command: ./cs_solver --mpi *************************************************************** (R) Code_Saturne Version 6.0.4 Copyright (C) 1998-2019 EDF S.A., France revision 6.0.4-4743b4795 build vie 02 oct 2020 22:39:59 -03 MPI version 3.1 (Open MPI 2.1.1) The Code_Saturne CFD tool is free software; you can redistribute it and/or modify it under the terms of the GNU General Public License as published by the Free Software Foundation; either version 2 of the License, or (at your option) any later version. The Code_Saturne CFD tool is distributed in the hope that it will be useful, but WITHOUT ANY WARRANTY; without even the implied warranty of MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU General Public License for more details. *************************************************************** Local case configuration: Date: vie 02 oct 2020 23:25:04 -03 System: Linux 4.13.0-38-generic (Ubuntu 17.10) Machine: valkyrie Processor: model name : Intel(R) Core(TM) i7-8550U CPU @ 1.80GHz Memory: 15781 MB User: lgarelli (lgarelli) Directory: /home/lgarelli/RUNS_local/Code_Saturne/Internal_coup_Gustavo/Interncal_coupling_example/RESU/LES_dyn_restart_KW2 MPI ranks: 2 (appnum attribute: 0) OpenMP threads: 1 Processors/node: 4 I/O read method: collective MPI-IO (explicit offsets) I/O write method: collective MPI-IO (explicit offsets) I/O rank step: 1 External libraries for partitioning: METIS Reading metadata from file: "restart/mesh_input" =============================================================== CALCULATION PREPARATION ======================= =========================================================== @ @@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@ @ @ @@ WARNING : WHEN READING INPUT DATA @ ========= @ NON-STANDARD CHOICE WITH TIME-SCHEME @ @ ORDER 2 IN TIME or LES @ THE VALUE RECOMMENDED FOR THE PARAMETER NSWRSM FOR @ VARIABLE Pressure IS 10 @ NSWRSM IS NOW IMPOSED AS 5 @ @ computation will go on @ @ Check the input data given through the User Interface @ or in cs_user_parameters.f90. @ @ @@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@ @ @ @@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@ @ @ @@ WARNING : WHEN READING INPUT DATA @ ========= @ CHOICE OF TIME-SCHEME @ @ TIME-SCHEME FOR VELOCITY IS SECOND ORDER @ (THETAV = 0.50E+00) @ SOME TERMS ARE HOWEVER FIRST ORDER IN TIME WITH @ THE FOLLOWING SETTINGS: @ @ parameters ISTMPF ISNO2T ISTO2T IROEXT IVIEXT ICPEXT @ Values entered 2 1 0 0 0 0 @ @ computation will go on. @ @ Check the input data given through the User Interface @ or in cs_user_parameters.f90. @ @ @@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@ @ No error detected during the data verification cs_user_parameters.f90 and others). =========================================================== CALCULATION PARAMETERS SUMMARY ============================== ----------------------------------------------------------- ** DIMENSIONS ---------- --- Physics NVAR = 5 (Nb variables ) NSCAL = 1 (Nb scalars ) NSCAUS = 0 (Nb user scalars ) NSCAPP = 1 (Nb specific physics scalars ) ----------------------------------------------------------- ** HOMOGENEOUS MIXTURE MODEL VoF ---------------------------------------- IVOFMT = 0 ( 0 : disabled ) ( > 0: enabled ) ----------------------------------------------------------- ** TIME STEPPING ------------- --- Per-variable properties ------------------------------------ Variable ISTAT CDTVAR ------------------------------------ Velocity 1 0.1000E+01 Pressure 0 0.1000E+01 TempC 1 0.1000E+01 ---------------------------- ISTAT = 0 ou 1 (1 for unsteady ) CDTVAR > 0 (time step multiplier ) --- Order of base time stepping scheme ISCHTP = 2 (1: order 1; 2: order 2 ) ----------------------------------------------------------- ** STOKES ------ -- Continuous phase: ISTMPF = 2 (time scheme for flow (0: explicit (THETFL = 0 ) (1: std scheme (Saturne 1.0 ) (2: 2nd-order (THETFL = 0.5 ) THETFL = 0.50000E+00 (theta for mass flow ) THETVI = 0.00000E+00 (theta for total viscosity ((1+theta).new-theta.old THETCP = 0.00000E+00 (specific heat theta-scheme ((1+theta).new-theta.old THETSN = 0.50000E+00 (Nav-Stokes S.T. theta scheme) ((1+theta).new-theta.old THETST = 0.00000E+00 (Turbulence S.T. theta-scheme) ((1+theta).new-theta.old EPSUP = 0.10000E-04 (Velocity/pressure coupling stop test ) ----------------------------------------------------------- ** SCALARS ------- ITBRRB = 0 (T or H reconstruction at bdy) ------------------------------------------------------------- Variable Number ISCACP ITURT VISLS0 SIGMAS ------------------------------------------------------------- TempC 1 1 0 0.2000E+00 0.1000E+01 ------------------------------------------------------------- ------------------------------------ Variable Number RVARFL ------------------------------------ TempC 1 0.8000E+00 ------------------------------------------- ------------------------------------------------------- Variable Number ICLVFL SCAMIN SCAMAX ------------------------------------------------------- TempC 1 -1 -0.2731E+03 0.1000E+13 ------------------------------------------------------- ------------------------------------------------------------- For each scalar, the number indicates it's rank in the list of all scalars. User scalars are placed first, from 1 to NSCAUS. Specific physics scalars are placed at the end, from NSCAUS+1 to NSCAPP+NSCAUS=NSCAL. ISCACP = 0 or 1 2 (use Cp or not ) VISLS0 = >0 (Reference viscosity ) SIGMAS = >0 (Schmidt ) RVARFL = >0 (Rf, cf variance dissipation ) ICLVFL = 0, 1 or 2 (Variance clipping mode ) SCAMIN = (Min authorized value ) SCAMAX = (Max authorized value ) For variances, SCAMIN is ignored and SCAMAX is used only if ICLVFL = 2 ------------------------------------------------------ Scalar THETSS THETVS ------------------------------------------------------ 1 0.5000E+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 = 1 (1: restarted calculation ) ILEAUX = 1 (1: read restart/auxiliary ) IECAUX = 1 (1: write checkpoint/auxiliary) --- Calculation time The numbering of time steps and the measure of simulated physical time are absolute values, and not values relative to the current calculation. NTPABS = 500 (Initial time step) NTMABS = 600 (Final time step required) ----------------------------------------------------------- ** INPUT-OUTPUT ------------ --- Restart file NTSUIT = 0 (Checkpoint frequency ) --- Probe history files NTHIST = 1 (Output frequency ) FRHIST = -.10000E+01 (Output frequency (s) ) -- -- -- --- run_solver.log files NTLIST = 1 (Output frequency ) -- -- -- --- Additional post-processing variables (ipstdv) ipstfo = 7 (Force exerted by the fluid on the boundary) ipstyp = 1 (y+ at boundary) ipsttp = 1 (T+ at boundary) ipstft = 1 (Thermal flux at boundary) ipstnu = 1 (Dimensionless thermal flux at boundary) ----------------------------------------------------------- ** ALE METHOD (MOVING MESH) ----------- IALE = 0 (1: activated,2: CDO ) NALINF = 0 (Fluid initialization iterations) IFLXMW = 0 (ALE mass flux computation 0: thanks to vertices 1: thanks to mesh velocity) ----------------------------------------------------------- Postprocessing output writers: ------------------------------ -1: name: results directory: postprocessing format: MED 3.2.1 options: time dependency: fixed mesh output: every 50 time steps -5: name: directory: monitoring format: time_plot options: time dependency: fixed mesh output: every 1 time steps -6: name: directory: profiles format: plot options: time dependency: fixed mesh output: at calculation end -7: name: histograms directory: histograms format: histogram options: txt time dependency: fixed mesh output: at calculation end Reading file: restart/mesh_input Finished reading: restart/mesh_input No "partition_input/domain_number_2" file available; ---------------------------------------------------------- Partitioning by space-filling curve: Morton (in bounding box). Number of cells per domain (histogramm): [ 5000 ; 5000 ] = 2 Partitioning finished (0.0573 s) ---------------------------------------------------------- Halo construction with extended neighborhood ============================================ Face interfaces creation Vertex interfaces creation Halo creation Halo definition Local halo definition Distant halo creation Updating the faces -> cells connectivity Extended neighborhood structures definition Histogram of the number of cells per rank: minimum value = 5000 maximum value = 5000 1 : [ 5000 ; 5000 ] = 2 ---------------------------------------------------------- Histogram of the number of standard + halo cells per rank: minimum value = 5100 maximum value = 5100 1 : [ 5100 ; 5100 ] = 2 ---------------------------------------------------------- Histogram of the number of ghost cells per rank: minimum value = 100 maximum value = 100 1 : [ 100 ; 100 ] = 2 Histogram of the number of ghost cells in the standard neighborhood per rank: minimum value = 100 maximum value = 100 1 : [ 100 ; 100 ] = 2 ---------------------------------------------------------- Histogram of the number of interior faces per rank: minimum value = 9850 maximum value = 9850 1 : [ 9850 ; 9850 ] = 2 ---------------------------------------------------------- Histogram of the number of boundary faces per rank: minimum value = 10400 maximum value = 10400 1 : [ 10400 ; 10400 ] = 2 ---------------------------------------------------------- Histogram of the number of interior faces per cell: minimum value = 2 maximum value = 4 1 : [ 2 ; 3 [ = 12 2 : [ 3 ; 4 ] = 9988 ---------------------------------------------------------- Histogram of the number of neighboring domains per rank: minimum value = 1 maximum value = 1 1 : [ 1 ; 1 ] = 2 ---------------------------------------------------------- Global definition of the number of elements (cells, vertices, faces...) Synchronizing cell families Renumbering mesh: renumbering for cells: pre-numbering: no renumbering cells adjacent to ghost cells last: no numbering: no renumbering renumbering for interior faces: cell adjacency pre-ordering: lowest id first faces adjacent to ghost cells last: no numbering: multipass renumbering for boundary faces: numbering: no shared cell across threads renumbering for vertices: numbering: no renumbering Numbering for cells: type: default Numbering for interior faces: type: default Numbering for boundary faces: type: default ---------------------------------------------------------- Histogram of volume mesh matrix bandwidth per rank: minimum value = 4951 maximum value = 5000 1 : [ 4951 ; 4960 [ = 1 2 : [ 4960 ; 4970 [ = 0 3 : [ 4970 ; 4980 [ = 0 4 : [ 4980 ; 4990 [ = 0 5 : [ 4990 ; 5000 ] = 1 Histogram of volume mesh matrix profile/lines per rank: minimum value = 99 maximum value = 100 1 : [ 99 ; 100 ] = 2 Mesh coordinates: minimum and maximum X : 0.0000000e+00 1.0000000e+00 Y : 0.0000000e+00 1.0000000e+00 Z : 0.0000000e+00 1.0000000e-02 Mesh Number of cells: 10000 Number of interior faces: 19600 Number of boundary faces: 20800 Number of vertices: 20806 Groups: "auto:internal_coupling_0" boundary faces: 400 --- Information on the volumes Minimum control volume = 1.0000000e-06 Maximum control volume = 1.0000000e-06 Total volume for the domain = 1.0000000e-02 Criterion 1: Orthogonality: Number of bad cells detected: 0 --> 0 % Criterion 2: Offset: Number of bad cells detected: 0 --> 0 % Criterion 3: Least-Squares Gradient Quality: Number of bad cells detected: 0 --> 0 % Criterion 4: Cells Volume Ratio: Number of bad cells detected: 0 --> 0 % Criterion 5: Guilt by Association: Number of bad cells detected: 0 --> 0 % Computing geometric quantities (0.00597 s) --- Information on volume zones Volume zone "cells" id = 0 Number of cells = 10000 Volume = 1.0000000e-02 Surface = -1 (not computed) Volume zone "all_cells" id = 1 Number of cells = 10000 Volume = 1.0000000e-02 Surface = -1 (not computed) --- Information on boundary zones Boundary zone "boundary_faces" id = 0 Number of faces = 20800 Surface = 2.0800000e+00 Perimeter = -1 (not computed) Boundary zone "BC_1" id = 1 Number of faces = 20800 Surface = 2.0800000e+00 Perimeter = -1 (not computed) Internal coupling coupling_id = 0 Coupled scalar: temperature Cell group selection criterion: x<0.25001 or x>0.74999 Face group selection criterion: auto:internal_coupling_0 Locator: n dist points (total coupled boundary faces) = 400 ALMAX = 0.21544E+00 (Characteristic length ) ALMAX is the cubic root of the domain volume. ------------------------------------------------------------- ----------------------------------------------------------- ** READING MAIN AND AUXILIARY RESTART FILES ---------------------------------------- READING THE MAIN RESTART FILE Start reading Warning: the number of variables or properties has been changed relative to the restart file. current: 3 model and 0 user variables 17 model and 0 user properties previous: 6 model and 0 user variables 16 model and 0 user properties The computation continues, with a partial restart. Reading dimensions complete Reading the previous time step number (restarting computation) NTPABS = 500 Reading the previous time step number (restarting computation) TTPABS = 0.5000E+02 Reading options complete Warning: the turbulence model has been changed relative to the restart file. current model: 41 previous model: 60 The computation continues, with a partial an/or adapted restart. Read variables from restart: restart/main Reading complete READING THE AUXILIARY RESTART FILE Start reading Fin de la lecture des options restart/auxiliary: section "ref_presstot01" not present. @ @@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@ @ @ @@ WARNING: WHEN READING THE AUXILIARY RESTART FILE @ ======= @ Lecture des proprietes physiques @ @ It was not possible to read some values from the @ auxiliary restart file. @ They will be initialized by the default values. @ @ This situation can occur when the restart file @ originates from a run realised with different @ options or when the file is damaged. @ @ The run will continue... @ @@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@ @ Fin de la lecture des proprietes physiques Fin de la lecture du pas de temps restart/auxiliary: section "inner_mass_flux::vals::1" not present. restart/auxiliary: section "boundary_mass_flux::vals::1" not present. Fin de la lecture des flux de masse Fin de la lecture des conditions aux limites restart/auxiliary: section "velocity_prev_st::vals::0" not present. restart/auxiliary: section "temperature_prev_st::vals::0" not present. restart/auxiliary: section "time_moments:sizes" not present. End reading ----------------------------------------------------------- ----------------------------------------------------------- ** VARIABLES INITIALIZATION ------------------------ ----------------------------------------- Variable Min. value Max. value ----------------------------------------- Velocity -0.1945E-01 0.3210E-01 Velocity -0.4059E-01 0.1045E+00 Velocity -0.8839E-04 0.8811E-04 Pressure -0.1033E-01 0.3577E-01 TempC 0.1189E-05 0.9901E+01 --------------------------------- dt 0.1000E+00 0.1000E+00 --------------------------------- ------------------------------------------------------------- ** INFORMATION ON BOUNDARY FACES TYPE ---------------------------------- ------------------------------------------------------------------------- Boundary type Code Nb faces ------------------------------------------------------------------------- Inlet 2 0 Smooth wall 5 20800 Rough wall 6 0 Symmetry 4 0 Free outlet 3 0 Free inlet 14 0 Convective inlet 16 0 Free surface 15 0 Undefined 1 0 ------------------------------------------------------------------------- =============================================================== MAIN