468E-04 0.10026E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11005E-04 0.21456E-02 Friction velocity uk : 0.11005E-04 0.21455E-02 Dimensionless distance yplus : 0.73281E-04 0.14275E-01 Friction thermal sca. tstar : -0.18252E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.51468E-04 0.10026E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.40467E-08 3 0.68056E-07 0.11214E-12 0.64746E+00 c Velocity[X] 0.23699E-32 c Velocity[Y] 0.56059E-13 c Velocity[Z] 0.56076E-13 c Pressure 0.52718E-14 16 0.40868E-07 0.40868E-07 0.74381E+00 c k 0.23822E-06 2 0.23154E-07 0.54101E-09 0.10728E+01 c omega 0.13153E+02 1 0.58126E-09 0.68274E-01 0.13603E-02 c TempK 0.94850E+02 1 0.57058E-07 0.12597E-01 0.12401E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.1416e-14 6.8498e-14 -8.5499e-18 -2.2506e-18 v Velocity[Y] -0.00011751 0.00011067 3.6625e-11 -2.7727e-12 v Velocity[Z] -0.00011055 0.00011752 -3.1912e-10 -1.2124e-12 v ǁVelocityǁ 8.5059e-10 0.00012589 1.2025e-05 9.3466e-06 v Pressure -0.0017626 0.025976 0.0015163 5.8439e-20 v k 3.2954e-10 0.00081148 0.00050936 0.00065468 v omega 10.619 1.0313e+05 2663.4 495.95 v TempK 288 342.19 294.62 291.51 v Density 1.205 1.205 1.205 1.205 v TurbVisc 3.8604e-15 9.2091e-05 5.2551e-05 6.9095e-05 v CourantNb 3.4284e-09 0.00018055 1.3928e-05 9.3682e-06 v FourierNb 0.078862 0.6281 0.1786 0.1491 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9649 4.965 0.00059289 -6.1655e-07 v volume_forces[Z] -4.9649 4.965 -0.00059282 7.2656e-07 v ǁvolume_forcesǁ 3.0878e-08 4.9659 0.59883 0.31386 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.83 291.65 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014275 5.0502e-05 2.81e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.07887 0.6281 0.17861 0.14911 INSTANT 0.101307600E+01 TIME STEP NUMBER 1052 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11003E-04 0.21452E-02 Friction velocity uk : 0.11002E-04 0.21451E-02 Dimensionless distance yplus : 0.73265E-04 0.14272E-01 Friction thermal sca. tstar : -0.18487E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.51456E-04 0.10024E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11003E-04 0.21452E-02 Friction velocity uk : 0.11002E-04 0.21451E-02 Dimensionless distance yplus : 0.73265E-04 0.14272E-01 Friction thermal sca. tstar : -0.18487E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.51456E-04 0.10024E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.40479E-08 3 0.67932E-07 0.11182E-12 0.64646E+00 c Velocity[X] 0.23630E-32 c Velocity[Y] 0.55899E-13 c Velocity[Z] 0.55916E-13 c Pressure 0.52578E-14 16 0.40758E-07 0.40758E-07 0.74306E+00 c k 0.23798E-06 2 0.23123E-07 0.53904E-09 0.10720E+01 c omega 0.13153E+02 1 0.58003E-09 0.68039E-01 0.13580E-02 c TempK 0.94850E+02 1 0.56981E-07 0.12579E-01 0.12392E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.138e-14 6.847e-14 -8.5465e-18 -2.2499e-18 v Velocity[Y] -0.00011749 0.00011065 3.8994e-11 -2.7708e-12 v Velocity[Z] -0.00011053 0.00011749 -3.2139e-10 -1.2116e-12 v ǁVelocityǁ 8.4147e-10 0.00012586 1.2027e-05 9.351e-06 v Pressure -0.0017642 0.025988 0.0015171 1.51e-20 v k 3.287e-10 0.00081073 0.00050881 0.00065399 v omega 10.61 1.0313e+05 2663.4 495.95 v TempK 288 342.19 294.62 291.51 v Density 1.205 1.205 1.205 1.205 v TurbVisc 3.8505e-15 9.2082e-05 5.2537e-05 6.9078e-05 v CourantNb 3.4295e-09 0.0001805 1.3929e-05 9.3708e-06 v FourierNb 0.078812 0.6281 0.17857 0.14907 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.965 4.965 0.00059306 -6.1673e-07 v volume_forces[Z] -4.965 4.965 -0.00059299 7.2676e-07 v ǁvolume_forcesǁ 3.0749e-08 4.9659 0.59899 0.314 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.83 291.65 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014272 5.0492e-05 2.8094e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.07882 0.6281 0.17859 0.14908 INSTANT 0.101403900E+01 TIME STEP NUMBER 1053 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10936E-04 0.21448E-02 Friction velocity uk : 0.10936E-04 0.21447E-02 Dimensionless distance yplus : 0.72825E-04 0.14269E-01 Friction thermal sca. tstar : -0.18730E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.51147E-04 0.10022E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10936E-04 0.21448E-02 Friction velocity uk : 0.10936E-04 0.21447E-02 Dimensionless distance yplus : 0.72825E-04 0.14269E-01 Friction thermal sca. tstar : -0.18730E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.51147E-04 0.10022E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.40491E-08 3 0.67814E-07 0.11150E-12 0.64546E+00 c Velocity[X] 0.23561E-32 c Velocity[Y] 0.55740E-13 c Velocity[Z] 0.55756E-13 c Pressure 0.52503E-14 16 0.40701E-07 0.40701E-07 0.74232E+00 c k 0.23774E-06 2 0.23093E-07 0.53707E-09 0.10711E+01 c omega 0.13153E+02 1 0.57880E-09 0.67804E-01 0.13556E-02 c TempK 0.94851E+02 1 0.56904E-07 0.12561E-01 0.12383E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.1344e-14 6.8441e-14 -8.5432e-18 -2.2491e-18 v Velocity[Y] -0.00011746 0.00011063 4.1361e-11 -2.7689e-12 v Velocity[Z] -0.00011051 0.00011747 -3.2365e-10 -1.2108e-12 v ǁVelocityǁ 8.3235e-10 0.00012584 1.203e-05 9.3554e-06 v Pressure -0.0017659 0.026 0.0015179 -1.0374e-19 v k 3.2786e-10 0.00080998 0.00050826 0.0006533 v omega 10.601 1.0313e+05 2663.4 495.94 v TempK 288 342.19 294.63 291.51 v Density 1.205 1.205 1.205 1.205 v TurbVisc 3.8406e-15 9.2074e-05 5.2524e-05 6.9061e-05 v CourantNb 3.4306e-09 0.00018045 1.3929e-05 9.3734e-06 v FourierNb 0.078763 0.6281 0.17855 0.14905 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.965 4.965 0.00059322 -6.1692e-07 v volume_forces[Z] -4.965 4.965 -0.00059315 7.2695e-07 v ǁvolume_forcesǁ 3.0419e-08 4.9659 0.59915 0.31415 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.83 291.65 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014269 5.0482e-05 2.8088e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.078771 0.6281 0.17856 0.14905 INSTANT 0.101500200E+01 TIME STEP NUMBER 1054 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10870E-04 0.21443E-02 Friction velocity uk : 0.10870E-04 0.21443E-02 Dimensionless distance yplus : 0.72381E-04 0.14267E-01 Friction thermal sca. tstar : -0.18984E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.50836E-04 0.10020E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10870E-04 0.21443E-02 Friction velocity uk : 0.10870E-04 0.21443E-02 Dimensionless distance yplus : 0.72381E-04 0.14267E-01 Friction thermal sca. tstar : -0.18984E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.50836E-04 0.10020E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.40503E-08 3 0.67680E-07 0.11118E-12 0.64446E+00 c Velocity[X] 0.23492E-32 c Velocity[Y] 0.55580E-13 c Velocity[Z] 0.55597E-13 c Pressure 0.52439E-14 16 0.40650E-07 0.40650E-07 0.74158E+00 c k 0.23749E-06 2 0.23062E-07 0.53512E-09 0.10702E+01 c omega 0.13153E+02 1 0.57758E-09 0.67571E-01 0.13533E-02 c TempK 0.94851E+02 1 0.56827E-07 0.12543E-01 0.12374E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.1309e-14 6.8413e-14 -8.5398e-18 -2.2483e-18 v Velocity[Y] -0.00011744 0.00011061 4.3726e-11 -2.767e-12 v Velocity[Z] -0.00011049 0.00011744 -3.2591e-10 -1.21e-12 v ǁVelocityǁ 8.2321e-10 0.00012581 1.2032e-05 9.3598e-06 v Pressure -0.0017675 0.026012 0.0015187 1.1786e-19 v k 3.2702e-10 0.00080923 0.00050771 0.00065261 v omega 10.593 1.0313e+05 2663.4 495.93 v TempK 288 342.19 294.63 291.51 v Density 1.205 1.205 1.205 1.205 v TurbVisc 3.8308e-15 9.2065e-05 5.251e-05 6.9044e-05 v CourantNb 3.4317e-09 0.0001804 1.3929e-05 9.3759e-06 v FourierNb 0.078713 0.6281 0.17852 0.14902 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.965 4.9651 0.00059339 -6.171e-07 v volume_forces[Z] -4.965 4.9651 -0.00059332 7.2714e-07 v ǁvolume_forcesǁ 3.0089e-08 4.966 0.59932 0.3143 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.83 291.65 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014267 5.0472e-05 2.8082e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.078721 0.6281 0.17854 0.14903 INSTANT 0.101596500E+01 TIME STEP NUMBER 1055 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10803E-04 0.21439E-02 Friction velocity uk : 0.10803E-04 0.21439E-02 Dimensionless distance yplus : 0.71934E-04 0.14264E-01 Friction thermal sca. tstar : -0.19248E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.50522E-04 0.10018E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10803E-04 0.21439E-02 Friction velocity uk : 0.10803E-04 0.21439E-02 Dimensionless distance yplus : 0.71934E-04 0.14264E-01 Friction thermal sca. tstar : -0.19248E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.50522E-04 0.10018E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.40515E-08 3 0.67574E-07 0.11086E-12 0.64346E+00 c Velocity[X] 0.23422E-32 c Velocity[Y] 0.55421E-13 c Velocity[Z] 0.55438E-13 c Pressure 0.52359E-14 16 0.40588E-07 0.40588E-07 0.74085E+00 c k 0.23725E-06 2 0.23032E-07 0.53317E-09 0.10694E+01 c omega 0.13153E+02 1 0.57636E-09 0.67339E-01 0.13510E-02 c TempK 0.94852E+02 1 0.56750E-07 0.12525E-01 0.12365E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.1273e-14 6.8385e-14 -8.5364e-18 -2.2475e-18 v Velocity[Y] -0.00011741 0.00011059 4.6089e-11 -2.7651e-12 v