CALCULATION ================ =============================================================== =============================================================== INSTANT 0.501000000E+02 TIME STEP NUMBER 501 ============================================================= ----------------------------------------- Property Min. value Max. value ----------------------------------------- density 0.9801E+00 0.1000E+01 molecular_viscos 0.1830E-04 0.1830E-04 turbulent_viscos 0.0000E+00 0.1180E-04 specific_heat 0.1017E+04 0.1017E+04 ----------------------------------------- --- Diffusivity: ----------------------------------------------- Scalar Number Min. value Max. value ----------------------------------------------- TempC 1 0.2000E+00 0.1000E+01 ----------------------------------------------- ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 20800 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00 Friction velocity uet : 0.21992E-04 0.19668E-01 Friction velocity uk : 0.21992E-04 0.19668E-01 Dimensionless distance yplus : 0.60088E-02 0.53129E+01 Friction thermal sca. tstar : -0.40690E+03 0.36748E+03 Rough dim-less th. sca. tplus : 0.11185E-03 0.49449E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 20800 Total number of wall faces : 20800 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.16840E-04 3 0.38154E-04 0.33457E-07 0.35499E-01 c Velocity[X] 0.28395E-08 c Velocity[Y] 0.30478E-07 c Velocity[Z] 0.13905E-09 c Pressure 0.34320E-06 8 0.85819E-05 0.34709E-01 0.45257E-02 c TempC 0.43518E+01 2 0.73505E-05 0.11373E-03 0.85824E-02 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a TempC ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.019636 0.032118 1.5701e-05 1.5701e-05 v Velocity[Y] -0.040599 0.10448 0.00011775 0.00011775 v Velocity[Z] -7.5437e-05 7.6632e-05 -2.9582e-07 -2.9582e-07 v ǁVelocityǁ 1.2957e-06 0.10448 0.0077534 0.0077534 v Pressure -0.010322 0.035742 8.4821e-18 -1.1435e-18 v TempC 1.2548e-06 9.9016 2.4405 2.4405 v Density 0.98011 1 0.99802 0.99802 v TurbVisc 0 1.1796e-05 9.791e-08 9.791e-08 v CourantNb 0 1.0485 0.08808 0.08808 v FourierNb 0.036603 0.090692 0.072228 0.072228 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Csdyn2 0 0.004225 0.0028651 0.0028651 v SpecHeat 1017.2 1017.2 1017.2 1017.2 v ThermalCond 0.2 1 0.6 0.6 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 1.1892e-06 10 2.4693 2.4693 v Boundary Density 0.98011 1 0.99799 0.99799 v Yplus 0.0060088 5.3129 0.98501 0.98501 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.036603 1.1225 0.16031 0.16031 INSTANT 0.502000000E+02 TIME STEP NUMBER 502 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 20800 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00 Friction velocity uet : 0.24062E-04 0.19666E-01 Friction velocity uk : 0.24062E-04 0.19666E-01 Dimensionless distance yplus : 0.65744E-02 0.53125E+01 Friction thermal sca. tstar : -0.42110E+03 0.41258E+03 Rough dim-less th. sca. tplus : 0.12238E-03 0.49446E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 20800 Total number of wall faces : 20800 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.16835E-04 3 0.32112E-04 0.23412E-07 0.29706E-01 c Velocity[X] 0.16333E-08 c Velocity[Y] 0.21677E-07 c Velocity[Z] 0.10219E-09 c Pressure 0.19226E-06 8 0.70253E-05 0.19426E-01 0.32470E-01 c TempC 0.43532E+01 2 0.70179E-05 0.11286E-03 0.85463E-02 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a TempC ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.019742 0.032138 1.5674e-05 1.5674e-05 v Velocity[Y] -0.040613 0.10445 0.00011836 0.00011836 v Velocity[Z] -6.4512e-05 6.6736e-05 -2.7443e-07 -2.7443e-07 v ǁVelocityǁ 8.5521e-07 0.10445 0.0077478 0.0077478 v Pressure -0.010339 0.035803 8.8818e-18 -8.0468e-19 v TempC 1.3275e-06 9.9017 2.4428 2.4428 v Density 0.98009 1 0.99801 0.99801 v TurbVisc 0 1.1784e-05 9.4728e-08 9.4728e-08 v CourantNb 1.6644e-06 1.0483 0.088101 0.088101 v FourierNb 0.036603 0.090683 0.072217 0.072217 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Csdyn2 0 0.004225 0.0028225 0.0028225 v SpecHeat 1017.2 1017.2 1017.2 1017.2 v ThermalCond 0.2 1 0.6 0.6 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 1.2548e-06 10 2.4715 2.4715 v Boundary Density 0.98009 1 0.99798 0.99798 v Yplus 0.0065744 5.3125 0.97907 0.97907 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.036613 1.1224 0.16032 0.16032 INSTANT 0.503000000E+02 TIME STEP NUMBER 503 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 20800 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00 Friction velocity uet : 0.26670E-04 0.19664E-01 Friction velocity uk : 0.26670E-04 0.19664E-01 Dimensionless distance yplus : 0.72868E-02 0.53117E+01 Friction thermal sca. tstar : -0.47376E+03 0.42216E+03 Rough dim-less th. sca. tplus : 0.13564E-03 0.49438E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 20800 Total number of wall faces : 20800 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.16830E-04 3 0.27419E-04 0.17437E-07 0.25645E-01 c Velocity[X] 0.12438E-08 c Velocity[Y] 0.16118E-07 c Velocity[Z] 0.75499E-10 c Pressure 0.12246E-06 7 0.72194E-05 0.12359E-01 0.33465E-01 c TempC 0.43546E+01 2 0.65752E-05 0.11243E-03 0.85264E-02 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a TempC ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.019799 0.032159 1.5672e-05 1.5672e-05 v Velocity[Y] -0.040623 0.10441 0.00011891 0.00011891 v Velocity[Z] -5.5278e-05 5.8197e-05 -2.5457e-07 -2.5457e-07 v ǁVelocityǁ 3.6624e-07 0.10441 0.0077424 0.0077424 v Pressure -0.01036 0.035871 -7.1054e-19 -1.0546e-17 v TempC 1.399e-06 9.9018 2.4451 2.4451 v Density 0.98008 1 0.99801 0.99801 v TurbVisc 0 1.1775e-05 9.357e-08 9.357e-08 v CourantNb 3.0683e-06 1.0481 0.088025 0.088025 v FourierNb 0.036602 0.090676 0.072213 0.072213 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Csdyn2 0 0.004225 0.0028178 0.0028178 v SpecHeat 1017.2 1017.2 1017.2 1017.2 v ThermalCond 0.2 1 0.6 0.6 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 1.3275e-06 10 2.4738 2.4738 v Boundary Density 0.98008 1 0.99798 0.99798 v Yplus 0.0072868 5.3117 0.97549 0.97549 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.036613 1.1221 0.16024 0.16024 INSTANT 0.504000000E+02 TIME STEP NUMBER 504 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 20800 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00 Friction velocity uet : 0.28479E-04 0.19660E-01 Friction velocity uk : 0.28479E-04 0.19660E-01 Dimensionless distance yplus : 0.77811E-02 0.53107E+01 Friction thermal sca. tstar : -0.75520E+03 0.51090E+03 Rough dim-less th. sca. tplus : 0.14484E-03 0.49428E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 20800 Total number of wall faces : 20800 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.16824E-04 3 0.24002E-04 0.13414E-07 0.22501E-01 c Velocity[X] 0.10214E-08 c Velocity[Y] 0.12336E-07 c Velocity[Z] 0.56074E-10 c Pressure 0.89974E-07 7 0.68785E-05 0.90696E-02 0.33461E-01 c TempC 0.43560E+01 2 0.69375E-05 0.11204E-03 0.85085E-02 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a TempC ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.019829 0.032179 1.568e-05 1.568e-05 v Velocity[Y] -0.04063 0.10436 0.0001194 0.0001194 v Velocity[Z] -4.7462e-05 5.0818e-05 -2.3613e-07 -2.3613e-07 v ǁVelocityǁ 4.792e-07 0.10436 0.0077372 0.0077372 v Pressure -0.010385 0.035941 1.1191e-17 1.6941e-18 v TempC 1.4784e-06 9.902 2.4473 2.4473 v Density 0.98006 1 0.998 0.998 v TurbVisc 0 1.177e-05 9.2942e-08 9.2942e-08 v CourantNb 3.4421e-06 1.0477 0.087952 0.087952 v FourierNb 0.036602 0.090664 0.072211 0.072211 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Csdyn2 0 0.004225 0.0028167 0.0028167 v SpecHeat 1017.2 1017.2 1017.2 1017.2 v ThermalCond 0.2 1 0.6 0.6 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 1.399e-06 10 2.476 2.476 v Boundary Density 0.98006 1 0.99797 0.99797 v Yplus 0.0077811 5.3107 0.97256 0.97256 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.036612 1.1218 0.16016 0.16016 INSTANT 0.505000000E+02 TIME STEP NUMBER 505 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 20800 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00 Friction velocity uet : 0.11975E-04 0.19655E-01 Friction velocity uk : 0.11975E-04 0.19655E-01 Dimensionless distance yplus : 0.32718E-02 0.53094E+01 Friction thermal sca. tstar : -0.58917E+03 0.47541E+03 Rough dim-less th. sca. tplus : 0.60903E-04 0.49417E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 20800 Total number of wall faces : 20800 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.16817E-04 3 0.21327E-04 0.10599E-07 0.20009E-01 c Velocity[X] 0.88271E-09 c Velocity[Y] 0.96741E-08 c Velocity[Z] 0.41864E-10 c Pressure 0.70772E-07 7 0.66839E-05 0.71257E-02 0.33387E-01 c TempC 0.43574E+01 2 0.68631E-05 0.11168E-03 0.84915E-02 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a TempC ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.019843 0.032193 1.5693e-05 1.5693e-05 v Velocity[Y] -0.040635 0.10431 0.00011983 0.00011983 v Velocity[Z] -4.1561e-05 4.4432e-05 -2.1901e-07 -2.1901e-07 v ǁVelocityǁ 8.7109e-07 0.10431 0.0077321 0.0077321 v Pressure -0.010412 0.036011 1.3101e-17 3.7269e-18 v TempC 1.5578e-06 9.9021 2.4496 2.4496 v Density 0.98005 1 0.998 0.998 v TurbVisc 0 1.1767e-05 9.2514e-08 9.2514e-08 v CourantNb 2.4256e-06 1.0472 0.08788 0.08788 v FourierNb 0.036602 0.090652 0.07221 0.07221 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Csdyn2 0 0.004225 0.0028169 0.0028169 v SpecHeat 1017.2 1017.2 1017.2 1017.2 v ThermalCond 0.2 1 0.6 0.6 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 1.4784e-06 10 2.4783 2.4783 v Boundary Density 0.98005 1 0.99797 0.99797 v Yplus 0.0032718 5.3094 0.97003 0.97003 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.036611 1.1213 0.16009 0.16009 INSTANT 0.506000000E+02 TIME STEP NUMBER 506 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 20800 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00 Friction velocity uet : 0.14166E-04 0.19651E-01 Friction velocity uk : 0.14166E-04 0.19651E-01 Dimensionless distance yplus : 0.38704E-02 0.53081E+01 Friction thermal sca. tstar : -0.46202E+03 0.46694E+03 Rough dim-less th. sca. tplus : 0.72047E-04 0.49404E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 20800 Total number of wall faces : 20800 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.16811E-04 3 0.19087E-04 0.85820E-08 0.18012E-01 c Velocity[X] 0.79113E-09 c Velocity[Y] 0.77594E-08 c Velocity[Z] 0.31417E-10 c Pressure 0.57931E-07 7 0.65259E-05 0.58260E-02 0.33285E-01 c TempC 0.43587E+01 2 0.74137E-05 0.11131E-03 0.84744E-02 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a TempC ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.019846 0.0322 1.5707e-05 1.5707e-05 v Velocity[Y] -0.040639 0.10425 0.00012021 0.00012021 v Velocity[Z] -3.6515e-05 3.89e-05 -2.0311e-07 -2.0311e-07 v ǁVelocityǁ 6.3811e-07 0.10425 0.0077271 0.0077271 v Pressure -0.010441 0.036081 5.1958e-18 -4.4469e-18 v TempC 1.6459e-06 9.9022 2.4519 2.4519 v Density 0.98003 1 0.99799 0.99799 v TurbVisc 0 1.1766e-05 9.2211e-08 9.2211e-08 v CourantNb 2.735e-06 1.0466 0.08781 0.08781 v FourierNb 0.036601 0.09064 0.072209 0.072209 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Csdyn2 0 0.004225 0.0028174 0.0028174 v SpecHeat 1017.2 1017.2 1017.2 1017.2 v ThermalCond 0.2 1 0.6 0.6 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 1.5578e-06 10 2.4805 2.4805 v Boundary Density 0.98003 1 0.99796 0.99796 v Yplus 0.0038704 5.3081 0.96778 0.96778 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.03661 1.1207 0.16002 0.16002 INSTANT 0.507000000E+02 TIME STEP NUMBER 507 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 20800 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00 Friction velocity uet : 0.17508E-04 0.19646E-01 Friction velocity uk : 0.17508E-04 0.19646E-01 Dimensionless distance yplus : 0.47835E-02 0.53067E+01 Friction thermal sca. tstar : -0.56242E+03 0.48106E+03 Rough dim-less th. sca. tplus : 0.89045E-04 0.49391E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 20800 Total number of wall faces : 20800 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.16804E-04 3 0.17139E-04 0.71178E-08 0.16411E-01 c Velocity[X] 0.72857E-09 c Velocity[Y] 0.63656E-08 c Velocity[Z] 0.23697E-10 c Pressure 0.48697E-07 7 0.63830E-05 0.48917E-02 0.33183E-01 c TempC 0.43601E+01 2 0.75860E-05 0.11096E-03 0.84577E-02 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a TempC ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.01984 0.032197 1.5723e-05 1.5723e-05 v Velocity[Y] -0.040644 0.1042 0.00012054 0.00012054 v Velocity[Z] -3.1966e-05 3.4099e-05 -1.8836e-07 -1.8836e-07 v ǁVelocityǁ 4.2736e-07 0.1042 0.007722 0.007722 v Pressure -0.01047 0.036151 7.2387e-18 -2.2023e-18 v TempC 1.7334e-06 9.9024 2.4542 2.4542 v Density 0.98002 1 0.99799 0.99799 v TurbVisc 0 1.1765e-05 9.2043e-08 9.2043e-08 v CourantNb 7.7867e-07 1.046 0.087741 0.087741 v FourierNb 0.036601 0.090629 0.072209 0.072209 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Csdyn2 0 0.004225 0.002817 0.002817 v SpecHeat 1017.2 1017.2 1017.2 1017.2 v ThermalCond 0.2 1 0.6 0.6 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 1.6459e-06 10 2.4828 2.4828 v Boundary Density 0.98002 1 0.99795 0.99795 v Yplus 0.0047835 5.3067 0.96576 0.96576 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.036609 1.1201 0.15995 0.15995 INSTANT 0.508000000E+02 TIME STEP NUMBER 508 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 20800 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00 Friction velocity uet : 0.20828E-04 0.19641E-01 Friction velocity uk : 0.20828E-04 0.19641E-01 Dimensionless distance yplus : 0.56908E-02 0.53053E+01 Friction thermal sca. tstar : -0.70514E+03 0.50918E+03 Rough dim-less th. sca. tplus : 0.10593E-03 0.49379E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 20800 Total number of wall faces : 20800 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.16797E-04 2 0.88060E-04 0.57461E-08 0.14751E-01 c Velocity[X] 0.67007E-09 c Velocity[Y] 0.50603E-08 c Velocity[Z] 0.15745E-10 c Pressure 0.41309E-07 7 0.62150E-05 0.41446E-02 0.33082E-01 c TempC 0.43615E+01 2 0.84478E-05 0.11058E-03 0.84401E-02 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a TempC ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.019829 0.032185 1.5739e-05 1.5739e-05 v Velocity[Y] -0.040649 0.10415 0.00012083 0.00012083 v Velocity[Z] -2.8111e-05 2.9966e-05 -1.7467e-07 -1.7467e-07 v ǁVelocityǁ 2.6418e-07 0.10415 0.0077171 0.0077171 v Pressure -0.010499 0.03622 1.2568e-17 3.007e-18 v TempC 1.8313e-06 9.9025 2.4564 2.4564 v Density 0.98 1 0.99798 0.99798 v TurbVisc 0 1.1765e-05 9.1973e-08 9.1973e-08 v CourantNb 5.9008e-07 1.0456 0.087673 0.087673 v FourierNb 0.036601 0.09062 0.072209 0.072209 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Csdyn2 0 0.004225 0.0028184 0.0028184 v SpecHeat 1017.2 1017.2 1017.2 1017.2 v ThermalCond 0.2 1 0.6 0.6 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 1.7334e-06 10 2.485 2.485 v Boundary Density 0.98 1 0.99795 0.99795 v Yplus 0.0056908 5.3053 0.96391 0.96391 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.036607 1.1196 0.15988 0.15988 INSTANT 0.509000000E+02 TIME STEP NUMBER 509 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 20800 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00 Friction velocity uet : 0.15269E-04 0.19636E-01 Friction velocity uk : 0.15269E-04 0.19636E-01 Dimensionless distance yplus : 0.41718E-02 0.53039E+01 Friction thermal sca. tstar : -0.88245E+03 0.54566E+03 Rough dim-less th. sca. tplus : 0.77657E-04 0.49366E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 