Velocity[Z] -0.00011046 0.00011742 -3.2816e-10 -1.2091e-12 v ǁVelocityǁ 8.1408e-10 0.00012578 1.2035e-05 9.3641e-06 v Pressure -0.0017691 0.026024 0.0015195 3.1769e-20 v k 3.2619e-10 0.00080848 0.00050716 0.00065193 v omega 10.584 1.0313e+05 2663.4 495.92 v TempK 288 342.19 294.63 291.51 v Density 1.205 1.205 1.205 1.205 v TurbVisc 3.821e-15 9.2057e-05 5.2496e-05 6.9028e-05 v CourantNb 3.4329e-09 0.00018035 1.393e-05 9.3785e-06 v FourierNb 0.078664 0.6281 0.1785 0.14899 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9651 4.9651 0.00059355 -6.1728e-07 v volume_forces[Z] -4.9651 4.9651 -0.00059348 7.2734e-07 v ǁvolume_forcesǁ 2.9759e-08 4.966 0.59948 0.31445 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.83 291.65 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014264 5.0462e-05 2.8076e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.078672 0.6281 0.17851 0.149 INSTANT 0.101692800E+01 TIME STEP NUMBER 1056 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10735E-04 0.21435E-02 Friction velocity uk : 0.10735E-04 0.21435E-02 Dimensionless distance yplus : 0.71484E-04 0.14261E-01 Friction thermal sca. tstar : -0.19523E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.50206E-04 0.10016E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10735E-04 0.21435E-02 Friction velocity uk : 0.10735E-04 0.21435E-02 Dimensionless distance yplus : 0.71484E-04 0.14261E-01 Friction thermal sca. tstar : -0.19523E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.50206E-04 0.10016E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.40526E-08 3 0.67460E-07 0.11054E-12 0.64246E+00 c Velocity[X] 0.23355E-32 c Velocity[Y] 0.55262E-13 c Velocity[Z] 0.55279E-13 c Pressure 0.52287E-14 16 0.40532E-07 0.40532E-07 0.74011E+00 c k 0.23701E-06 2 0.23002E-07 0.53123E-09 0.10685E+01 c omega 0.13153E+02 1 0.57514E-09 0.67107E-01 0.13486E-02 c TempK 0.94852E+02 1 0.56674E-07 0.12507E-01 0.12356E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.1238e-14 6.8357e-14 -8.5331e-18 -2.2468e-18 v Velocity[Y] -0.00011739 0.00011057 4.845e-11 -2.7633e-12 v Velocity[Z] -0.00011044 0.00011739 -3.3041e-10 -1.2083e-12 v ǁVelocityǁ 8.0493e-10 0.00012576 1.2038e-05 9.3685e-06 v Pressure -0.0017708 0.026036 0.0015203 5.2752e-20 v k 3.2536e-10 0.00080774 0.00050661 0.00065124 v omega 10.575 1.0313e+05 2663.3 495.92 v TempK 288 342.19 294.63 291.52 v Density 1.205 1.205 1.205 1.205 v TurbVisc 3.8113e-15 9.2048e-05 5.2482e-05 6.9011e-05 v CourantNb 3.434e-09 0.0001803 1.393e-05 9.3811e-06 v FourierNb 0.078614 0.6281 0.17847 0.14896 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9651 4.9651 0.00059372 -6.1747e-07 v volume_forces[Z] -4.9651 4.9651 -0.00059365 7.2753e-07 v ǁvolume_forcesǁ 2.9429e-08 4.966 0.59964 0.31459 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.83 291.65 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014261 5.0453e-05 2.8071e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.078622 0.6281 0.17849 0.14897 INSTANT 0.101789100E+01 TIME STEP NUMBER 1057 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10667E-04 0.21431E-02 Friction velocity uk : 0.10667E-04 0.21431E-02 Dimensionless distance yplus : 0.71029E-04 0.14258E-01 Friction thermal sca. tstar : -0.19811E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.49886E-04 0.10014E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10667E-04 0.21431E-02 Friction velocity uk : 0.10667E-04 0.21431E-02 Dimensionless distance yplus : 0.71029E-04 0.14258E-01 Friction thermal sca. tstar : -0.19811E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.49886E-04 0.10014E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.40538E-08 3 0.67343E-07 0.11022E-12 0.64146E+00 c Velocity[X] 0.23287E-32 c Velocity[Y] 0.55104E-13 c Velocity[Z] 0.55121E-13 c Pressure 0.52291E-14 16 0.40535E-07 0.40535E-07 0.73937E+00 c k 0.23677E-06 2 0.22971E-07 0.52930E-09 0.10676E+01 c omega 0.13153E+02 1 0.57393E-09 0.66877E-01 0.13463E-02 c TempK 0.94853E+02 1 0.56598E-07 0.12489E-01 0.12347E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.1202e-14 6.8329e-14 -8.5297e-18 -2.246e-18 v Velocity[Y] -0.00011736 0.00011055 5.0808e-11 -2.7614e-12 v Velocity[Z] -0.00011042 0.00011737 -3.3266e-10 -1.2075e-12 v ǁVelocityǁ 7.9578e-10 0.00012573 1.204e-05 9.3728e-06 v Pressure -0.0017724 0.026047 0.0015211 -1.2021e-19 v k 3.2453e-10 0.00080699 0.00050607 0.00065056 v omega 10.566 1.0313e+05 2663.3 495.91 v TempK 288 342.19 294.63 291.52 v Density 1.205 1.205 1.205 1.205 v TurbVisc 3.8016e-15 9.204e-05 5.2468e-05 6.8994e-05 v CourantNb 3.4351e-09 0.00018025 1.393e-05 9.3836e-06 v FourierNb 0.078565 0.6281 0.17845 0.14893 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9651 4.9652 0.00059388 -6.1765e-07 v volume_forces[Z] -4.9651 4.9652 -0.00059381 7.2773e-07 v ǁvolume_forcesǁ 2.9098e-08 4.9661 0.59981 0.31474 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.84 291.66 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014258 5.0443e-05 2.8065e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.078573 0.6281 0.17846 0.14894 INSTANT 0.101885400E+01 TIME STEP NUMBER 1058 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10598E-04 0.21427E-02 Friction velocity uk : 0.10598E-04 0.21427E-02 Dimensionless distance yplus : 0.70571E-04 0.14256E-01 Friction thermal sca. tstar : -0.20111E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.49565E-04 0.10012E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10598E-04 0.21427E-02 Friction velocity uk : 0.10598E-04 0.21427E-02 Dimensionless distance yplus : 0.70571E-04 0.14256E-01 Friction thermal sca. tstar : -0.20111E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.49565E-04 0.10012E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.40550E-08 3 0.67224E-07 0.10991E-12 0.64046E+00 c Velocity[X] 0.23219E-32 c Velocity[Y] 0.54945E-13 c Velocity[Z] 0.54962E-13 c Pressure 0.52172E-14 16 0.40442E-07 0.40442E-07 0.73864E+00 c k 0.23653E-06 2 0.22941E-07 0.52737E-09 0.10668E+01 c omega 0.13153E+02 1 0.57272E-09 0.66647E-01 0.13440E-02 c TempK 0.94853E+02 1 0.56522E-07 0.12472E-01 0.12338E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.1167e-14 6.8301e-14 -8.5263e-18 -2.2452e-18 v Velocity[Y] -0.00011734 0.00011053 5.3165e-11 -2.7594e-12 v Velocity[Z] -0.0001104 0.00011734 -3.349e-10 -1.2066e-12 v ǁVelocityǁ 7.8663e-10 0.0001257 1.2043e-05 9.3772e-06 v Pressure -0.001774 0.026059 0.0015219 -1.2668e-19 v k 3.237e-10 0.00080625 0.00050552 0.00064988 v omega 10.558 1.0313e+05 2663.3 495.9 v TempK 288 342.19 294.63 291.52 v Density 1.205 1.205 1.205 1.205 v TurbVisc 3.7919e-15 9.2031e-05 5.2455e-05 6.8977e-05 v CourantNb 3.4362e-09 0.0001802 1.3931e-05 9.3862e-06 v FourierNb 0.078516 0.6281 0.17842 0.14891 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9652 4.9652 0.00059405 -6.1783e-07 v volume_forces[Z] -4.9652 4.9652 -0.00059398 7.2792e-07 v ǁvolume_forcesǁ 2.8768e-08 4.9661 0.59997 0.31489 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.84 291.66 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014256 5.0433e-05 2.8059e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.078524 0.6281 0.17843 0.14892 INSTANT 0.101981700E+01 TIME STEP NUMBER 1059 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10529E-04 0.21423E-02 Friction velocity uk : 0.10529E-04 0.21423E-02 Dimensionless distance yplus : 0.70109E-04 0.14253E-01 Friction thermal sca. tstar : -0.20425E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.49240E-04 0.10010E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10529E-04 0.21423E-02 Friction velocity uk : 0.10529E-04 0.21423E-02 Dimensionless distance yplus : 0.70109E-04 0.14253E-01 Friction thermal sca. tstar : -0.20425E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.49240E-04 0.10010E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.40562E-08 3 0.67105E-07 0.10959E-12 0.63946E+00 c Velocity[X] 0.23151E-32 c Velocity[Y] 0.54787E-13 c Velocity[Z] 0.54804E-13 c Pressure 0.52070E-14 16 0.40362E-07 0.40362E-07 0.73791E+00 c k 0.23629E-06 2 0.22911E-07 0.52546E-09 0.10659E+01 c omega 0.13153E+02 1 0.57151E-09 0.66419E-01 0.13417E-02 c TempK 0.94854E+02 1 0.56446E-07 0.12454E-01 0.12329E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.1131e-14 6.8273e-14 -8.523e-18 -2.2444e-18 v Velocity[Y] -0.00011731 0.00011051 5.5519e-11 -2.7576e-12 v Velocity[Z] -0.00011038 0.00011732 -3.3714e-10 -1.2057e-12 v ǁVelocityǁ 7.7748e-10 0.00012568 1.2046e-05 9.3815e-06 v Pressure -0.0017757 0.026071 0.0015227 -2.9122e-20 v k 3.2288e-10 0.00080551 0.00050497 0.00064919 v omega 10.549 1.0313e+05 2663.3 495.89 v TempK 288 342.19 294.64 291.52 v Density 1.205 1.205 1.205 1.205 v TurbVisc 3.7822e-15 9.2023e-05 5.2441e-05 6.8961e-05 v CourantNb 3.4372e-09 0.00018016 1.3931e-05 9.3888e-06 v FourierNb 0.078467 0.6281 0.1784 0.14888 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9652 4.9652 0.00059421 -6.1801e-07 v volume_forces[Z] -4.9652 4.9652 -0.00059414 7.2811e-07 v ǁvolume_forcesǁ 2.8437e-08 4.9661 0.60013 0.31503 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.84 291.66 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014253 5.0423e-05 2.8053e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.078475 