20800 Total number of wall faces : 20800 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.16789E-04 2 0.78057E-04 0.50672E-08 0.13859E-01 c Velocity[X] 0.64329E-09 c Velocity[Y] 0.44118E-08 c Velocity[Z] 0.12126E-10 c Pressure 0.36404E-07 7 0.60924E-05 0.36484E-02 0.32977E-01 c TempC 0.43628E+01 2 0.89646E-05 0.11020E-03 0.84225E-02 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a TempC ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.019814 0.032165 1.5755e-05 1.5755e-05 v Velocity[Y] -0.040656 0.10409 0.00012109 0.00012109 v Velocity[Z] -2.4995e-05 2.6363e-05 -1.6195e-07 -1.6195e-07 v ǁVelocityǁ 1.6323e-07 0.10409 0.0077121 0.0077121 v Pressure -0.010529 0.036289 1.3456e-17 3.7693e-18 v TempC 1.9275e-06 9.9026 2.4587 2.4587 v Density 0.97998 1 0.99798 0.99798 v TurbVisc 0 1.1765e-05 9.1929e-08 9.1929e-08 v CourantNb 1.2857e-06 1.0451 0.087605 0.087605 v FourierNb 0.036601 0.090612 0.072209 0.072209 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Csdyn2 0 0.004225 0.0028193 0.0028193 v SpecHeat 1017.2 1017.2 1017.2 1017.2 v ThermalCond 0.2 1 0.6 0.6 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 1.8313e-06 10 2.4873 2.4873 v Boundary Density 0.97998 1 0.99794 0.99794 v Yplus 0.0041718 5.3039 0.9622 0.9622 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.036606 1.1191 0.15981 0.15981 INSTANT 0.510000000E+02 TIME STEP NUMBER 510 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 20800 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00 Friction velocity uet : 0.12464E-04 0.19631E-01 Friction velocity uk : 0.12464E-04 0.19631E-01 Dimensionless distance yplus : 0.34054E-02 0.53025E+01 Friction thermal sca. tstar : -0.93758E+03 0.58977E+03 Rough dim-less th. sca. tplus : 0.63390E-04 0.49353E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 20800 Total number of wall faces : 20800 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.16782E-04 2 0.69225E-04 0.45561E-08 0.13147E-01 c Velocity[X] 0.62314E-09 c Velocity[Y] 0.39236E-08 c Velocity[Z] 0.93801E-11 c Pressure 0.32722E-07 7 0.59855E-05 0.32756E-02 0.32873E-01 c TempC 0.43642E+01 2 0.10025E-04 0.10980E-03 0.84040E-02 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a TempC ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.019796 0.032138 1.577e-05 1.577e-05 v Velocity[Y] -0.040664 0.10404 0.00012133 0.00012133 v Velocity[Z] -2.2244e-05 2.3957e-05 -1.5015e-07 -1.5015e-07 v ǁVelocityǁ 1.1603e-07 0.10404 0.0077071 0.0077071 v Pressure -0.010559 0.036358 1.1369e-17 1.7788e-18 v TempC 2.036e-06 9.9027 2.461 2.461 v Density 0.97997 1 0.99797 0.99797 v TurbVisc 0 1.1765e-05 9.1912e-08 9.1912e-08 v CourantNb 8.2457e-07 1.0446 0.087538 0.087538 v FourierNb 0.036601 0.090605 0.07221 0.07221 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Csdyn2 0 0.004225 0.0028203 0.0028203 v SpecHeat 1017.2 1017.2 1017.2 1017.2 v ThermalCond 0.2 1 0.6 0.6 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 1.9275e-06 10 2.4895 2.4895 v Boundary Density 0.97997 1 0.99794 0.99794 v Yplus 0.0034054 5.3025 0.96061 0.96061 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.036605 1.1186 0.15975 0.15975 INSTANT 0.511000000E+02 TIME STEP NUMBER 511 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 20800 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00 Friction velocity uet : 0.12590E-04 0.19626E-01 Friction velocity uk : 0.12590E-04 0.19626E-01 Dimensionless distance yplus : 0.34400E-02 0.53011E+01 Friction thermal sca. tstar : -0.83798E+03 0.63850E+03 Rough dim-less th. sca. tplus : 0.64034E-04 0.49340E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 20800 Total number of wall faces : 20800 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.16774E-04 2 0.61449E-04 0.41683E-08 0.12581E-01 c Velocity[X] 0.60761E-09 c Velocity[Y] 0.35534E-08 c Velocity[Z] 0.72876E-11 c Pressure 0.29940E-07 7 0.58901E-05 0.29937E-02 0.32769E-01 c TempC 0.43655E+01 3 0.12854E-05 0.10974E-03 0.83987E-02 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a TempC ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.019776 0.032106 1.5784e-05 1.5784e-05 v Velocity[Y] -0.040674 0.10398 0.00012154 0.00012154 v Velocity[Z] -1.9811e-05 2.1765e-05 -1.392e-07 -1.392e-07 v ǁVelocityǁ 1.2606e-07 0.10398 0.0077022 0.0077022 v Pressure -0.010589 0.036426 2.6645e-18 -6.8186e-18 v TempC 2.142e-06 9.9029 2.4632 2.4632 v Density 0.97995 1 0.99796 0.99796 v TurbVisc 0 1.1765e-05 9.1894e-08 9.1894e-08 v CourantNb 5.2776e-07 1.044 0.087472 0.087472 v FourierNb 0.036601 0.0906 0.07221 0.07221 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Csdyn2 0 0.004225 0.0028204 0.0028204 v SpecHeat 1017.2 1017.2 1017.2 1017.2 v ThermalCond 0.2 1 0.6 0.6 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 2.036e-06 10 2.4918 2.4918 v Boundary Density 0.97995 1 0.99793 0.99793 v Yplus 0.00344 5.3011 0.95914 0.95914 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.036605 1.1181 0.15968 0.15968 INSTANT 0.512000000E+02 TIME STEP NUMBER 512 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 20800 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00 Friction velocity uet : 0.49545E-05 0.19620E-01 Friction velocity uk : 0.49545E-05 0.19620E-01 Dimensionless distance yplus : 0.13537E-02 0.52997E+01 Friction thermal sca. tstar : -0.74557E+03 0.69276E+03 Rough dim-less th. sca. tplus : 0.25199E-04 0.49326E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 20800 Total number of wall faces : 20800 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.16766E-04 2 0.54576E-04 0.38713E-08 0.12130E-01 c Velocity[X] 0.59533E-09 c Velocity[Y] 0.32702E-08 c Velocity[Z] 0.56855E-11 c Pressure 0.27840E-07 7 0.58049E-05 0.27806E-02 0.32664E-01 c TempC 0.43669E+01 2 0.76397E-05 0.10930E-03 0.83786E-02 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a TempC ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.019755 0.032069 1.5798e-05 1.5798e-05 v Velocity[Y] -0.040685 0.10393 0.00012174 0.00012174 v Velocity[Z] -1.7658e-05 2.1385e-05 -1.2904e-07 -1.2904e-07 v ǁVelocityǁ 1.551e-07 0.10393 0.0076972 0.0076972 v Pressure -0.010618 0.036494 1.4966e-17 5.2093e-18 v TempC 2.2622e-06 9.903 2.4655 2.4655 v Density 0.97994 1 0.99796 0.99796 v TurbVisc 0 1.1766e-05 9.1903e-08 9.1903e-08 v CourantNb 8.4376e-07 1.0435 0.087406 0.087406 v FourierNb 0.036601 0.090596 0.07221 0.07221 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Csdyn2 0 0.004225 0.002821 0.002821 v SpecHeat 1017.2 1017.2 1017.2 1017.2 v ThermalCond 0.2 1 0.6 0.6 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 2.142e-06 10 2.494 2.494 v Boundary Density 0.97994 1 0.99793 0.99793 v Yplus 0.0013537 5.2997 0.95776 0.95776 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.036604 1.1175 0.15962 0.15962 INSTANT 0.513000000E+02 TIME STEP NUMBER 513 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 20800 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00 Friction velocity uet : 0.11877E-04 0.19615E-01 Friction velocity uk : 0.11877E-04 0.19615E-01 Dimensionless distance yplus : 0.32452E-02 0.52983E+01 Friction thermal sca. tstar : -0.81610E+03 0.75002E+03 Rough dim-less th. sca. tplus : 0.60408E-04 0.49313E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 20800 Total number of wall faces : 20800 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.16758E-04 2 0.48521E-04 0.36385E-08 0.11765E-01 c Velocity[X] 0.58507E-09 c Velocity[Y] 0.30490E-08 c Velocity[Z] 0.44534E-11 c Pressure 0.26163E-07 7 0.57425E-05 0.26101E-02 0.32582E-01 c TempC 0.43683E+01 2 0.84138E-05 0.10893E-03 0.83613E-02 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a TempC ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.019734 0.032029 1.5812e-05 1.5812e-05 v Velocity[Y] -0.040697 0.10387 0.00012191 0.00012191 v Velocity[Z] -1.5752e-05 1.9596e-05 -1.1961e-07 -1.1961e-07 v ǁVelocityǁ 1.2794e-07 0.10387 0.0076923 0.0076923 v Pressure -0.010648 0.036562 6.3505e-18 -3.6422e-18 v TempC 2.3807e-06 9.9031 2.4678 2.4678 v Density 0.97993 1 0.99795 0.99795 v TurbVisc 0 1.1767e-05 9.1925e-08 9.1925e-08 v CourantNb 1.3753e-06 1.0429 0.087341 0.087341 v FourierNb 0.036601 0.090593 0.072211 0.072211 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Csdyn2 0 0.004225 0.0028216 0.0028216 v SpecHeat 1017.2 1017.2 1017.2 1017.2 v ThermalCond 0.2 1 0.6 0.6 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 2.2622e-06 10 2.4963 2.4963 v Boundary Density 0.97993 1 0.99792 0.99792 v Yplus 0.0032452 5.2983 0.95646 0.95646 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.036603 1.117 0.15955 0.15955 INSTANT 0.514000000E+02 TIME STEP NUMBER 514 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 20800 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00 Friction velocity uet : 0.47150E-05 0.19610E-01 Friction velocity uk : 0.47150E-05 0.19610E-01 Dimensionless distance yplus : 0.12882E-02 0.52968E+01 Friction thermal sca. tstar : -0.85896E+03 0.81078E+03 Rough dim-less th. sca. tplus : 0.23980E-04 0.49300E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 20800 Total number of wall faces : 20800 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.16750E-04 2 0.43183E-04 0.34645E-08 0.11486E-01 c Velocity[X] 0.57725E-09 c Velocity[Y] 0.28838E-08 c Velocity[Z] 0.35016E-11 c Pressure 0.25013E-07 7 0.56528E-05 0.24926E-02 0.32481E-01 c TempC 0.43696E+01 2 0.75001E-05 0.10858E-03 0.83449E-02 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a TempC ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.019714 0.031987 1.5825e-05 1.5825e-05 v Velocity[Y] -0.040711 0.10381 0.00012208 0.00012208 v Velocity[Z] -1.4062e-05 1.6272e-05 -1.1086e-07 -1.1086e-07 v ǁVelocityǁ 9.7644e-08 0.10381 0.0076874 0.0076874 v Pressure -0.010678 0.03663 4.9294e-18 -4.5316e-18 v TempC 2.5101e-06 9.9032 2.47 2.47 v Density 0.97991 1 0.99795 0.99795 v TurbVisc 0 1.1768e-05 9.1951e-08 9.1951e-08 v CourantNb 8.9949e-07 1.0424 0.087275 0.087275 v FourierNb 0.036601 0.090591 0.072211 0.072211 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Csdyn2 0 0.004225 0.0028221 0.0028221 v SpecHeat 1017.2 1017.2 1017.2 1017.2 v ThermalCond 0.2 1 0.6 0.6 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 2.3807e-06 10 2.4985 2.4985 v Boundary Density 0.97991 1 0.99792 0.99792 v Yplus 0.0012882 5.2968 0.95523 0.95523 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.036603 1.1164 0.15949 0.15949 INSTANT 0.515000000E+02 TIME STEP NUMBER 515 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 20800 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00 Friction velocity uet : 0.11633E-04 0.19605E-01 Friction velocity uk : 0.11633E-04 0.19605E-01 Dimensionless distance yplus : 0.31784E-02 0.52955E+01 Friction thermal sca. tstar : -0.83004E+03 0.89570E+03 Rough dim-less th. sca. tplus : 0.59166E-04 0.49287E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 20800 Total number of wall faces : 20800 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.16742E-04 2 0.38491E-04 0.33282E-08 0.11263E-01 c Velocity[X] 0.57055E-09 c Velocity[Y] 0.27549E-08 c Velocity[Z] 0.27633E-11 c Pressure 0.24130E-07 7 0.55845E-05 0.24019E-02 0.32377E-01 c TempC 0.43710E+01 2 0.91292E-05 0.10822E-03 0.83278E-02 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a TempC ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.019696 0.031944 1.5838e-05 1.5838e-05 v Velocity[Y] -0.040726 0.10375 0.00012224 0.00012224 v Velocity[Z] -1.2562e-05 1.4757e-05 -1.0275e-07 -1.0275e-07 v ǁVelocityǁ 8.1825e-08 0.10375 0.0076825 0.0076825 v Pressure -0.010708 0.036698 9.6811e-18 8.4703e-20 v TempC 2.6436e-06 9.9034 2.4723 2.4723 v Density 0.9799 1 0.99794 0.99794 v TurbVisc 0 1.177e-05 9.1971e-08 9.1971e-08 v CourantNb 4.0873e-07 1.0418 0.087211 0.087211 v FourierNb 0.0366 0.09059 0.072212 0.072212 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Csdyn2 0 0.004225 0.0028225 0.0028225 v SpecHeat 1017.2 1017.2 1017.2 1017.2 v ThermalCond 0.2 1 0.6 0.6 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 2.5101e-06 10 2.5008 2.5008 v Boundary Density 0.9799 1 0.99791 0.99791 v Yplus 0.0031784 5.2955 0.95408 0.95408 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.036602 1.1158 0.15942 0.15942 INSTANT 0.516000000E+02 TIME STEP NUMBER 516 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 20800 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00 Friction velocity uet : 0.14614E-04 0.19599E-01 Friction velocity uk : 0.14614E-04 0.19599E-01 Dimensionless distance yplus : 0.39928E-02 0.52941E+01 Friction thermal sca. tstar : -0.91043E+03 0.13689E+04 Rough dim-less th. sca. tplus : 0.74324E-04 0.49274E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 20800 Total number of wall faces : 20800 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.16734E-04 2 0.34359E-04 0.32195E-08 0.11083E-01 c Velocity[X] 0.56459E-09 c Velocity[Y] 0.26527E-08 c Velocity[Z] 0.21882E-11 c Pressure 0.23418E-07 7 0.55243E-05 0.23284E-02 0.32276E-01 c TempC 0.43723E+01 2 0.57672E-05 0.10791E-03 0.83129E-02 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a TempC ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.019679 0.031901 1.585e-05 1.585e-05 v Velocity[Y] -0.040742 0.1037 0.00012238 0.00012238 v Velocity[Z] -1.1231e-05 1.3378e-05 -9.5226e-08 -9.5226e-08 v ǁVelocityǁ 9.5306e-08 0.1037 0.0076776 0.0076776 v Pressure -0.010738 0.036765 8.5709e-18 -1.6517e-18 v TempC 2.7836e-06 9.9035 2.4746 2.4746 v Density 0.97988 1 0.99794 0.99794 v TurbVisc 0 1.1772e-05 9.2009e-08 9.2009e-08 v CourantNb 4.9322e-07 1.0412 0.087146 0.087146 v FourierNb 0.0366 0.09059 0.072212 0.072212 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Csdyn2 0 0.004225 0.0028247 0.0028247 v SpecHeat 1017.2 1017.2 1017.2 1017.2 v ThermalCond 0.2 1 0.6 0.6 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 2.6436e-06 10 2.503 2.503 v Boundary Density 0.97988 1 0.99791 0.99791 v Yplus 0.0039928 5.2941 0.95299 0.95299 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.036602 1.1153 0.15936 0.15936 INSTANT 0.517000000E+02 TIME STEP NUMBER 517 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 20800 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00 Friction velocity uet : 0.12424E-04 0.19594E-01 Friction velocity uk : 0.12424E-04 0.19594E-01 Dimensionless distance yplus : 0.33946E-02 0.52927E+01 Friction thermal sca. tstar : -0.11648E+04 0.11640E+04 Rough dim-less th. sca. tplus : 0.63190E-04 0.49261E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 20800 Total number of wall faces : 20800 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.16725E-04 2 0.30717E-04 0.31325E-08 0.10938E-01 c Velocity[X] 0.55916E-09 c Velocity[Y] 0.25716E-08 c Velocity[Z] 0.17384E-11 c Pressure 0.22867E-07 7 0.54648E-05 0.22710E-02 0.32177E-01 c TempC 0.43736E+01 2 0.86747E-05 0.10768E-03 0.83007E-02 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a TempC ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.019663 0.031858 1.5862e-05 1.5862e-05 v Velocity[Y] -0.040759 0.10365 0.00012252 0.00012252 v Velocity[Z] -1.0047e-05 1.2126e-05 -8.8248e-08 -8.8248e-08 v ǁVelocityǁ 1.2189e-07 0.10365 0.0076727 0.0076727 v Pressure -0.010768 0.036832 5.3291e-18 -4.3199e-18 v TempC 2.9335e-06 9.9036 2.4768 2.4768 v Density 0.97987 1 0.99793 0.99793 v TurbVisc 0 1.1775e-05 9.2039e-08 9.2039e-08 v CourantNb 2.7476e-07 1.0407 0.087082 0.087082 v FourierNb 0.0366 0.09059 0.072213 0.072213 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Csdyn2 0 0.004225 0.0028256 0.0028256 v SpecHeat 1017.2 1017.2 1017.2 1017.2 v ThermalCond 0.2 1 0.6 0.6 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 2.7836e-06 10 2.5052 2.5052 v Boundary Density 0.97987 1 0.9979 0.9979 v Yplus 0.0033946 5.2927 