0.6281 0.17841 0.14889 INSTANT 0.102078000E+01 TIME STEP NUMBER 1060 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10459E-04 0.21419E-02 Friction velocity uk : 0.10459E-04 0.21419E-02 Dimensionless distance yplus : 0.69643E-04 0.14250E-01 Friction thermal sca. tstar : -0.20755E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.48913E-04 0.10008E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10459E-04 0.21419E-02 Friction velocity uk : 0.10459E-04 0.21419E-02 Dimensionless distance yplus : 0.69643E-04 0.14250E-01 Friction thermal sca. tstar : -0.20755E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.48913E-04 0.10008E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.40574E-08 3 0.66989E-07 0.10928E-12 0.63847E+00 c Velocity[X] 0.23084E-32 c Velocity[Y] 0.54630E-13 c Velocity[Z] 0.54647E-13 c Pressure 0.51998E-14 16 0.40306E-07 0.40306E-07 0.73718E+00 c k 0.23606E-06 2 0.22881E-07 0.52356E-09 0.10651E+01 c omega 0.13153E+02 1 0.57031E-09 0.66192E-01 0.13394E-02 c TempK 0.94854E+02 1 0.56370E-07 0.12436E-01 0.12321E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.1096e-14 6.8245e-14 -8.5197e-18 -2.2437e-18 v Velocity[Y] -0.00011729 0.00011049 5.787e-11 -2.7558e-12 v Velocity[Z] -0.00011036 0.00011729 -3.3938e-10 -1.2049e-12 v ǁVelocityǁ 7.6832e-10 0.00012565 1.2048e-05 9.3858e-06 v Pressure -0.0017773 0.026083 0.0015235 1.912e-20 v k 3.2206e-10 0.00080477 0.00050443 0.00064852 v omega 10.54 1.0313e+05 2663.3 495.89 v TempK 288 342.19 294.64 291.52 v Density 1.205 1.205 1.205 1.205 v TurbVisc 3.7726e-15 9.2014e-05 5.2427e-05 6.8944e-05 v CourantNb 3.4383e-09 0.00018011 1.3931e-05 9.3913e-06 v FourierNb 0.078418 0.6281 0.17837 0.14885 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9652 4.9652 0.00059438 -6.1819e-07 v volume_forces[Z] -4.9652 4.9652 -0.00059431 7.283e-07 v ǁvolume_forcesǁ 2.8106e-08 4.9662 0.6003 0.31518 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.84 291.66 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.01425 5.0413e-05 2.8048e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.078426 0.6281 0.17838 0.14886 INSTANT 0.102174300E+01 TIME STEP NUMBER 1061 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10388E-04 0.21415E-02 Friction velocity uk : 0.10388E-04 0.21415E-02 Dimensionless distance yplus : 0.69173E-04 0.14248E-01 Friction thermal sca. tstar : -0.21101E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.48582E-04 0.10007E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10388E-04 0.21415E-02 Friction velocity uk : 0.10388E-04 0.21415E-02 Dimensionless distance yplus : 0.69173E-04 0.14248E-01 Friction thermal sca. tstar : -0.21101E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.48582E-04 0.10007E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.40586E-08 3 0.66873E-07 0.10896E-12 0.63747E+00 c Velocity[X] 0.23017E-32 c Velocity[Y] 0.54472E-13 c Velocity[Z] 0.54489E-13 c Pressure 0.51927E-14 16 0.40251E-07 0.40251E-07 0.73645E+00 c k 0.23582E-06 2 0.22851E-07 0.52166E-09 0.10642E+01 c omega 0.13153E+02 1 0.56911E-09 0.65965E-01 0.13371E-02 c TempK 0.94855E+02 1 0.56294E-07 0.12419E-01 0.12312E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.1061e-14 6.8217e-14 -8.5163e-18 -2.2429e-18 v Velocity[Y] -0.00011726 0.00011047 6.022e-11 -2.7539e-12 v Velocity[Z] -0.00011034 0.00011727 -3.4162e-10 -1.204e-12 v ǁVelocityǁ 7.5916e-10 0.00012562 1.2051e-05 9.3901e-06 v Pressure -0.0017789 0.026095 0.0015243 -5.8832e-20 v k 3.2124e-10 0.00080403 0.00050389 0.00064784 v omega 10.531 1.0313e+05 2663.3 495.88 v TempK 288 342.19 294.64 291.52 v Density 1.205 1.205 1.205 1.205 v TurbVisc 3.763e-15 9.2006e-05 5.2414e-05 6.8927e-05 v CourantNb 3.4394e-09 0.00018006 1.3931e-05 9.3938e-06 v FourierNb 0.078369 0.6281 0.17834 0.14882 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9653 4.9653 0.00059454 -6.1837e-07 v volume_forces[Z] -4.9653 4.9653 -0.00059447 7.285e-07 v ǁvolume_forcesǁ 2.7775e-08 4.9662 0.60046 0.31533 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.84 291.66 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014248 5.0403e-05 2.8042e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.078377 0.6281 0.17836 0.14883 INSTANT 0.102270600E+01 TIME STEP NUMBER 1062 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10317E-04 0.21411E-02 Friction velocity uk : 0.10317E-04 0.21411E-02 Dimensionless distance yplus : 0.68698E-04 0.14245E-01 Friction thermal sca. tstar : -0.21465E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.48249E-04 0.10005E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10317E-04 0.21411E-02 Friction velocity uk : 0.10317E-04 0.21411E-02 Dimensionless distance yplus : 0.68698E-04 0.14245E-01 Friction thermal sca. tstar : -0.21465E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.48249E-04 0.10005E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.40598E-08 3 0.66757E-07 0.10865E-12 0.63648E+00 c Velocity[X] 0.22950E-32 c Velocity[Y] 0.54315E-13 c Velocity[Z] 0.54332E-13 c Pressure 0.51866E-14 16 0.40203E-07 0.40203E-07 0.73572E+00 c k 0.23558E-06 2 0.22821E-07 0.51977E-09 0.10634E+01 c omega 0.13153E+02 1 0.56791E-09 0.65739E-01 0.13348E-02 c TempK 0.94855E+02 1 0.56219E-07 0.12401E-01 0.12303E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.1026e-14 6.8189e-14 -8.513e-18 -2.2422e-18 v Velocity[Y] -0.00011724 0.00011045 6.2567e-11 -2.7521e-12 v Velocity[Z] -0.00011032 0.00011724 -3.4385e-10 -1.2031e-12 v ǁVelocityǁ 7.5e-10 0.00012559 1.2053e-05 9.3944e-06 v Pressure -0.0017806 0.026106 0.0015251 -3.5103e-20 v k 3.2043e-10 0.0008033 0.00050334 0.00064716 v omega 10.523 1.0313e+05 2663.3 495.87 v TempK 288 342.19 294.64 291.53 v Density 1.205 1.205 1.205 1.205 v TurbVisc 3.7535e-15 9.1997e-05 5.24e-05 6.8911e-05 v CourantNb 3.4404e-09 0.00018001 1.3932e-05 9.3964e-06 v FourierNb 0.07832 0.6281 0.17832 0.1488 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9653 4.9653 0.00059471 -6.1855e-07 v volume_forces[Z] -4.9653 4.9653 -0.00059464 7.2869e-07 v ǁvolume_forcesǁ 2.7444e-08 4.9662 0.60062 0.31547 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.85 291.66 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014245 5.0393e-05 2.8036e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.078328 0.6281 0.17833 0.14881 INSTANT 0.102366900E+01 TIME STEP NUMBER 1063 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10245E-04 0.21407E-02 Friction velocity uk : 0.10245E-04 0.21407E-02 Dimensionless distance yplus : 0.68220E-04 0.14242E-01 Friction thermal sca. tstar : -0.21848E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.47913E-04 0.10003E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10245E-04 0.21407E-02 Friction velocity uk : 0.10245E-04 0.21407E-02 Dimensionless distance yplus : 0.68220E-04 0.14242E-01 Friction thermal sca. tstar : -0.21848E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.47913E-04 0.10003E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.40609E-08 3 0.66641E-07 0.10833E-12 0.63548E+00 c Velocity[X] 0.22884E-32 c Velocity[Y] 0.54158E-13 c Velocity[Z] 0.54175E-13 c Pressure 0.51785E-14 16 0.40140E-07 0.40140E-07 0.73499E+00 c k 0.23534E-06 2 0.22791E-07 0.51789E-09 0.10625E+01 c omega 0.13153E+02 1 0.56672E-09 0.65515E-01 0.13325E-02 c TempK 0.94856E+02 1 0.56144E-07 0.12383E-01 0.12294E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.099e-14 6.8161e-14 -8.5097e-18 -2.2414e-18 v Velocity[Y] -0.00011721 0.00011043 6.4912e-11 -2.7503e-12 v Velocity[Z] -0.0001103 0.00011722 -3.4608e-10 -1.2022e-12 v ǁVelocityǁ 7.4084e-10 0.00012557 1.2056e-05 9.3987e-06 v Pressure -0.0017822 0.026118 0.0015259 -4.5104e-20 v k 3.1962e-10 0.00080256 0.0005028 0.00064648 v omega 10.514 1.0313e+05 2663.3 495.86 v TempK 288 342.19 294.64 291.53 v Density 1.205 1.205 1.205 1.205 v TurbVisc 3.744e-15 9.1989e-05 5.2386e-05 6.8894e-05 v CourantNb 3.4415e-09 0.00017996 1.3932e-05 9.3989e-06 v FourierNb 0.078272 0.6281 0.17829 0.14877 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9653 4.9653 0.00059487 -6.1873e-07 v volume_forces[Z] -4.9653 4.9653 -0.0005948 7.2888e-07 v ǁvolume_forcesǁ 2.7112e-08 4.9663 0.60078 0.31562 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.85 291.67 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014242 5.0383e-05 2.803e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.07828 0.6281 0.17831 0.14878 INSTANT 0.102463200E+01 TIME STEP NUMBER 1064 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10172E-04 0.21403E-02 Friction velocity uk : 0.10172E-04 0.21403E-02 Dimensionless distance yplus : 0.67737E-04 0.14240E-01 Friction thermal sca. tstar : -0.22252E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.47574E-04 0.10001E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10172E-04 0.21403E-02 Friction velocity uk : 0.10172E-04 0.21403E-02 Dimensionless distance yplus : 0.67737E-04 0.14240E-01 Friction thermal sca. tstar : -0.22252E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.47574E-04 0.10001E-01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.40621E-08 3 0.66526E-07 0.10802E-12 0.63449E+00 c Velocity[X] 0.22817E-32 c Velocity[Y] 0.54001E-13 c Velocity[Z] 0.54018E-13 c Pressure 0.51714E-14 16 