0.95195 0.95195 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.036602 1.1147 0.15929 0.15929 INSTANT 0.518000000E+02 TIME STEP NUMBER 518 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 20800 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00 Friction velocity uet : 0.64823E-05 0.19588E-01 Friction velocity uk : 0.64823E-05 0.19588E-01 Dimensionless distance yplus : 0.17711E-02 0.52913E+01 Friction thermal sca. tstar : -0.13917E+04 0.10606E+04 Rough dim-less th. sca. tplus : 0.32969E-04 0.49248E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 20800 Total number of wall faces : 20800 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.16717E-04 2 0.27500E-04 0.30615E-08 0.10819E-01 c Velocity[X] 0.55374E-09 c Velocity[Y] 0.25064E-08 c Velocity[Z] 0.13854E-11 c Pressure 0.22406E-07 9 0.73937E-05 0.22228E-02 0.32063E-01 c TempC 0.43750E+01 2 0.83275E-05 0.10733E-03 0.82845E-02 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a TempC ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.01965 0.031816 1.5872e-05 1.5872e-05 v Velocity[Y] -0.040777 0.10359 0.00012266 0.00012266 v Velocity[Z] -8.9949e-06 1.0988e-05 -8.1778e-08 -8.1778e-08 v ǁVelocityǁ 1.2706e-07 0.10359 0.0076678 0.0076678 v Pressure -0.010798 0.036899 4.2633e-18 -5.5481e-18 v TempC 3.086e-06 9.9037 2.4791 2.4791 v Density 0.97985 1 0.99793 0.99793 v TurbVisc 0 1.1777e-05 9.2072e-08 9.2072e-08 v CourantNb 5.4856e-07 1.0401 0.087018 0.087018 v FourierNb 0.0366 0.09059 0.072213 0.072213 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Csdyn2 0 0.004225 0.0028263 0.0028263 v SpecHeat 1017.2 1017.2 1017.2 1017.2 v ThermalCond 0.2 1 0.6 0.6 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 2.9335e-06 10 2.5075 2.5075 v Boundary Density 0.97985 1 0.9979 0.9979 v Yplus 0.0017711 5.2913 0.95097 0.95097 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.036601 1.1141 0.15923 0.15923 INSTANT 0.519000000E+02 TIME STEP NUMBER 519 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 20800 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00 Friction velocity uet : 0.66409E-05 0.19583E-01 Friction velocity uk : 0.66409E-05 0.19583E-01 Dimensionless distance yplus : 0.18144E-02 0.52899E+01 Friction thermal sca. tstar : -0.13456E+04 0.11205E+04 Rough dim-less th. sca. tplus : 0.33776E-04 0.49235E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 20800 Total number of wall faces : 20800 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.16709E-04 2 0.24650E-04 0.30051E-08 0.10724E-01 c Velocity[X] 0.54953E-09 c Velocity[Y] 0.24545E-08 c Velocity[Z] 0.11073E-11 c Pressure 0.22067E-07 9 0.72770E-05 0.21867E-02 0.32003E-01 c TempC 0.43763E+01 2 0.98935E-05 0.10692E-03 0.82655E-02 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a TempC ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.019638 0.031775 1.5884e-05 1.5884e-05 v Velocity[Y] -0.040795 0.10354 0.00012278 0.00012278 v Velocity[Z] -8.143e-06 9.9555e-06 -7.578e-08 -7.578e-08 v ǁVelocityǁ 1.285e-07 0.10354 0.0076629 0.0076629 v Pressure -0.010829 0.036966 4.0856e-18 -5.8445e-18 v TempC 3.2513e-06 9.9039 2.4813 2.4813 v Density 0.97984 1 0.99792 0.99792 v TurbVisc 0 1.178e-05 9.2103e-08 9.2103e-08 v CourantNb 3.5304e-07 1.0395 0.086954 0.086954 v FourierNb 0.0366 0.090591 0.072214 0.072214 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Csdyn2 0 0.004225 0.0028269 0.0028269 v SpecHeat 1017.2 1017.2 1017.2 1017.2 v ThermalCond 0.2 1 0.6 0.6 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 3.086e-06 10 2.5097 2.5097 v Boundary Density 0.97984 1 0.99789 0.99789 v Yplus 0.0018144 5.2899 0.95003 0.95003 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.036601 1.1136 0.15917 0.15917 INSTANT 0.520000000E+02 TIME STEP NUMBER 520 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 20800 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00 Friction velocity uet : 0.10100E-04 0.19578E-01 Friction velocity uk : 0.10100E-04 0.19578E-01 Dimensionless distance yplus : 0.27596E-02 0.52885E+01 Friction thermal sca. tstar : -0.12045E+04 0.11793E+04 Rough dim-less th. sca. tplus : 0.51368E-04 0.49222E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 20800 Total number of wall faces : 20800 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.16700E-04 2 0.22127E-04 0.29574E-08 0.10644E-01 c Velocity[X] 0.54504E-09 c Velocity[Y] 0.24114E-08 c Velocity[Z] 0.88746E-12 c Pressure 0.21756E-07 9 0.72103E-05 0.21536E-02 0.31889E-01 c TempC 0.43777E+01 2 0.55946E-05 0.10664E-03 0.82516E-02 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a TempC ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.019628 0.031735 1.5895e-05 1.5895e-05 v Velocity[Y] -0.040814 0.10348 0.0001229 0.0001229 v Velocity[Z] -7.6481e-06 9.0187e-06 -7.0221e-08 -7.0221e-08 v ǁVelocityǁ 1.1104e-07 0.10348 0.007658 0.007658 v Pressure -0.010859 0.037033 1.3056e-17 2.5411e-18 v TempC 3.4182e-06 9.904 2.4836 2.4836 v Density 0.97983 1 0.99792 0.99792 v TurbVisc 0 1.1783e-05 9.2112e-08 9.2112e-08 v CourantNb 2.3045e-07 1.039 0.086891 0.086891 v FourierNb 0.0366 0.090593 0.072214 0.072214 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Csdyn2 0 0.004225 0.0028276 0.0028276 v SpecHeat 1017.2 1017.2 1017.2 1017.2 v ThermalCond 0.2 1 0.6 0.6 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 3.2513e-06 10 2.5119 2.5119 v Boundary Density 0.97983 1 0.99789 0.99789 v Yplus 0.0027596 5.2885 0.94914 0.94914 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.036601 1.113 0.1591 0.1591 INSTANT 0.521000000E+02 TIME STEP NUMBER 521 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 20800 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00 Friction velocity uet : 0.96362E-05 0.19573E-01 Friction velocity uk : 0.96362E-05 0.19573E-01 Dimensionless distance yplus : 0.26328E-02 0.52871E+01 Friction thermal sca. tstar : -0.11043E+04 0.13422E+04 Rough dim-less th. sca. tplus : 0.49009E-04 0.49209E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 20800 Total number of wall faces : 20800 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.16692E-04 2 0.19892E-04 0.29158E-08 0.10574E-01 c Velocity[X] 0.54045E-09 c Velocity[Y] 0.23746E-08 c Velocity[Z] 0.71312E-12 c Pressure 0.21492E-07 9 0.71302E-05 0.21251E-02 0.31787E-01 c TempC 0.43790E+01 2 0.90153E-05 0.10644E-03 0.82407E-02 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a TempC ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.019619 0.031696 1.5905e-05 1.5905e-05 v Velocity[Y] -0.040832 0.10343 0.00012302 0.00012302 v Velocity[Z] -7.1513e-06 9.0387e-06 -6.5067e-08 -6.5067e-08 v ǁVelocityǁ 9.5185e-08 0.10343 0.0076532 0.0076532 v Pressure -0.010889 0.0371 9.5923e-18 1.2705e-19 v TempC 3.5243e-06 9.9041 2.4858 2.4858 v Density 0.97981 1 0.99791 0.99791 v TurbVisc 0 1.1786e-05 9.2102e-08 9.2102e-08 v CourantNb 2.1614e-07 1.0384 0.086828 0.086828 v FourierNb 0.0366 0.090594 0.072214 0.072214 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Csdyn2 0 0.004225 0.0028282 0.0028282 v SpecHeat 1017.2 1017.2 1017.2 1017.2 v ThermalCond 0.2 1 0.6 0.6 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 3.4182e-06 10 2.5142 2.5142 v Boundary Density 0.97981 1 0.99788 0.99788 v Yplus 0.0026328 5.2871 0.94828 0.94828 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.036601 1.1124 0.15904 0.15904 INSTANT 0.522000000E+02 TIME STEP NUMBER 522 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 20800 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00 Friction velocity uet : 0.99649E-05 0.19568E-01 Friction velocity uk : 0.99649E-05 0.19568E-01 Dimensionless distance yplus : 0.27227E-02 0.52856E+01 Friction thermal sca. tstar : -0.12067E+04 0.12910E+04 Rough dim-less th. sca. tplus : 0.50682E-04 0.49195E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 20800 Total number of wall faces : 20800 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.16683E-04 2 0.17911E-04 0.28796E-08 0.10514E-01 c Velocity[X] 0.53592E-09 c Velocity[Y] 0.23431E-08 c Velocity[Z] 0.57443E-12 c Pressure 0.21248E-07 9 0.70551E-05 0.20986E-02 0.31690E-01 c TempC 0.43803E+01 2 0.92358E-05 0.10609E-03 0.82244E-02 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a TempC ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.019612 0.031659 1.5915e-05 1.5915e-05 v Velocity[Y] -0.04085 0.10337 0.00012313 0.00012313 v Velocity[Z] -6.6578e-06 7.3989e-06 -6.0291e-08 -6.0291e-08 v ǁVelocityǁ 1.1263e-07 0.10337 0.0076483 0.0076483 v Pressure -0.010919 0.037166 9.015e-18 -1.3129e-18 v TempC 3.628e-06 9.9042 2.4881 2.4881 v Density 0.9798 1 0.99791 0.99791 v TurbVisc 0 1.1789e-05 9.2089e-08 9.2089e-08 v CourantNb 2.9412e-07 1.0378 0.086764 0.086764 v FourierNb 0.0366 0.090596 0.072215 0.072215 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Csdyn2 0 0.004225 0.0028286 0.0028286 v SpecHeat 1017.2 1017.2 1017.2 1017.2 v ThermalCond 0.2 1 0.6 0.6 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 3.5243e-06 10 2.5164 2.5164 v Boundary Density 0.9798 1 0.99788 0.99788 v Yplus 0.0027227 5.2856 0.94746 0.94746 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.036601 1.1119 0.15898 0.15898 INSTANT 0.523000000E+02 TIME STEP NUMBER 523 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 20800 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00 Friction velocity uet : 0.82275E-05 0.19563E-01 Friction velocity uk : 0.82275E-05 0.19563E-01 Dimensionless distance yplus : 0.22479E-02 0.52842E+01 Friction thermal sca. tstar : -0.14256E+04 0.13450E+04 Rough dim-less th. sca. tplus : 0.41845E-04 0.49182E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 20800 Total number of wall faces : 20800 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.16675E-04 2 0.16154E-04 0.28501E-08 0.10465E-01 c Velocity[X] 0.53162E-09 c Velocity[Y] 0.23180E-08 c Velocity[Z] 0.46377E-12 c Pressure 0.21083E-07 9 0.69780E-05 0.20801E-02 0.31603E-01 c TempC 0.43817E+01 3 0.10310E-05 0.10598E-03 0.82170E-02 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a TempC ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.019606 0.031622 1.5925e-05 1.5925e-05 v Velocity[Y] -0.040869 0.10332 0.00012324 0.00012324 v Velocity[Z] -6.1724e-06 6.701e-06 -5.5866e-08 -5.5866e-08 v ǁVelocityǁ 8.1447e-08 0.10332 0.0076434 0.0076434 v Pressure -0.010949 0.037232 6.9722e-18 -3.2187e-18 v TempC 3.7315e-06 9.9044 2.4903 2.4903 v Density 0.97978 1 0.9979 0.9979 v TurbVisc 0 1.1792e-05 9.207e-08 9.207e-08 v CourantNb 3.0251e-07 1.0373 0.086701 0.086701 v FourierNb 0.0366 0.090598 0.072215 0.072215 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Csdyn2 0 0.004225 0.0028295 0.0028295 v SpecHeat 1017.2 1017.2 1017.2 1017.2 v ThermalCond 0.2 1 0.6 0.6 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 3.628e-06 10 2.5186 2.5186 v Boundary Density 0.97978 1 0.99787 0.99787 v Yplus 0.0022479 5.2842 0.94667 0.94667 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.0366 1.1113 0.15892 0.15892 INSTANT 0.524000000E+02 TIME STEP NUMBER 524 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 20800 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00 Friction velocity uet : 0.61636E-05 0.19557E-01 Friction velocity uk : 0.61636E-05 0.19557E-01 Dimensionless distance yplus : 0.16840E-02 0.52827E+01 Friction thermal sca. tstar : -0.16753E+04 0.13990E+04 Rough dim-less th. sca. tplus : 0.31348E-04 0.49169E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 20800 Total number of wall faces : 20800 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.16666E-04 2 0.14599E-04 0.28228E-08 0.10420E-01 c Velocity[X] 0.52727E-09 c Velocity[Y] 0.22952E-08 c Velocity[Z] 0.37524E-12 c Pressure 0.20921E-07 9 0.69099E-05 0.20619E-02 0.31502E-01 c TempC 0.43830E+01 2 0.78964E-05 0.10558E-03 0.81985E-02 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a TempC ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.019601 0.031587 1.5935e-05 1.5935e-05 v Velocity[Y] -0.040887 0.10326 0.00012335 0.00012335 v Velocity[Z] -5.6989e-06 6.0687e-06 -5.1765e-08 -5.1765e-08 v ǁVelocityǁ 5.7182e-08 0.10326 0.0076386 0.0076386 v Pressure -0.01098 0.037298 1.4255e-17 4.574e-18 v TempC 3.8445e-06 9.9045 2.4926 2.4926 v Density 0.97977 1 0.9979 0.9979 v TurbVisc 0 1.1794e-05 9.2043e-08 9.2043e-08 v CourantNb 2.3682e-07 1.0367 0.086638 0.086638 v FourierNb 0.0366 0.0906 0.072215 0.072215 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Csdyn2 0 0.004225 0.0028299 0.0028299 v SpecHeat 1017.2 1017.2 1017.2 1017.2 v ThermalCond 0.2 1 0.6 0.6 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 3.7315e-06 10 2.5209 2.5209 v Boundary Density 0.97977 1 0.99787 0.99787 v Yplus 0.001684 5.2827 0.94591 0.94591 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.0366 1.1108 0.15885 0.15885 INSTANT 0.525000000E+02 TIME STEP NUMBER 525 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 20800 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00 Friction velocity uet : 0.35766E-05 0.19552E-01 Friction velocity uk : 0.35766E-05 0.19552E-01 Dimensionless distance yplus : 0.97720E-03 0.52813E+01 Friction thermal sca. tstar : -0.18734E+04 0.14526E+04 Rough dim-less th. sca. tplus : 0.18190E-04 0.49155E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 20800 Total number of wall faces : 20800 ------------------------------------------------------------ Write intermediate restart files checkpoint at iteration 525, Physical time 0.52500E+02 ** Writing the main restart file ----------------------------- Start writing Wrote field names and types to checkpoint at iteration 525: checkpoint/main End writing the options Wrote main variables to checkpoint: checkpoint/main End writing ** Writing the auxiliary restart file ---------------------------------- Start writing End writing the dimensions and options End writing the physical properties End writing the time step Wrote boundary condition coefficients to checkpoint: checkpoint/auxiliary End writing the source terms End writing ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.16657E-04 2 0.13216E-04 0.27933E-08 0.10371E-01 c Velocity[X] 0.52237E-09 c Velocity[Y] 0.22706E-08 c Velocity[Z] 0.30423E-12 c Pressure 0.20672E-07 9 0.68570E-05 0.20351E-02 0.31418E-01 c TempC 0.43843E+01 2 0.76382E-05 0.10527E-03 0.81834E-02 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a TempC ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.019598 0.031551 1.5945e-05 1.5945e-05 v Velocity[Y] -0.040904 0.1032 0.00012346 0.00012346 v Velocity[Z] -5.2407e-06 5.4961e-06 -4.7965e-08 -4.7965e-08 v ǁVelocityǁ 3.2014e-08 0.1032 0.0076337 0.0076337 v Pressure -0.01101 0.037364 1.0036e-17 3.8116e-19 v TempC 3.9485e-06 9.9046 2.4948 2.4948 v Density 0.97976 1 0.99789 0.99789 v TurbVisc 0 1.1797e-05 9.2012e-08 9.2012e-08 v CourantNb 1.8424e-07 1.0362 0.086576 0.086576 v FourierNb 0.0366 0.090603 0.072216 0.072216 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Csdyn2 0 0.004225 0.0028303 0.0028303 v SpecHeat 1017.2 1017.2 1017.2 1017.2 v ThermalCond 0.2 1 0.6 0.6 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 3.8445e-06 10 2.5231 2.5231 v Boundary Density 0.97976 1 0.99786 0.99786 v Yplus 0.0009772 5.2813 0.94518 0.94518 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.0366 1.1102 0.15879 0.15879 INSTANT 0.526000000E+02 TIME STEP NUMBER 526 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 20800 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00 Friction velocity uet : 0.42398E-05 0.19547E-01 Friction velocity uk : 0.42398E-05 0.19547E-01 Dimensionless distance yplus : 0.11584E-02 0.52798E+01 Friction thermal sca. tstar : -0.19105E+04 0.15074E+04 Rough dim-less th. sca. tplus : 0.21564E-04 0.49141E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 