0.40085E-07 0.40085E-07 0.73427E+00 c k 0.23511E-06 2 0.22761E-07 0.51602E-09 0.10617E+01 c omega 0.13153E+02 1 0.56553E-09 0.65291E-01 0.13303E-02 c TempK 0.94856E+02 1 0.56069E-07 0.12366E-01 0.12286E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.0955e-14 6.8133e-14 -8.5063e-18 -2.2406e-18 v Velocity[Y] -0.00011719 0.00011041 6.7254e-11 -2.7485e-12 v Velocity[Z] -0.00011027 0.00011719 -3.483e-10 -1.2014e-12 v ǁVelocityǁ 7.3168e-10 0.00012554 1.2058e-05 9.4029e-06 v Pressure -0.0017838 0.02613 0.0015267 8.9228e-20 v k 3.1881e-10 0.00080182 0.00050226 0.00064581 v omega 10.505 1.0313e+05 2663.3 495.86 v TempK 288 342.19 294.65 291.53 v Density 1.205 1.205 1.205 1.205 v TurbVisc 3.7345e-15 9.1981e-05 5.2372e-05 6.8877e-05 v CourantNb 3.4425e-09 0.00017991 1.3932e-05 9.4014e-06 v FourierNb 0.078223 0.6281 0.17827 0.14874 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9654 4.9654 0.00059503 -6.1891e-07 v volume_forces[Z] -4.9654 4.9654 -0.00059497 7.2907e-07 v ǁvolume_forcesǁ 2.6781e-08 4.9663 0.60094 0.31576 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.85 291.67 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.01424 5.0373e-05 2.8024e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.078231 0.6281 0.17828 0.14875 INSTANT 0.102559500E+01 TIME STEP NUMBER 1065 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10099E-04 0.21399E-02 Friction velocity uk : 0.10099E-04 0.21399E-02 Dimensionless distance yplus : 0.67249E-04 0.14237E-01 Friction thermal sca. tstar : -0.22680E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.47232E-04 0.99990E-02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10099E-04 0.21399E-02 Friction velocity uk : 0.10099E-04 0.21399E-02 Dimensionless distance yplus : 0.67249E-04 0.14237E-01 Friction thermal sca. tstar : -0.22680E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.47232E-04 0.99990E-02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.40633E-08 3 0.66411E-07 0.10771E-12 0.63350E+00 c Velocity[X] 0.22751E-32 c Velocity[Y] 0.53845E-13 c Velocity[Z] 0.53862E-13 c Pressure 0.51643E-14 16 0.40029E-07 0.40029E-07 0.73355E+00 c k 0.23487E-06 2 0.22732E-07 0.51416E-09 0.10608E+01 c omega 0.13153E+02 1 0.56434E-09 0.65069E-01 0.13280E-02 c TempK 0.94857E+02 1 0.55994E-07 0.12348E-01 0.12277E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.092e-14 6.8106e-14 -8.503e-18 -2.2399e-18 v Velocity[Y] -0.00011716 0.00011039 6.9594e-11 -2.7467e-12 v Velocity[Z] -0.00011025 0.00011717 -3.5053e-10 -1.2005e-12 v ǁVelocityǁ 7.2251e-10 0.00012551 1.2061e-05 9.4072e-06 v Pressure -0.0017855 0.026142 0.0015275 -1.2845e-20 v k 3.18e-10 0.00080109 0.00050172 0.00064513 v omega 10.497 1.0313e+05 2663.3 495.85 v TempK 288 342.19 294.65 291.53 v Density 1.205 1.205 1.205 1.205 v TurbVisc 3.725e-15 9.1972e-05 5.2359e-05 6.8861e-05 v CourantNb 3.4436e-09 0.00017987 1.3932e-05 9.4039e-06 v FourierNb 0.078175 0.6281 0.17824 0.14871 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9654 4.9654 0.0005952 -6.1909e-07 v volume_forces[Z] -4.9654 4.9654 -0.00059513 7.2926e-07 v ǁvolume_forcesǁ 2.645e-08 4.9663 0.60111 0.31591 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.85 291.67 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014237 5.0363e-05 2.8019e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.078183 0.6281 0.17826 0.14872 INSTANT 0.102655800E+01 TIME STEP NUMBER 1066 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10025E-04 0.21395E-02 Friction velocity uk : 0.10025E-04 0.21395E-02 Dimensionless distance yplus : 0.66757E-04 0.14234E-01 Friction thermal sca. tstar : -0.23133E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.46886E-04 0.99971E-02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10025E-04 0.21395E-02 Friction velocity uk : 0.10025E-04 0.21395E-02 Dimensionless distance yplus : 0.66757E-04 0.14234E-01 Friction thermal sca. tstar : -0.23133E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.46886E-04 0.99971E-02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.40644E-08 3 0.66295E-07 0.10740E-12 0.63250E+00 c Velocity[X] 0.22686E-32 c Velocity[Y] 0.53689E-13 c Velocity[Z] 0.53706E-13 c Pressure 0.51572E-14 16 0.39974E-07 0.39974E-07 0.73282E+00 c k 0.23463E-06 2 0.22702E-07 0.51230E-09 0.10600E+01 c omega 0.13153E+02 1 0.56316E-09 0.64847E-01 0.13257E-02 c TempK 0.94857E+02 1 0.55919E-07 0.12331E-01 0.12268E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.0885e-14 6.8078e-14 -8.4997e-18 -2.2391e-18 v Velocity[Y] -0.00011714 0.00011037 7.1932e-11 -2.7449e-12 v Velocity[Z] -0.00011023 0.00011714 -3.5275e-10 -1.1996e-12 v