20800 Total number of wall faces : 20800 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.16649E-04 2 0.11995E-04 0.27727E-08 0.10338E-01 c Velocity[X] 0.51817E-09 c Velocity[Y] 0.22543E-08 c Velocity[Z] 0.24713E-12 c Pressure 0.20609E-07 9 0.67750E-05 0.20268E-02 0.31323E-01 c TempC 0.43857E+01 2 0.90933E-05 0.10488E-03 0.81655E-02 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a TempC ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.019595 0.031516 1.5954e-05 1.5954e-05 v Velocity[Y] -0.040922 0.10314 0.00012356 0.00012356 v Velocity[Z] -4.8006e-06 4.9775e-06 -4.4444e-08 -4.4444e-08 v ǁVelocityǁ 1.1871e-08 0.10314 0.0076289 0.0076289 v Pressure -0.01104 0.03743 1.5987e-17 6.141e-18 v TempC 4.0448e-06 9.9047 2.4971 2.4971 v Density 0.97974 1 0.99789 0.99789 v TurbVisc 0 1.18e-05 9.1977e-08 9.1977e-08 v CourantNb 1.424e-07 1.0356 0.086513 0.086513 v FourierNb 0.0366 0.090605 0.072216 0.072216 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Csdyn2 0 0.004225 0.0028307 0.0028307 v SpecHeat 1017.2 1017.2 1017.2 1017.2 v ThermalCond 0.2 1 0.6 0.6 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 3.9485e-06 10 2.5253 2.5253 v Boundary Density 0.97974 1 0.99786 0.99786 v Yplus 0.0011584 5.2798 0.94447 0.94447 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.0366 1.1097 0.15873 0.15873 INSTANT 0.527000000E+02 TIME STEP NUMBER 527 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 20800 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00 Friction velocity uet : 0.61915E-05 0.19541E-01 Friction velocity uk : 0.61915E-05 0.19541E-01 Dimensionless distance yplus : 0.16917E-02 0.52783E+01 Friction thermal sca. tstar : -0.18296E+04 0.15681E+04 Rough dim-less th. sca. tplus : 0.31490E-04 0.49127E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 20800 Total number of wall faces : 20800 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.16640E-04 2 0.10911E-04 0.27528E-08 0.10306E-01 c Velocity[X] 0.51389E-09 c Velocity[Y] 0.22387E-08 c Velocity[Z] 0.20111E-12 c Pressure 0.20521E-07 9 0.67156E-05 0.20159E-02 0.31222E-01 c TempC 0.43870E+01 2 0.59091E-05 0.10460E-03 0.81515E-02 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a TempC ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.019593 0.031481 1.5963e-05 1.5963e-05 v Velocity[Y] -0.040939 0.10308 0.00012366 0.00012366 v Velocity[Z] -4.3807e-06 4.6462e-06 -4.1182e-08 -4.1182e-08 v ǁVelocityǁ 2.2027e-08 0.10309 0.007624 0.007624 v Pressure -0.011071 0.037496 1.1946e-17 1.3553e-18 v TempC 4.1443e-06 9.9049 2.4993 2.4993 v Density 0.97973 1 0.99788 0.99788 v TurbVisc 0 1.1802e-05 9.196e-08 9.196e-08 v CourantNb 1.0935e-07 1.035 0.086451 0.086451 v FourierNb 0.0366 0.090607 0.072216 0.072216 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Csdyn2 0 0.004225 0.0028322 0.0028322 v SpecHeat 1017.2 1017.2 1017.2 1017.2 v ThermalCond 0.2 1 0.6 0.6 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 4.0448e-06 10 2.5275 2.5275 v Boundary Density 0.97973 1 0.99785 0.99785 v Yplus 0.0016917 5.2783 0.94378 0.94378 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.0366 1.1091 0.15867 0.15867 INSTANT 0.528000000E+02 TIME STEP NUMBER 528 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 20800 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00 Friction velocity uet : 0.52517E-05 0.19536E-01 Friction velocity uk : 0.52517E-05 0.19536E-01 Dimensionless distance yplus : 0.14349E-02 0.52768E+01 Friction thermal sca. tstar : -0.17658E+04 0.17249E+04 Rough dim-less th. sca. tplus : 0.26710E-04 0.49113E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 20800 Total number of wall faces : 20800 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.16631E-04 2 0.99783E-05 0.27328E-08 0.10274E-01 c Velocity[X] 0.50954E-09 c Velocity[Y] 0.22231E-08 c Velocity[Z] 0.16394E-12 c Pressure 0.20425E-07 7 0.99759E-05 0.20044E-02 0.31119E-01 c TempC 0.43883E+01 2 0.86798E-05 0.10434E-03 0.81382E-02 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a TempC ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.019592 0.031445 1.5971e-05 1.5971e-05 v Velocity[Y] -0.040956 0.10303 0.00012376 0.00012376 v Velocity[Z] -3.9826e-06 4.083e-06 -3.8161e-08 -3.8161e-08 v ǁVelocityǁ 3.8189e-08 0.10303 0.0076192 0.0076192 v Pressure -0.011101 0.037561 1.4522e-17 4.4469e-18 v TempC 4.2483e-06 9.905 2.5016 2.5016 v Density 0.97972 1 0.99788 0.99788 v TurbVisc 0 1.1805e-05 9.1952e-08 9.1952e-08 v CourantNb 8.3428e-08 1.0345 0.086388 0.086388 v FourierNb 0.0366 0.09061 0.072216 0.072216 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Csdyn2 0 0.004225 0.0028327 0.0028327 v SpecHeat 1017.2 1017.2 1017.2 1017.2 v ThermalCond 0.2 1 0.6 0.6 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 4.1443e-06 10 2.5298 2.5298 v Boundary Density 0.97972 1 0.99785 0.99785 v Yplus 0.0014349 5.2768 0.94312 0.94312 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.0366 1.1085 0.1586 0.1586 INSTANT 0.529000000E+02 TIME STEP NUMBER 529 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 20800 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00 Friction velocity uet : 0.51747E-05 0.19530E-01 Friction velocity uk : 0.51747E-05 0.19530E-01 Dimensionless distance yplus : 0.14139E-02 0.52752E+01 Friction thermal sca. tstar : -0.21832E+04 0.19006E+04 Rough dim-less th. sca. tplus : 0.26319E-04 0.49099E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 20800 Total number of wall faces : 20800 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.16623E-04 2 0.91729E-05 0.27132E-08 0.10242E-01 c Velocity[X] 0.50512E-09 c Velocity[Y] 0.22079E-08 c Velocity[Z] 0.13386E-12 c Pressure 0.20361E-07 7 0.98769E-05 0.19960E-02 0.31027E-01 c TempC 0.43896E+01 2 0.59812E-05 0.10405E-03 0.81242E-02 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a TempC ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.019591 0.031409 1.598e-05 1.598e-05 v Velocity[Y] -0.040972 0.10297 0.00012386 0.00012386 v Velocity[Z] -3.6074e-06 3.6983e-06 -3.5361e-08 -3.5361e-08 v ǁVelocityǁ 4.3268e-08 0.10297 0.0076143 0.0076143 v Pressure -0.011132 0.037627 6.4837e-18 -3.9387e-18 v TempC 4.3545e-06 9.9051 2.5038 2.5038 v Density 0.9797 1 0.99787 0.99787 v TurbVisc 0 1.1807e-05 9.1938e-08 9.1938e-08 v CourantNb 6.3284e-08 1.0339 0.086326 0.086326 v FourierNb 0.0366 0.090612 0.072217 0.072217 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Csdyn2 0 0.004225 0.002833 0.002833 v SpecHeat 1017.2 1017.2 1017.2 1017.2 v ThermalCond 0.2 1 0.6 0.6 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 4.2483e-06 10 2.532 2.532 v Boundary Density 0.9797 1 0.99784 0.99784 v Yplus 0.0014139 5.2752 0.94248 0.94248 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.0366 1.108 0.15854 0.15854 INSTANT 0.530000000E+02 TIME STEP NUMBER 530 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 20800 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00 Friction velocity uet : 0.58782E-05 0.19525E-01 Friction velocity uk : 0.58782E-05 0.19525E-01 Dimensionless distance yplus : 0.16061E-02 0.52738E+01 Friction thermal sca. tstar : -0.26979E+04 0.20986E+04 Rough dim-less th. sca. tplus : 0.29897E-04 0.49085E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 20800 Total number of wall faces : 20800 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.16614E-04 2 0.84934E-05 0.26954E-08 0.10214E-01 c Velocity[X] 0.50082E-09 c Velocity[Y] 0.21945E-08 c Velocity[Z] 0.10946E-12 c Pressure 0.20290E-07 7 0.98004E-05 0.19869E-02 0.30934E-01 c TempC 0.43909E+01 2 0.83588E-05 0.10376E-03 0.81100E-02 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a TempC ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.019591 0.031372 1.5989e-05 1.5989e-05 v Velocity[Y] -0.040989 0.10291 0.00012396 0.00012396 v Velocity[Z] -3.5194e-06 3.3501e-06 -3.2768e-08 -3.2768e-08 v ǁVelocityǁ 3.7356e-08 0.10291 0.0076095 0.0076095 v Pressure -0.011162 0.037692 8.6597e-18 -1.5247e-18 v TempC 4.4658e-06 9.9052 2.506 2.506 v Density 0.97969 1 0.99787 0.99787 v TurbVisc 0 1.1809e-05 9.1934e-08 9.1934e-08 v CourantNb 4.7782e-08 1.0333 0.086263 0.086263 v FourierNb 0.0366 0.090615 0.072217 0.072217 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Csdyn2 0 0.004225 0.0028338 0.0028338 v SpecHeat 1017.2 1017.2 1017.2 1017.2 v ThermalCond 0.2 1 0.6 0.6 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 4.3545e-06 10 2.5342 2.5342 v Boundary Density 0.97969 1 0.99784 0.99784 v Yplus 0.0016061 5.2738 0.94186 0.94186 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.0366 1.1074 0.15848 0.15848 INSTANT 0.531000000E+02 TIME STEP NUMBER 531 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 20800 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00 Friction velocity uet : 0.39591E-05 0.19519E-01 Friction velocity uk : 0.39591E-05 0.19519E-01 Dimensionless distance yplus : 0.10817E-02 0.52723E+01 Friction thermal sca. tstar : -0.29834E+04 0.23223E+04 Rough dim-less th. sca. tplus : 0.20136E-04 0.49071E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 20800 Total number of wall faces : 20800 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.16605E-04 2 0.79169E-05 0.26774E-08 0.10185E-01 c Velocity[X] 0.49648E-09 c Velocity[Y] 0.21808E-08 c Velocity[Z] 0.89637E-13 c Pressure 0.20195E-07 7 0.97193E-05 0.19755E-02 0.30838E-01 c TempC 0.43922E+01 2 0.55921E-05 0.10350E-03 0.80966E-02 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a TempC ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.019591 0.031334 1.5997e-05 1.5997e-05 v Velocity[Y] -0.041004 0.10285 0.00012406 0.00012406 v Velocity[Z] -2.9339e-06 3.1926e-06 -3.0366e-08 -3.0366e-08 v ǁVelocityǁ 2.932e-08 0.10285 0.0076047 0.0076047 v Pressure -0.011193 0.037758 1.2479e-17 2.287e-18 v TempC 4.5797e-06 9.9053 2.5083 2.5083 v Density 0.97967 1 0.99786 0.99786 v TurbVisc 0 1.1811e-05 9.1933e-08 9.1933e-08 v CourantNb 3.5997e-08 1.0327 0.086201 0.086201 v FourierNb 0.0366 0.090617 0.072218 0.072218 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Csdyn2 0 0.004225 0.002834 0.002834 v SpecHeat 1017.2 1017.2 1017.2 1017.2 v ThermalCond 0.2 1 0.6 0.6 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 4.4658e-06 10 2.5364 2.5364 v Boundary Density 0.97967 1 0.99783 0.99783 v Yplus 0.0010817 5.2723 0.94125 0.94125 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.0366 1.1068 0.15842 0.15842 INSTANT 0.532000000E+02 TIME STEP NUMBER 532 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 20800 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00 Friction velocity uet : 0.47877E-05 0.19513E-01 Friction velocity uk : 0.47877E-05 0.19513E-01 Dimensionless distance yplus : 0.13081E-02 0.52709E+01 Friction thermal sca. tstar : -0.28020E+04 0.25776E+04 Rough dim-less th. sca. tplus : 0.24350E-04 0.49058E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 20800 Total number of wall faces : 20800 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.16597E-04 2 0.74427E-05 0.26605E-08 0.10158E-01 c Velocity[X] 0.49220E-09 c Velocity[Y] 0.21682E-08 c Velocity[Z] 0.73504E-13 c Pressure 0.20144E-07 7 0.96353E-05 0.19685E-02 0.30746E-01 c TempC 0.43936E+01 2 0.79763E-05 0.10323E-03 0.80835E-02 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a TempC ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.019591 0.031296 1.6005e-05 1.6005e-05 v Velocity[Y] -0.04102 0.10279 0.00012415 0.00012415 v Velocity[Z] -2.6899e-06 3.0069e-06 -2.8141e-08 -2.8141e-08 v ǁVelocityǁ 2.2735e-08 0.10279 0.0075998 0.0075998 v Pressure -0.011223 0.037823 8.3045e-18 -1.8635e-18 v TempC 4.6994e-06 9.9054 2.5105 2.5105 v Density 0.97966 1 0.99786 0.99786 v TurbVisc 0 1.1814e-05 9.1948e-08 9.1948e-08 v CourantNb 2.7167e-08 1.0321 0.086139 0.086139 v FourierNb 0.0366 0.09062 0.072218 0.072218 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Csdyn2 0 0.004225 0.0028349 0.0028349 v SpecHeat 1017.2 1017.2 1017.2 1017.2 v ThermalCond 0.2 1 0.6 0.6 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 4.5797e-06 10 2.5386 2.5386 v Boundary Density 0.97966 1 0.99783 0.99783 v Yplus 0.0013081 5.2709 0.94066 0.94066 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.0366 1.1062 0.15836 0.15836 INSTANT 0.533000000E+02 TIME STEP NUMBER 533 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 20800 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00 Friction velocity uet : 0.37779E-05 0.19508E-01 Friction velocity uk : 0.37779E-05 0.19508E-01 Dimensionless distance yplus : 0.10322E-02 0.52694E+01 Friction thermal sca. tstar : -0.28969E+04 0.28700E+04 Rough dim-less th. sca. tplus : 0.19214E-04 0.49044E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 20800 Total number of wall faces : 20800 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.16588E-04 2 0.70474E-05 0.26433E-08 0.10131E-01 c Velocity[X] 0.48786E-09 c Velocity[Y] 0.21553E-08 c Velocity[Z] 0.60351E-13 c Pressure 0.20062E-07 7 0.95569E-05 0.19584E-02 0.30651E-01 c TempC 0.43949E+01 2 0.79798E-05 0.10294E-03 0.80692E-02 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a TempC ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.019592 0.031257 1.6014e-05 1.6014e-05 v Velocity[Y] -0.041035 0.10273 0.00012425 0.00012425 v Velocity[Z] -2.4573e-06 2.4917e-06 -2.608e-08 -2.608e-08 v ǁVelocityǁ 1.7444e-08 0.10273 0.007595 0.007595 v Pressure -0.011254 0.037888 5.107e-18 -4.7434e-18 v TempC 4.8224e-06 9.9056 2.5127 2.5127 v Density 0.97965 1 0.99785 0.99785 v TurbVisc 0 1.1816e-05 9.1949e-08 9.1949e-08 v CourantNb 2.0668e-08 1.0316 0.086077 0.086077 v FourierNb 0.0366 0.090622 0.072218 0.072218 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Csdyn2 0 0.004225 0.0028347 0.0028347 v SpecHeat 1017.2 1017.2 1017.2 1017.2 v ThermalCond 0.2 1 0.6 0.6 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 4.6994e-06 10 2.5408 2.5408 v Boundary Density 0.97965 1 0.99782 0.99782 v Yplus 0.0010322 5.2694 0.94008 0.94008 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.0366 1.1056 0.1583 0.1583 INSTANT 0.534000000E+02 TIME STEP NUMBER 534 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 20800 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00 Friction velocity uet : 0.27236E-05 0.19502E-01 Friction velocity uk : 0.27236E-05 0.19502E-01 Dimensionless distance yplus : 0.74416E-03 0.52679E+01 Friction thermal sca. tstar : -0.33440E+04 0.32092E+04 Rough dim-less th. sca. tplus : 0.13852E-04 0.49030E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 20800 Total number of wall faces : 20800 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.16579E-04 2 0.67325E-05 0.26275E-08 0.10106E-01 c Velocity[X] 0.48362E-09 c Velocity[Y] 0.21438E-08 c Velocity[Z] 0.49612E-13 c Pressure 0.20022E-07 7 0.94750E-05 0.19526E-02 0.30561E-01 c TempC 0.43962E+01 2 0.96561E-05 0.10257E-03 0.80518E-02 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a TempC ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.019592 0.031216 1.6022e-05 1.6022e-05 v Velocity[Y] -0.04105 0.10268 0.00012434 0.00012434 v Velocity[Z] -2.7185e-06 2.2582e-06 -2.4171e-08 -2.4171e-08 v ǁVelocityǁ 1.3358e-08 0.10268 0.0075902 0.0075902 v Pressure -0.011285 0.037953 1.5232e-17 4.6163e-18 v TempC 4.9498e-06 9.9057 2.515 2.515 v Density 0.97963 1 0.99784 0.99784 v TurbVisc 0 1.1818e-05 9.1972e-08 9.1972e-08 v CourantNb 1.5992e-08 1.031 0.086015 0.086015 v FourierNb 0.0366 0.090625 0.072219 0.072219 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Csdyn2 0 0.004225 0.0028361 0.0028361 v SpecHeat 1017.2 1017.2 1017.2 1017.2 v ThermalCond 0.2 1 0.6 0.6 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 4.8224e-06 10 2.5431 2.5431 v Boundary Density 0.97963 1 0.99782 0.99782 v Yplus 0.00074416 5.2679 0.93952 0.93952 