ǁVelocityǁ 7.1336e-10 0.00012549 1.2063e-05 9.4114e-06 v Pressure -0.0017871 0.026154 0.0015283 5.9224e-20 v k 3.172e-10 0.00080036 0.00050119 0.00064446 v omega 10.488 1.0313e+05 2663.3 495.84 v TempK 288 342.19 294.65 291.53 v Density 1.205 1.205 1.205 1.205 v TurbVisc 3.7156e-15 9.1964e-05 5.2345e-05 6.8844e-05 v CourantNb 3.4446e-09 0.00017982 1.3933e-05 9.4064e-06 v FourierNb 0.078126 0.6281 0.17822 0.14869 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9654 4.9654 0.00059536 -6.1927e-07 v volume_forces[Z] -4.9654 4.9654 -0.00059529 7.2945e-07 v ǁvolume_forcesǁ 2.6119e-08 4.9663 0.60127 0.31606 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.85 291.67 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014234 5.0353e-05 2.8013e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.078135 0.6281 0.17823 0.1487 Options set or changed by "control_file": ------------------------- max_time_step 1067 (current: 1067) Finished reading "control_file". INSTANT 0.102752100E+01 TIME STEP NUMBER 1067 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.99507E-05 0.21391E-02 Friction velocity uk : 0.99507E-05 0.21391E-02 Dimensionless distance yplus : 0.66261E-04 0.14231E-01 Friction thermal sca. tstar : -0.23614E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.46537E-04 0.99953E-02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 1584 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 158400 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.99507E-05 0.21391E-02 Friction velocity uk : 0.99507E-05 0.21391E-02 Dimensionless distance yplus : 0.66261E-04 0.14231E-01 Friction thermal sca. tstar : -0.23614E+04 0.00000E+00 Dim-less thermal sca. tplus : 0.46537E-04 0.99953E-02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1584 Total number of wall faces : 1584 ------------------------------------------------------------ Write final restart files checkpoint at iteration 1067, Physical time 0.10275E+01 ** Writing the main restart file ----------------------------- Start writing Wrote field names and types to checkpoint at iteration 1067: checkpoint/main.csc End writing the options Wrote main variables to checkpoint: checkpoint/main.csc End writing ** Writing the auxiliary restart file ---------------------------------- Start writing End writing the dimensions and options End writing the physical properties End writing the time step Wrote boundary condition coefficients to checkpoint: checkpoint/auxiliary.csc End writing ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.40656E-08 3 0.66182E-07 0.10708E-12 0.63151E+00 c Velocity[X] 0.22620E-32 c Velocity[Y] 0.53533E-13 c Velocity[Z] 0.53550E-13 c Pressure 0.51502E-14 16 0.39919E-07 0.39919E-07 0.73210E+00 c k 0.23440E-06 2 0.22672E-07 0.51046E-09 0.10591E+01 c omega 0.13153E+02 1 0.56198E-09 0.64626E-01 0.13235E-02 c TempK 0.94858E+02 1 0.55845E-07 0.12314E-01 0.12259E-01 c Wall distance 0.25964E-06 22 0.39335E-03 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a k a omega a TempK ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.085e-14 6.805e-14 -8.4964e-18 -2.2383e-18 v Velocity[Y] -0.00011711 0.00011034 7.4268e-11 -2.743e-12 v Velocity[Z] -0.00011021 0.00011712 -3.5496e-10 -1.1989e-12 v ǁVelocityǁ 7.042e-10 0.00012546 1.2066e-05 9.4157e-06 v Pressure -0.0017887 0.026165 0.0015291 -1.1766e-21 v k 3.164e-10 0.00079963 0.00050065 0.00064379 v omega 10.479 1.0313e+05 2663.3 495.83 v TempK 288 342.19 294.65 291.53 v Density 1.205 1.205 1.205 1.205 v TurbVisc 3.7062e-15 9.1955e-05 5.2331e-05 6.8828e-05 v CourantNb 3.4456e-09 0.00017977 1.3933e-05 9.4089e-06 v FourierNb 0.078078 0.6281 0.17819 0.14866 v total_pressure 1.0132e+05 1.0133e+05 1.0133e+05 1.0132e+05 v Beta 0 0 0 0 v Wall distance 9.9922e-05 0.05712 0.022384 0.028817 v volume_forces[X] 0 0 0 0 v volume_forces[Y] -4.9655 4.9655 0.00059553 -6.1945e-07 v volume_forces[Z] -4.9655 4.9655 -0.00059546 7.2964e-07 v ǁvolume_forcesǁ 2.5788e-08 4.9664 0.60143 0.3162 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 288 342.89 294.85 291.67 v Boundary Density 1.205 1.205 1.205 1.205 v Yplus 0 0.014231 5.0343e-05 2.8007e-05 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.078086 0.6281 0.17821 0.14867 =============================================================== FINAL STAGE OF THE CALCULATION ============================== =========================================================== =========================================================== END OF CALCULATION ================== =============================================================== Destroying structures and ending computation