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.0366 1.105 0.15823 0.15823 INSTANT 0.535000000E+02 TIME STEP NUMBER 535 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 20800 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00 Friction velocity uet : 0.17461E-05 0.19497E-01 Friction velocity uk : 0.17461E-05 0.19497E-01 Dimensionless distance yplus : 0.47706E-03 0.52664E+01 Friction thermal sca. tstar : -0.38879E+04 0.36059E+04 Rough dim-less th. sca. tplus : 0.88804E-05 0.49017E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 20800 Total number of wall faces : 20800 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.16570E-04 2 0.64730E-05 0.26112E-08 0.10080E-01 c Velocity[X] 0.47931E-09 c Velocity[Y] 0.21319E-08 c Velocity[Z] 0.40829E-13 c Pressure 0.19960E-07 7 0.93971E-05 0.19445E-02 0.30465E-01 c TempC 0.43975E+01 2 0.82347E-05 0.10229E-03 0.80380E-02 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a TempC ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.019593 0.031175 1.603e-05 1.603e-05 v Velocity[Y] -0.041065 0.10262 0.00012443 0.00012443 v Velocity[Z] -2.6923e-06 2.0468e-06 -2.2403e-08 -2.2403e-08 v ǁVelocityǁ 5.8409e-09 0.10262 0.0075854 0.0075854 v Pressure -0.011316 0.038018 8.9262e-18 -1.3129e-18 v TempC 5.0812e-06 9.9058 2.5172 2.5172 v Density 0.97962 1 0.99784 0.99784 v TurbVisc 0 1.1819e-05 9.1988e-08 9.1988e-08 v CourantNb 6.207e-09 1.0304 0.085953 0.085953 v FourierNb 0.0366 0.090627 0.072219 0.072219 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Csdyn2 0 0.004225 0.0028368 0.0028368 v SpecHeat 1017.2 1017.2 1017.2 1017.2 v ThermalCond 0.2 1 0.6 0.6 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 4.9498e-06 10 2.5453 2.5453 v Boundary Density 0.97962 1 0.99781 0.99781 v Yplus 0.00047706 5.2664 0.93897 0.93897 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.0366 1.1044 0.15817 0.15817 INSTANT 0.536000000E+02 TIME STEP NUMBER 536 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 20800 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00 Friction velocity uet : 0.21432E-05 0.19491E-01 Friction velocity uk : 0.21432E-05 0.19491E-01 Dimensionless distance yplus : 0.58558E-03 0.52649E+01 Friction thermal sca. tstar : -0.45025E+04 0.40780E+04 Rough dim-less th. sca. tplus : 0.10900E-04 0.49003E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 20800 Total number of wall faces : 20800 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.16561E-04 2 0.62657E-05 0.25941E-08 0.10052E-01 c Velocity[X] 0.47484E-09 c Velocity[Y] 0.21192E-08 c Velocity[Z] 0.33637E-13 c Pressure 0.19899E-07 7 0.93178E-05 0.19365E-02 0.30366E-01 c TempC 0.43988E+01 3 0.88008E-06 0.10224E-03 0.80329E-02 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a TempC ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.019595 0.031133 1.6038e-05 1.6038e-05 v Velocity[Y] -0.04108 0.10256 0.00012453 0.00012453 v Velocity[Z] -2.1232e-06 1.8555e-06 -2.0765e-08 -2.0765e-08 v ǁVelocityǁ 8.7463e-09 0.10256 0.0075806 0.0075806 v Pressure -0.011346 0.038083 1.2479e-17 1.8635e-18 v TempC 5.2138e-06 9.9059 2.5194 2.5194 v Density 0.97961 1 0.99783 0.99783 v TurbVisc 0 1.1821e-05 9.2007e-08 9.2007e-08 v CourantNb 7.4944e-09 1.0298 0.085891 0.085891 v FourierNb 0.0366 0.090629 0.07222 0.07222 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Csdyn2 0 0.004225 0.0028377 0.0028377 v SpecHeat 1017.2 1017.2 1017.2 1017.2 v ThermalCond 0.2 1 0.6 0.6 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 5.0812e-06 10 2.5475 2.5475 v Boundary Density 0.97961 1 0.99781 0.99781 v Yplus 0.00058558 5.2649 0.93844 0.93844 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.0366 1.1038 0.15811 0.15811 INSTANT 0.537000000E+02 TIME STEP NUMBER 537 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 20800 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00 Friction velocity uet : 0.18456E-05 0.19486E-01 Friction velocity uk : 0.18456E-05 0.19486E-01 Dimensionless distance yplus : 0.50426E-03 0.52635E+01 Friction thermal sca. tstar : -0.50281E+04 0.46486E+04 Rough dim-less th. sca. tplus : 0.93866E-05 0.48989E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 20800 Total number of wall faces : 20800 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.16553E-04 2 0.58109E-05 0.25760E-08 0.10022E-01 c Velocity[X] 0.46991E-09 c Velocity[Y] 0.21061E-08 c Velocity[Z] 0.27740E-13 c Pressure 0.19831E-07 7 0.92518E-05 0.19279E-02 0.30269E-01 c TempC 0.44001E+01 2 0.74828E-05 0.10186E-03 0.80152E-02 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a TempC ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.019596 0.031091 1.6046e-05 1.6046e-05 v Velocity[Y] -0.041094 0.1025 0.00012462 0.00012462 v Velocity[Z] -2.4882e-06 1.6824e-06 -1.9248e-08 -1.9248e-08 v ǁVelocityǁ 8.121e-09 0.10251 0.0075758 0.0075758 v Pressure -0.011377 0.038148 1.3767e-17 3.5575e-18 v TempC 5.3578e-06 9.906 2.5217 2.5217 v Density 0.9796 1 0.99783 0.99783 v TurbVisc 0 1.1823e-05 9.2011e-08 9.2011e-08 v CourantNb 9.1711e-09 1.0292 0.08583 0.08583 v FourierNb 0.0366 0.090632 0.07222 0.07222 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Csdyn2 0 0.004225 0.0028389 0.0028389 v SpecHeat 1017.2 1017.2 1017.2 1017.2 v ThermalCond 0.2 1 0.6 0.6 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 5.2138e-06 10 2.5497 2.5497 v Boundary Density 0.9796 1 0.9978 0.9978 v Yplus 0.00050426 5.2635 0.93791 0.93791 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.0366 1.1032 0.15805 0.15805 INSTANT 0.538000000E+02 TIME STEP NUMBER 538 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 20800 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00 Friction velocity uet : 0.22189E-05 0.19480E-01 Friction velocity uk : 0.22189E-05 0.19480E-01 Dimensionless distance yplus : 0.60626E-03 0.52620E+01 Friction thermal sca. tstar : -0.52165E+04 0.53560E+04 Rough dim-less th. sca. tplus : 0.11285E-04 0.48975E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 20800 Total number of wall faces : 20800 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.16544E-04 2 0.54391E-05 0.25542E-08 0.99849E-02 c Velocity[X] 0.46459E-09 c Velocity[Y] 0.20896E-08 c Velocity[Z] 0.22898E-13 c Pressure 0.19698E-07 7 0.91964E-05 0.19130E-02 0.30191E-01 c TempC 0.44014E+01 2 0.54881E-05 0.10160E-03 0.80020E-02 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a TempC ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.019597 0.031047 1.6054e-05 1.6054e-05 v Velocity[Y] -0.041108 0.10245 0.00012471 0.00012471 v Velocity[Z] -2.2065e-06 1.5257e-06 -1.7843e-08 -1.7843e-08 v ǁVelocityǁ 8.2653e-09 0.10245 0.007571 0.007571 v Pressure -0.011408 0.038213 7.9048e-18 -2.4564e-18 v TempC 5.5048e-06 9.9061 2.5239 2.5239 v Density 0.97958 1 0.99782 0.99782 v TurbVisc 0 1.1824e-05 9.2049e-08 9.2049e-08 v CourantNb 8.4012e-09 1.0286 0.085768 0.085768 v FourierNb 0.0366 0.090634 0.072221 0.072221 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Csdyn2 0 0.004225 0.0028406 0.0028406 v SpecHeat 1017.2 1017.2 1017.2 1017.2 v ThermalCond 0.2 1 0.6 0.6 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 5.3578e-06 10 2.5519 2.5519 v Boundary Density 0.97958 1 0.9978 0.9978 v Yplus 0.00060626 5.262 0.9374 0.9374 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.0366 1.1026 0.15799 0.15799 INSTANT 0.539000000E+02 TIME STEP NUMBER 539 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 20800 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00 Friction velocity uet : 0.27417E-05 0.19475E-01 Friction velocity uk : 0.27417E-05 0.19475E-01 Dimensionless distance yplus : 0.74911E-03 0.52605E+01 Friction thermal sca. tstar : -0.50701E+04 0.62617E+04 Rough dim-less th. sca. tplus : 0.13944E-04 0.48961E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 20800 Total number of wall faces : 20800 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.16535E-04 2 0.51791E-05 0.25394E-08 0.99612E-02 c Velocity[X] 0.45993E-09 c Velocity[Y] 0.20794E-08 c Velocity[Z] 0.18918E-13 c Pressure 0.19719E-07 7 0.91082E-05 0.19131E-02 0.30097E-01 c TempC 0.44027E+01 2 0.73398E-05 0.10132E-03 0.79883E-02 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a TempC ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.019598 0.031003 1.6062e-05 1.6062e-05 v Velocity[Y] -0.041122 0.10239 0.0001248 0.0001248 v Velocity[Z] -1.5172e-06 1.3838e-06 -1.6541e-08 -1.6541e-08 v ǁVelocityǁ 8.2166e-09 0.10239 0.0075662 0.0075662 v Pressure -0.011439 0.038278 7.2831e-18 -3.134e-18 v TempC 5.6593e-06 9.9062 2.5261 2.5261 v Density 0.97957 1 0.99782 0.99782 v TurbVisc 0 1.1826e-05 9.2057e-08 9.2057e-08 v CourantNb 8.0649e-09 1.028 0.085706 0.085706 v FourierNb 0.0366 0.090636 0.072221 0.072221 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Csdyn2 0 0.004225 0.0028416 0.0028416 v SpecHeat 1017.2 1017.2 1017.2 1017.2 v ThermalCond 0.2 1 0.6 0.6 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 5.5048e-06 10 2.5541 2.5541 v Boundary Density 0.97957 1 0.99779 0.99779 v Yplus 0.00074911 5.2605 0.9369 0.9369 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.0366 1.102 0.15793 0.15793 INSTANT 0.540000000E+02 TIME STEP NUMBER 540 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 20800 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00 Friction velocity uet : 0.25864E-05 0.19469E-01 Friction velocity uk : 0.25864E-05 0.19469E-01 Dimensionless distance yplus : 0.70665E-03 0.52590E+01 Friction thermal sca. tstar : -0.48116E+04 0.74755E+04 Rough dim-less th. sca. tplus : 0.13154E-04 0.48947E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 20800 Total number of wall faces : 20800 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.16526E-04 2 0.49881E-05 0.25238E-08 0.99358E-02 c Velocity[X] 0.45525E-09 c Velocity[Y] 0.20685E-08 c Velocity[Z] 0.15643E-13 c Pressure 0.19676E-07 7 0.90385E-05 0.19071E-02 0.30002E-01 c TempC 0.44040E+01 2 0.67313E-05 0.10106E-03 0.79751E-02 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a TempC ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.019599 0.030958 1.6069e-05 1.6069e-05 v Velocity[Y] -0.041135 0.10233 0.00012489 0.00012489 v Velocity[Z] -1.3106e-06 1.4037e-06 -1.5335e-08 -1.5335e-08 v ǁVelocityǁ 6.2513e-09 0.10233 0.0075614 0.0075614 v Pressure -0.01147 0.038342 1.0481e-17 -2.5411e-19 v TempC 5.7953e-06 9.9063 2.5284 2.5284 v Density 0.97956 1 0.99781 0.99781 v TurbVisc 0 1.1827e-05 9.2078e-08 9.2078e-08 v CourantNb 8.0307e-09 1.0274 0.085645 0.085645 v FourierNb 0.0366 0.090639 0.072222 0.072222 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Csdyn2 0 0.004225 0.0028434 0.0028434 v SpecHeat 1017.2 1017.2 1017.2 1017.2 v ThermalCond 0.2 1 0.6 0.6 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 5.6593e-06 10 2.5563 2.5563 v Boundary Density 0.97956 1 0.99779 0.99779 v Yplus 0.00070665 5.259 0.93641 0.93641 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.0366 1.1015 0.15787 0.15787 INSTANT 0.541000000E+02 TIME STEP NUMBER 541 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 20800 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00 Friction velocity uet : 0.33190E-05 0.19464E-01 Friction velocity uk : 0.33190E-05 0.19464E-01 Dimensionless distance yplus : 0.90683E-03 0.52574E+01 Friction thermal sca. tstar : -0.45708E+04 0.92084E+04 Rough dim-less th. sca. tplus : 0.16880E-04 0.48933E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 20800 Total number of wall faces : 20800 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.16517E-04 2 0.47357E-05 0.25091E-08 0.99122E-02 c Velocity[X] 0.45067E-09 c Velocity[Y] 0.20584E-08 c Velocity[Z] 0.12945E-13 c Pressure 0.19616E-07 7 0.89671E-05 0.18993E-02 0.29911E-01 c TempC 0.44053E+01 2 0.82474E-05 0.10074E-03 0.79598E-02 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a TempC ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.019601 0.030913 1.6076e-05 1.6076e-05 v Velocity[Y] -0.041148 0.10227 0.00012498 0.00012498 v Velocity[Z] -1.2228e-06 1.1391e-06 -1.4218e-08 -1.4218e-08 v ǁVelocityǁ 4.7512e-09 0.10227 0.0075566 0.0075566 v Pressure -0.011501 0.038407 1.3856e-17 3.134e-18 v TempC 5.928e-06 9.9065 2.5306 2.5306 v Density 0.97954 1 0.99781 0.99781 v TurbVisc 0 1.1828e-05 9.204e-08 9.204e-08 v CourantNb 8.1964e-09 1.0268 0.085583 0.085583 v FourierNb 0.0366 0.090641 0.072222 0.072222 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Csdyn2 0 0.004225 0.0028442 0.0028442 v SpecHeat 1017.2 1017.2 1017.2 1017.2 v ThermalCond 0.2 1 0.6 0.6 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 5.7953e-06 10 2.5585 2.5585 v Boundary Density 0.97954 1 0.99778 0.99778 v Yplus 0.00090683 5.2574 0.93592 0.93592 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.0366 1.1009 0.15781 0.15781 INSTANT 0.542000000E+02 TIME STEP NUMBER 542 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 20800 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00 Friction velocity uet : 0.13802E-05 0.19458E-01 Friction velocity uk : 0.13802E-05 0.19458E-01 Dimensionless distance yplus : 0.37709E-03 0.52559E+01 Friction thermal sca. tstar : -0.43824E+04 0.11900E+05 Rough dim-less th. sca. tplus : 0.70195E-05 0.48919E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 20800 Total number of wall faces : 20800 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.16509E-04 2 0.45286E-05 0.24940E-08 0.98875E-02 c Velocity[X] 0.44608E-09 c Velocity[Y] 0.20479E-08 c Velocity[Z] 0.10720E-13 c Pressure 0.19531E-07 7 0.88985E-05 0.18892E-02 0.29818E-01 c TempC 0.44066E+01 2 0.83924E-05 0.10047E-03 0.79462E-02 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a TempC ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.019602 0.030867 1.6084e-05 1.6084e-05 v Velocity[Y] -0.041161 0.10221 0.00012507 0.00012507 v Velocity[Z] -1.5075e-06 1.0338e-06 -1.3183e-08 -1.3183e-08 v ǁVelocityǁ 3.6849e-09 0.10221 0.0075518 0.0075518 v Pressure -0.011532 0.038472 7.6383e-18 -3.2187e-18 v TempC 6.0661e-06 9.9066 2.5328 2.5328 v Density 0.97953 1 0.9978 0.9978 v TurbVisc 0 1.1829e-05 9.201e-08 9.201e-08 v CourantNb 8.4837e-09 1.0263 0.085522 0.085522 v FourierNb 0.0366 0.090643 0.072222 0.072222 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Csdyn2 0 0.004225 0.0028459 0.0028459 v SpecHeat 1017.2 1017.2 1017.2 1017.2 v ThermalCond 0.2 1 0.6 0.6 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 5.928e-06 10 2.5607 2.5607 v Boundary Density 0.97953 1 0.99778 0.99778 v Yplus 0.00037709 5.2559 0.93545 0.93545 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.0366 1.1003 0.15774 0.15774 INSTANT 0.543000000E+02 TIME STEP NUMBER 543 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 20800 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00 Friction velocity uet : 0.20788E-05 0.19453E-01 Friction velocity uk : 0.20788E-05 0.19453E-01 Dimensionless distance yplus : 0.56797E-03 0.52543E+01 Friction thermal sca. tstar : -0.44435E+04 0.15998E+05 Rough dim-less th. sca. tplus : 0.10573E-04 0.48904E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 20800 Total number of wall faces : 20800 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.16500E-04 2 0.43706E-05 0.24787E-08 0.98625E-02 c Velocity[X] 0.44147E-09 c Velocity[Y] 0.20372E-08 c Velocity[Z] 0.88843E-14 c Pressure 0.19463E-07 7 0.88275E-05 0.18807E-02 0.29724E-01 c TempC 0.44079E+01 3 0.10696E-05 0.10035E-03 0.79390E-02 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a TempC ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.019603 0.030822 1.6091e-05 1.6091e-05 v Velocity[Y] -0.041173 0.10215 0.00012516 0.00012516 v Velocity[Z] -1.4554e-06 9.3844e-07 -1.2224e-08 -1.2224e-08 v ǁVelocityǁ 3.0268e-09 0.10215 0.007547 0.007547 v Pressure -0.011563 0.038536 1.1902e-17 1.1858e-18 v TempC 6.2029e-06 9.9067 2.535 2.535 v Density 0.97952 1 0.9978 0.9978 v TurbVisc 0 1.1831e-05 9.1984e-08 9.1984e-08 v CourantNb 6.7671e-09 1.0257 0.08546 0.08546 v FourierNb 0.0366 0.090645 0.072223 0.072223 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Csdyn2 0 0.004225 0.002848 0.002848 v SpecHeat 1017.2 1017.2 1017.2 1017.2 v ThermalCond 0.2 1 0.6 0.6 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 6.0661e-06 10 2.5629 2.5629 v Boundary Density 0.97952 1 0.99777 0.99777 v Yplus 0.00056797 5.2543 0.93498 0.93498 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.0366 1.0997 0.15768 0.15768 INSTANT 0.544000000E+02 TIME STEP NUMBER 544 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 20800 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00 Friction velocity uet : 0.19209E-05 0.19447E-01 Friction velocity uk : 0.19209E-05 0.19447E-01 Dimensionless distance yplus : 0.52484E-03 0.52528E+01 Friction thermal sca. tstar : -0.46727E+04 0.17315E+05 Rough dim-less th. sca. tplus : 0.97697E-05 0.48890E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 20800 Total number of wall faces : 20800 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.16491E-04 2 0.42299E-05 0.24631E-08 0.98367E-02 c Velocity[X] 0.43686E-09 c Velocity[Y] 0.20263E-08 c Velocity[Z] 0.73681E-14 c Pressure 0.19388E-07 7 0.87588E-05 0.18716E-02 0.29629E-01 c TempC 0.44091E+01 2 0.74233E-05 0.10001E-03 0.79225E-02 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a TempC ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.019604 0.030776 1.6098e-05 1.6098e-05 v Velocity[Y] -0.041186 0.10209 0.00012525 0.00012525 v Velocity[Z] -1.057e-06 8.5208e-07 -1.1335e-08 -1.1335e-08 v ǁVelocityǁ 2.7221e-09 0.10209 0.0075422 0.0075422 v Pressure -0.011594 0.038601 1.2346e-17 2.0329e-18 v TempC 6.3512e-06 9.9068 2.5373 2.5373 v Density 0.9795 1 0.99779 0.99779 v TurbVisc 0 1.1832e-05 9.1935e-08 9.1935e-08 v CourantNb 5.1077e-09 1.0251 0.085399 0.085399 v FourierNb 0.0366 0.090648 0.072223 0.072223 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Csdyn2 0 0.004225 0.002848 0.002848 v SpecHeat 1017.2 1017.2 1017.2 1017.2 v ThermalCond 0.2 1 0.6 0.6 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 6.2029e-06 10 2.5651 2.5651 v Boundary Density 0.9795 1 0.99777 0.99777 v Yplus 0.00052484 5.2528 0.93452 0.93452 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.0366 1.0992 0.15762 0.15762 INSTANT 0.545000000E+02 TIME STEP NUMBER 545 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 20800 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00 Friction velocity uet : 0.16835E-05 0.19441E-01 Friction velocity uk : 0.16835E-05 0.19441E-01 Dimensionless distance yplus : 0.45997E-03 0.52512E+01 Friction thermal sca. tstar : -0.46814E+04 0.14557E+05 Rough dim-less th. sca. tplus : 0.85623E-05 0.48875E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 20800 Total number of wall faces : 20800 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.16482E-04 2 0.40963E-05 0.24431E-08 0.98018E-02 c Velocity[X] 0.43178E-09 c Velocity[Y] 0.20113E-08 c Velocity[Z] 0.61149E-14 c Pressure 0.19217E-07 7 0.87038E-05 0.18533E-02 0.29547E-01 c TempC 0.44104E+01 2 0.75985E-05 0.99731E-04 0.79087E-02 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a TempC ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.019606 0.030731 1.6105e-05 1.6105e-05 v Velocity[Y] -0.041198 0.10203 0.00012534 0.00012534 v Velocity[Z] -8.8749e-07 1.0241e-06 -1.0512e-08 -1.0512e-08 v ǁVelocityǁ 2.6646e-09 0.10203 0.0075374 0.0075374 v Pressure -0.011625 0.038665 1.2612e-17 2.2446e-18 v TempC 6.503e-06 9.9069 2.5395 2.5395 v Density 0.97949 1 0.99779 0.99779 v TurbVisc 0 1.1833e-05 9.1886e-08 9.1886e-08 v CourantNb 3.768e-09 1.0245 0.085338 0.085338 v FourierNb 0.0366 0.09065 0.072223 0.072223 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Csdyn2 0 0.004225 0.002848 0.002848 v SpecHeat 1017.2 1017.2 1017.2 1017.2 v ThermalCond 0.2 1 0.6 0.6 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 6.3512e-06 10 2.5673 2.5673 v Boundary Density 0.97949 1 0.99776 0.99776 v Yplus 0.00045997 5.2512 0.93406 0.93406 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.0366 1.0986 0.15756 0.15756 INSTANT 0.546000000E+02 TIME STEP NUMBER 546 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 20800 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00 Friction velocity uet : 0.21292E-05 0.19436E-01 Friction velocity uk : 0.21292E-05 0.19436E-01 Dimensionless distance yplus : 0.58175E-03 0.52498E+01 Friction thermal sca. tstar : -0.45759E+04 0.12617E+05 Rough dim-less th. sca. tplus : 0.10829E-04 0.48861E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 20800 Total number of wall faces : 20800 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.16473E-04 2 0.40280E-05 0.24299E-08 0.97806E-02 c Velocity[X] 0.42736E-09 c Velocity[Y] 0.20025E-08 c Velocity[Z] 0.50782E-14 c Pressure 0.19219E-07 7 0.86199E-05 0.18517E-02 0.29458E-01 c TempC 0.44117E+01 2 0.91875E-05 0.99382E-04 0.78921E-02 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a TempC ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.019607 0.030686 1.6112e-05 1.6112e-05 v Velocity[Y] -0.041209 0.10197 0.00012543 0.00012543 v Velocity[Z] -8.1115e-07 9.0576e-07 -9.7486e-09 -9.7486e-09 v ǁVelocityǁ 2.7339e-09 0.10197 0.0075327 0.0075327 v Pressure -0.011656 0.03873 1.4611e-17 3.6846e-18 v TempC 6.6598e-06 9.907 2.5417 2.5417 v Density 0.97948 1 0.99778 0.99778 v TurbVisc 0 1.1834e-05 9.1842e-08 9.1842e-08 v CourantNb 2.692e-09 1.0239 0.085276 0.085276 v FourierNb 0.0366 0.090652 0.072223 0.072223 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Csdyn2 0 0.004225 0.0028484 0.0028484 v SpecHeat 1017.2 1017.2 1017.2 1017.2 v ThermalCond 0.2 1 0.6 0.6 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 6.503e-06 10 2.5695 2.5695 v Boundary Density 0.97948 1 0.99776 0.99776 v Yplus 0.00058175 5.2498 0.93362 0.93362 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.0366 1.098 0.1575 0.1575 INSTANT 0.547000000E+02 TIME STEP NUMBER 547 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 20800 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00 Friction velocity uet : 0.23401E-05 0.19430E-01 Friction velocity uk : 0.23401E-05 0.19430E-01 Dimensionless distance yplus : 0.63937E-03 0.52483E+01 Friction thermal sca. tstar : -0.44314E+04 0.11491E+05 Rough dim-less th. sca. tplus : 0.11902E-04 0.48848E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 20800 Total number of wall faces : 20800 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.16464E-04 2 0.39754E-05 0.24162E-08 0.97583E-02 c Velocity[X] 0.42292E-09 c Velocity[Y] 0.19933E-08 c Velocity[Z] 0.42201E-14 c Pressure 0.19194E-07 7 0.85531E-05 0.18474E-02 0.29363E-01 c TempC 0.44130E+01 2 0.73387E-05 0.99111E-04 0.78786E-02 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a TempC ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.019608 0.03064 1.6118e-05 1.6118e-05 v Velocity[Y] -0.041221 0.10191 0.00012551 0.00012551 v Velocity[Z] -8.1742e-07 6.5927e-07 -9.0415e-09 -9.0415e-09 v ǁVelocityǁ 2.8425e-09 0.10191 0.0075279 0.0075279 v Pressure -0.011687 0.038794 4.7962e-18 -6.3104e-18 v TempC 6.8204e-06 9.9071 2.5439 2.5439 v Density 0.97946 1 0.99778 0.99778 v TurbVisc 0 1.1835e-05 9.18e-08 9.18e-08 v CourantNb 1.8329e-09 1.0234 0.085215 0.085215 v FourierNb 0.0366 0.090654 0.072223 0.072223 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Csdyn2 0 0.004225 0.0028488 0.0028488 v SpecHeat 1017.2 1017.2 1017.2 1017.2 v ThermalCond 0.2 1 0.6 0.6 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 6.6598e-06 10 2.5717 2.5717 v Boundary Density 0.97946 1 0.99775 0.99775 v Yplus 0.00063937 5.2483 0.93318 0.93318 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.0366 1.0974 0.15744 0.15744 INSTANT 0.548000000E+02 TIME STEP NUMBER 548 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 20800 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00 Friction velocity uet : 0.21027E-05 0.19424E-01 Friction velocity uk : 0.21027E-05 0.19424E-01 Dimensionless distance yplus : 0.57450E-03 0.52468E+01 Friction thermal sca. tstar : -0.43130E+04 0.10816E+05 Rough dim-less th. sca. tplus : 0.10694E-04 0.48834E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 20800 Total number of wall faces : 20800 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.16455E-04 2 0.39387E-05 0.24016E-08 0.97338E-02 c Velocity[X] 0.41839E-09 c Velocity[Y] 0.19832E-08 c Velocity[Z] 0.35092E-14 c Pressure 0.19154E-07 7 0.84857E-05 0.18418E-02 0.29266E-01 c TempC 0.44143E+01 2 0.95392E-05 0.98788E-04 0.78630E-02 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a TempC ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.019609 0.030595 1.6125e-05 1.6125e-05 v Velocity[Y] -0.041232 0.10185 0.0001256 0.0001256 v Velocity[Z] -8.3799e-07 5.946e-07 -8.3861e-09 -8.3861e-09 v ǁVelocityǁ 2.9434e-09 0.10185 0.0075231 0.0075231 v Pressure -0.011719 0.038858 6.2617e-18 -3.9387e-18 v TempC 6.9877e-06 9.9073 2.5461 2.5461 v Density 0.97945 1 0.99777 0.99777 v TurbVisc 0 1.1835e-05 9.1769e-08 9.1769e-08 v CourantNb 1.152e-09 1.0228 0.085154 0.085154 v FourierNb 0.0366 0.090656 0.072224 0.072224 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Csdyn2 0 0.004225 0.00285 0.00285 v SpecHeat 1017.2 1017.2 1017.2 1017.2 v ThermalCond 0.2 1 0.6 0.6 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 6.8204e-06 10 2.5739 2.5739 v Boundary Density 0.97945 1 0.99775 0.99775 v Yplus 0.0005745 5.2468 0.93274 0.93274 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.0366 1.0968 0.15738 0.15738 INSTANT 0.549000000E+02 TIME STEP NUMBER 549 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 20800 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00 Friction velocity uet : 0.18401E-05 0.19419E-01 Friction velocity uk : 0.18401E-05 0.19419E-01 Dimensionless distance yplus : 0.50276E-03 0.52453E+01 Friction thermal sca. tstar : -0.42112E+04 0.10403E+05 Rough dim-less th. sca. tplus : 0.93587E-05 0.48820E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 20800 Total number of wall faces : 20800 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.16446E-04 2 0.39040E-05 0.23864E-08 0.97082E-02 c Velocity[X] 0.41384E-09 c Velocity[Y] 0.19725E-08 c Velocity[Z] 0.29199E-14 c Pressure 0.19084E-07 7 0.84214E-05 0.18332E-02 0.29173E-01 c TempC 0.44156E+01 2 0.42155E-05 0.98581E-04 0.78521E-02 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a TempC ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.01961 0.03055 1.6132e-05 1.6132e-05 v Velocity[Y] -0.041245 0.1018 0.00012569 0.00012569 v Velocity[Z] -6.2011e-07 5.6274e-07 -7.7787e-09 -7.7787e-09 v ǁVelocityǁ 3.0162e-09 0.1018 0.0075184 0.0075184 v Pressure -0.01175 0.038922 9.992e-18 -8.0468e-19 v TempC 7.1584e-06 9.9074 2.5483 2.5483 v Density 0.97944 1 0.99777 0.99777 v TurbVisc 0 1.1836e-05 9.1727e-08 9.1727e-08 v CourantNb 6.172e-10 1.0222 0.085093 0.085093 v FourierNb 0.0366 0.090658 0.072224 0.072224 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Csdyn2 0 0.004225 0.0028503 0.0028503 v SpecHeat 1017.2 1017.2 1017.2 1017.2 v ThermalCond 0.2 1 0.6 0.6 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 6.9877e-06 10 2.5761 2.5761 v Boundary Density 0.97944 1 0.99774 0.99774 v Yplus 0.00050276 5.2453 0.93232 0.93232 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.0366 1.0962 0.15732 0.15732 INSTANT 0.550000000E+02 TIME STEP NUMBER 550 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 20800 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00 Friction velocity uet : 0.15910E-05 0.19413E-01 Friction velocity uk : 0.15910E-05 0.19413E-01 Dimensionless distance yplus : 0.43471E-03 0.52438E+01 Friction thermal sca. tstar : -0.41490E+04 0.10159E+05 Rough dim-less th. sca. tplus : 0.80920E-05 0.48806E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 20800 Total number of wall faces : 20800 ------------------------------------------------------------ Write intermediate restart files checkpoint at iteration 550, Physical time 0.55000E+02 ** Writing the main restart file ----------------------------- Start writing Wrote field names and types to checkpoint at iteration 550: checkpoint/main End writing the options Wrote main variables to checkpoint: checkpoint/main End writing ** Writing the auxiliary restart file ---------------------------------- Start writing End writing the dimensions and options End writing the physical properties End writing the time step Wrote boundary condition coefficients to checkpoint: checkpoint/auxiliary End writing the source terms End writing ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.16438E-04 2 0.38769E-05 0.23711E-08 0.96824E-02 c Velocity[X] 0.40926E-09 c Velocity[Y] 0.19618E-08 c Velocity[Z] 0.24311E-14 c Pressure 0.19033E-07 7 0.83548E-05 0.18265E-02 0.29082E-01 c TempC 0.44168E+01 2 0.55413E-05 0.98460E-04 0.78445E-02 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a TempC ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.019612 0.030505 1.6138e-05 1.6138e-05 v Velocity[Y] -0.041257 0.10174 0.00012577 0.00012577 v Velocity[Z] -5.4667e-07 7.4147e-07 -7.2158e-09 -7.2158e-09 v ǁVelocityǁ 2.26e-09 0.10174 0.0075136 0.0075136 v Pressure -0.011781 0.038987 1.1768e-17 1.2705e-18 v TempC 7.337e-06 9.9074 2.5506 2.5506 v Density 0.97943 1 0.99776 0.99776 v TurbVisc 0 1.1837e-05 9.1686e-08 9.1686e-08 v CourantNb 2.0168e-10 1.0216 0.085032 0.085032 v FourierNb 0.0366 0.09066 0.072224 0.072224 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Csdyn2 0 0.004225 0.0028507 0.0028507 v SpecHeat 1017.2 1017.2 1017.2 1017.2 v ThermalCond 0.2 1 0.6 0.6 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 7.1584e-06 10 2.5783 2.5783 v Boundary Density 0.97943 1 0.99773 0.99773 v Yplus 0.00043471 5.2438 0.93189 0.93189 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.0366 1.0956 0.15726 0.15726 INSTANT 0.551000000E+02 TIME STEP NUMBER 551 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 20800 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00 Friction velocity uet : 0.13608E-05 0.19407E-01 Friction velocity uk : 0.13608E-05 0.19407E-01 Dimensionless distance yplus : 0.37180E-03 0.52423E+01 Friction thermal sca. tstar : -0.41042E+04 0.10031E+05 Rough dim-less th. sca. tplus : 0.69210E-05 0.48792E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 20800 Total number of wall faces : 20800 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.16429E-04 2 0.38406E-05 0.23562E-08 0.96570E-02 c Velocity[X] 0.40476E-09 c Velocity[Y] 0.19514E-08 c Velocity[Z] 0.20253E-14 c Pressure 0.18961E-07 7 0.82919E-05 0.18179E-02 0.28993E-01 c TempC 0.44181E+01 2 0.68187E-05 0.98199E-04 0.78314E-02 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a TempC ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.019613 0.03046 1.6145e-05 1.6145e-05 v Velocity[Y] -0.041269 0.10168 0.00012586 0.00012586 v Velocity[Z] -4.9132e-07 7.2015e-07 -6.694e-09 -6.694e-09 v ǁVelocityǁ 1.6363e-09 0.10168 0.0075089 0.0075089 v Pressure -0.011813 0.039051 1.1813e-17 1.3976e-18 v TempC 7.5237e-06 9.9076 2.5528 2.5528 v Density 0.97941 1 0.99776 0.99776 v TurbVisc 0 1.1838e-05 9.1645e-08 9.1645e-08 v CourantNb 1.1725e-10 1.021 0.084972 0.084972 v FourierNb 0.0366 0.090662 0.072224 0.072224 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Csdyn2 0 0.004225 0.0028511 0.0028511 v SpecHeat 1017.2 1017.2 1017.2 1017.2 v ThermalCond 0.2 1 0.6 0.6 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 7.337e-06 10 2.5805 2.5805 v Boundary Density 0.97941 1 0.99773 0.99773 v Yplus 0.0003718 5.2423 0.93147 0.93147 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.0366 1.095 0.1572 0.1572 INSTANT 0.552000000E+02 TIME STEP NUMBER 552 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 20800 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00 Friction velocity uet : 0.77415E-06 0.19402E-01 Friction velocity uk : 0.77415E-06 0.19402E-01 Dimensionless distance yplus : 0.21152E-03 0.52408E+01 Friction thermal sca. tstar : -0.41322E+04 0.17055E+05 Rough dim-less th. sca. tplus : 0.39373E-05 0.48778E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 20800 Total number of wall faces : 20800 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.16420E-04 2 0.38107E-05 0.23435E-08 0.96362E-02 c Velocity[X] 0.40051E-09 c Velocity[Y] 0.19430E-08 c Velocity[Z] 0.16883E-14 c Pressure 0.18921E-07 7 0.82281E-05 0.18123E-02 0.28916E-01 c TempC 0.44194E+01 2 0.72270E-05 0.97956E-04 0.78190E-02 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a TempC ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.019614 0.030414 1.6151e-05 1.6151e-05 v Velocity[Y] -0.041281 0.10162 0.00012595 0.00012595 v Velocity[Z] -4.4414e-07 5.1818e-07 -6.2104e-09 -6.2104e-09 v ǁVelocityǁ 1.291e-09 0.10162 0.0075041 0.0075041 v Pressure -0.011844 0.039115 1.4921e-17 4.3622e-18 v TempC 7.716e-06 9.9077 2.555 2.555 v Density 0.9794 1 0.99775 0.99775 v TurbVisc 0 1.1839e-05 9.1602e-08 9.1602e-08 v CourantNb 3.5654e-10 1.0204 0.084911 0.084911 v FourierNb 0.0366 0.090664 0.072225 0.072225 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Csdyn2 0 0.004225 0.0028514 0.0028514 v SpecHeat 1017.2 1017.2 1017.2 1017.2 v ThermalCond 0.2 1 0.6 0.6 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 7.5237e-06 10 2.5827 2.5827 v Boundary Density 0.9794 1 0.99772 0.99772 v Yplus 0.00021152 5.2408 0.93106 0.93106 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.0366 1.0944 0.15714 0.15714 INSTANT 0.553000000E+02 TIME STEP NUMBER 553 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 20800 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00 Friction velocity uet : 0.95114E-06 0.19396E-01 Friction velocity uk : 0.95114E-06 0.19396E-01 Dimensionless distance yplus : 0.25988E-03 0.52393E+01 Friction thermal sca. tstar : -0.42901E+04 0.10294E+05 Rough dim-less th. sca. tplus : 0.48375E-05 0.48764E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 20800 Total number of wall faces : 20800 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.16411E-04 2 0.37810E-05 0.23317E-08 0.96173E-02 c Velocity[X] 0.39638E-09 c Velocity[Y] 0.19354E-08 c Velocity[Z] 0.14081E-14 c Pressure 0.18903E-07 7 0.81626E-05 0.18088E-02 0.28829E-01 c TempC 0.44207E+01 2 0.86277E-05 0.97639E-04 0.78036E-02 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a TempC ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.019615 0.030369 1.6158e-05 1.6158e-05 v Velocity[Y] -0.041293 0.10156 0.00012603 0.00012603 v Velocity[Z] -4.3379e-07 4.5821e-07 -5.7621e-09 -5.7621e-09 v ǁVelocityǁ 1.2323e-09 0.10156 0.0074993 0.0074993 v Pressure -0.011875 0.039179 3.7303e-18 -6.7763e-18 v TempC 7.9153e-06 9.9078 2.5572 2.5572 v Density 0.97939 1 0.99775 0.99775 v TurbVisc 0 1.1839e-05 9.1555e-08 9.1555e-08 v CourantNb 5.3215e-10 1.0198 0.08485 0.08485 v FourierNb 0.0366 0.090667 0.072225 0.072225 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Csdyn2 0 0.004225 0.0028514 0.0028514 v SpecHeat 1017.2 1017.2 1017.2 1017.2 v ThermalCond 0.2 1 0.6 0.6 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 7.716e-06 10 2.5849 2.5849 v Boundary Density 0.97939 1 0.99772 0.99772 v Yplus 0.00025988 5.2393 0.93065 0.93065 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.0366 1.0938 0.15707 0.15707 INSTANT 0.554000000E+02 TIME STEP NUMBER 554 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 20800 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00 Friction velocity uet : 0.77498E-06 0.19391E-01 Friction velocity uk : 0.77498E-06 0.19391E-01 Dimensionless distance yplus : 0.21174E-03 0.52378E+01 Friction thermal sca. tstar : -0.45009E+04 0.10085E+05 Rough dim-less th. sca. tplus : 0.39415E-05 0.48750E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 20800 Total number of wall faces : 20800 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.16402E-04 2 0.37399E-05 0.23200E-08 0.95981E-02 c Velocity[X] 0.39229E-09 c Velocity[Y] 0.19277E-08 c Velocity[Z] 0.11751E-14 c Pressure 0.18864E-07 7 0.81004E-05 0.18034E-02 0.28740E-01 c TempC 0.44219E+01 2 0.78803E-05 0.97376E-04 0.77905E-02 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a TempC ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.019616 0.030324 1.6164e-05 1.6164e-05 v Velocity[Y] -0.041305 0.10151 0.00012612 0.00012612 v Velocity[Z] -4.1822e-07 3.7558e-07 -5.3466e-09 -5.3466e-09 v ǁVelocityǁ 1.362e-09 0.10151 0.0074946 0.0074946 v Pressure -0.011907 0.039243 1.1013e-17 5.5057e-19 v TempC 8.1199e-06 9.9079 2.5594 2.5594 v Density 0.97937 1 0.99774 0.99774 v TurbVisc 0 1.184e-05 9.1533e-08 9.1533e-08 v CourantNb 6.5655e-10 1.0191 0.084789 0.084789 v FourierNb 0.0366 0.090669 0.072225 0.072225 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Csdyn2 0 0.004225 0.0028529 0.0028529 v SpecHeat 1017.2 1017.2 1017.2 1017.2 v ThermalCond 0.2 1 0.6 0.6 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 7.9153e-06 10 2.5871 2.5871 v Boundary Density 0.97937 1 0.99771 0.99771 v Yplus 0.00021174 5.2378 0.93025 0.93025 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.0366 1.0932 0.15701 0.15701 INSTANT 0.555000000E+02 TIME STEP NUMBER 555 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 20800 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00 Friction velocity uet : 0.63547E-06 0.19385E-01 Friction velocity uk : 0.63547E-06 0.19385E-01 Dimensionless distance yplus : 0.17363E-03 0.52362E+01 Friction thermal sca. tstar : -0.47181E+04 0.10203E+05 Rough dim-less th. sca. tplus : 0.32320E-05 0.48736E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 20800 Total number of wall faces : 20800 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.16393E-04 2 0.37045E-05 0.23077E-08 0.95779E-02 c Velocity[X] 0.38819E-09 c Velocity[Y] 0.19195E-08 c Velocity[Z] 0.98124E-15 c Pressure 0.18821E-07 7 0.80370E-05 0.17975E-02 0.28648E-01 c TempC 0.44232E+01 2 0.95550E-05 0.97024E-04 0.77737E-02 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a TempC ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.019617 0.03028 1.6171e-05 1.6171e-05 v Velocity[Y] -0.041316 0.10145 0.0001262 0.0001262 v Velocity[Z] -3.4706e-07 3.3362e-07 -4.9613e-09 -4.9613e-09 v ǁVelocityǁ 1.5031e-09 0.10145 0.0074898 0.0074898 v Pressure -0.011939 0.039307 1.1546e-17 8.4703e-19 v TempC 8.2995e-06 9.908 2.5616 2.5616 v Density 0.97936 1 0.99774 0.99774 v TurbVisc 0 1.1841e-05 9.1497e-08 9.1497e-08 v CourantNb 7.4006e-10 1.0185 0.084729 0.084729 v FourierNb 0.0366 0.090671 0.072226 0.072226 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Csdyn2 0 0.004225 0.0028533 0.0028533 v SpecHeat 1017.2 1017.2 1017.2 1017.2 v ThermalCond 0.2 1 0.6 0.6 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 8.1199e-06 10 2.5893 2.5893 v Boundary Density 0.97936 1 0.99771 0.99771 v Yplus 0.00017363 5.2362 0.92985 0.92985 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.0366 1.0926 0.15695 0.15695 INSTANT 0.556000000E+02 TIME STEP NUMBER 556 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 20800 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00 Friction velocity uet : 0.56915E-06 0.19380E-01 Friction velocity uk : 0.56915E-06 0.19380E-01 Dimensionless distance yplus : 0.15550E-03 0.52347E+01 Friction thermal sca. tstar : -0.49286E+04 0.10360E+05 Rough dim-less th. sca. tplus : 0.28947E-05 0.48721E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 20800 Total number of wall faces : 20800 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.16384E-04 2 0.36637E-05 0.22950E-08 0.95567E-02 c Velocity[X] 0.38410E-09 c Velocity[Y] 0.19109E-08 c Velocity[Z] 0.81976E-15 c Pressure 0.18753E-07 7 0.79758E-05 0.17893E-02 0.28557E-01 c TempC 0.44245E+01 2 0.48426E-05 0.96832E-04 0.77633E-02 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a TempC ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.019618 0.030235 1.6177e-05 1.6177e-05 v Velocity[Y] -0.041328 0.10139 0.00012629 0.00012629 v Velocity[Z] -3.4654e-07 3.0821e-07 -4.6041e-09 -4.6041e-09 v ǁVelocityǁ 1.6194e-09 0.10139 0.0074851 0.0074851 v Pressure -0.01197 0.039371 1.5721e-17 5.1669e-18 v TempC 8.4768e-06 9.9081 2.5638 2.5638 v Density 0.97935 1 0.99773 0.99773 v TurbVisc 0 1.1841e-05 9.1459e-08 9.1459e-08 v CourantNb 7.9112e-10 1.018 0.084668 0.084668 v FourierNb 0.0366 0.090673 0.072226 0.072226 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Csdyn2 0 0.004225 0.0028537 0.0028537 v SpecHeat 1017.2 1017.2 1017.2 1017.2 v ThermalCond 0.2 1 0.6 0.6 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 8.2995e-06 10 2.5914 2.5914 v Boundary Density 0.97935 1 0.9977 0.9977 v Yplus 0.0001555 5.2347 0.92945 0.92945 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.0366 1.092 0.15689 0.15689 INSTANT 0.557000000E+02 TIME STEP NUMBER 557 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 20800 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00 Friction velocity uet : 0.58224E-06 0.19374E-01 Friction velocity uk : 0.58224E-06 0.19374E-01 Dimensionless distance yplus : 0.15908E-03 0.52331E+01 Friction thermal sca. tstar : -0.51453E+04 0.10550E+05 Rough dim-less th. sca. tplus : 0.29613E-05 0.48707E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 20800 Total number of wall faces : 20800 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.16375E-04 2 0.36299E-05 0.22816E-08 0.95341E-02 c Velocity[X] 0.37995E-09 c Velocity[Y] 0.19017E-08 c Velocity[Z] 0.68521E-15 c Pressure 0.18697E-07 7 0.79130E-05 0.17823E-02 0.28465E-01 c TempC 0.44257E+01 2 0.77020E-05 0.96688E-04 0.77549E-02 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a TempC ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.019619 0.03019 1.6183e-05 1.6183e-05 v Velocity[Y] -0.041339 0.10133 0.00012637 0.00012637 v Velocity[Z] -2.8942e-07 2.8417e-07 -4.2729e-09 -4.2729e-09 v ǁVelocityǁ 1.7831e-09 0.10133 0.0074803 0.0074803 v Pressure -0.012002 0.039434 5.5955e-18 -5.2516e-18 v TempC 8.6649e-06 9.9082 2.566 2.566 v Density 0.97934 1 0.99773 0.99773 v TurbVisc 0 1.1842e-05 9.1414e-08 9.1414e-08 v CourantNb 8.1668e-10 1.0174 0.084607 0.084607 v FourierNb 0.0366 0.090675 0.072226 0.072226 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Csdyn2 0 0.004225 0.0028537 0.0028537 v SpecHeat 1017.2 1017.2 1017.2 1017.2 v ThermalCond 0.2 1 0.6 0.6 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 8.4768e-06 10 2.5936 2.5936 v Boundary Density 0.97934 1 0.9977 0.9977 v Yplus 0.00015908 5.2331 0.92906 0.92906 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.0366 1.0914 0.15683 0.15683 INSTANT 0.558000000E+02 TIME STEP NUMBER 558 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 20800 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00 Friction velocity uet : 0.62480E-06 0.19369E-01 Friction velocity uk : 0.62480E-06 0.19369E-01 Dimensionless distance yplus : 0.17071E-03 0.52316E+01 Friction thermal sca. tstar : -0.53542E+04 0.10771E+05 Rough dim-less th. sca. tplus : 0.31777E-05 0.48692E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 20800 Total number of wall faces : 20800 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.16366E-04 2 0.35935E-05 0.22688E-08 0.95124E-02 c Velocity[X] 0.37591E-09 c Velocity[Y] 0.18929E-08 c Velocity[Z] 0.57302E-15 c Pressure 0.18625E-07 7 0.78531E-05 0.17737E-02 0.28379E-01 c TempC 0.44270E+01 2 0.89670E-05 0.96410E-04 0.77411E-02 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a TempC ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.01962 0.030146 1.6189e-05 1.6189e-05 v Velocity[Y] -0.04135 0.10127 0.00012646 0.00012646 v Velocity[Z] -2.6303e-07 2.6149e-07 -3.9657e-09 -3.9657e-09 v ǁVelocityǁ 1.9477e-09 0.10127 0.0074756 0.0074756 v Pressure -0.012033 0.039498 1.8607e-17 7.0304e-18 v TempC 8.8568e-06 9.9083 2.5682 2.5682 v Density 0.97932 1 0.99772 0.99772 v TurbVisc 0 1.1843e-05 9.138e-08 9.138e-08 v CourantNb 8.2242e-10 1.0168 0.084547 0.084547 v FourierNb 0.0366 0.090677 0.072226 0.072226 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Csdyn2 0 0.004225 0.0028544 0.0028544 v SpecHeat 1017.2 1017.2 1017.2 1017.2 v ThermalCond 0.2 1 0.6 0.6 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 8.6649e-06 10 2.5958 2.5958 v Boundary Density 0.97932 1 0.99769 0.99769 v Yplus 0.00017071 5.2316 0.92867 0.92867 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.0366 1.0909 0.15677 0.15677 INSTANT 0.559000000E+02 TIME STEP NUMBER 559 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 20800 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00 Friction velocity uet : 0.66488E-06 0.19363E-01 Friction velocity uk : 0.66488E-06 0.19363E-01 Dimensionless distance yplus : 0.18166E-03 0.52300E+01 Friction thermal sca. tstar : -0.55685E+04 0.11020E+05 Rough dim-less th. sca. tplus : 0.33816E-05 0.48678E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 20800 Total number of wall faces : 20800 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.16357E-04 2 0.35703E-05 0.22584E-08 0.94958E-02 c Velocity[X] 0.37216E-09 c Velocity[Y] 0.18863E-08 c Velocity[Z] 0.47943E-15 c Pressure 0.18601E-07 7 0.77919E-05 0.17697E-02 0.28303E-01 c TempC 0.44283E+01 3 0.10084E-05 0.96331E-04 0.77353E-02 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a TempC ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.019621 0.030102 1.6196e-05 1.6196e-05 v Velocity[Y] -0.04136 0.10121 0.00012654 0.00012654 v Velocity[Z] -2.383e-07 2.4015e-07 -3.6809e-09 -3.6809e-09 v ǁVelocityǁ 2.0927e-09 0.10121 0.0074709 0.0074709 v Pressure -0.012065 0.039562 1.9273e-17 7.708e-18 v TempC 9.0478e-06 9.9084 2.5704 2.5704 v Density 0.97931 1 0.99772 0.99772 v TurbVisc 0 1.1843e-05 9.1352e-08 9.1352e-08 v CourantNb 8.1298e-10 1.0162 0.084486 0.084486 v FourierNb 0.0366 0.090679 0.072227 0.072227 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Csdyn2 0 0.004225 0.0028555 0.0028555 v SpecHeat 1017.2 1017.2 1017.2 1017.2 v ThermalCond 0.2 1 0.6 0.6 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 8.8568e-06 10 2.598 2.598 v Boundary Density 0.97931 1 0.99769 0.99769 v Yplus 0.00018166 5.23 0.92829 0.92829 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.0366 1.0903 0.15671 0.15671 INSTANT 0.560000000E+02 TIME STEP NUMBER 560 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 20800 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00 Friction velocity uet : 0.69498E-06 0.19357E-01 Friction velocity uk : 0.69498E-06 0.19357E-01 Dimensionless distance yplus : 0.18988E-03 0.52284E+01 Friction thermal sca. tstar : -0.57745E+04 0.11296E+05 Rough dim-less th. sca. tplus : 0.35347E-05 0.48663E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 20800 Total number of wall faces : 20800 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.16348E-04 2 0.35267E-05 0.22479E-08 0.94789E-02 c Velocity[X] 0.36846E-09 c Velocity[Y] 0.18795E-08 c Velocity[Z] 0.40131E-15 c Pressure 0.18571E-07 7 0.77318E-05 0.17652E-02 0.28213E-01 c TempC 0.44295E+01 2 0.72111E-05 0.96002E-04 0.77194E-02 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a TempC ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.019622 0.030058 1.6202e-05 1.6202e-05 v Velocity[Y] -0.041371 0.10115 0.00012663 0.00012663 v Velocity[Z] -2.1524e-07 2.2014e-07 -3.4167e-09 -3.4167e-09 v ǁVelocityǁ 2.2102e-09 0.10115 0.0074661 0.0074661 v Pressure -0.012097 0.039626 5.1958e-18 -5.3787e-18 v TempC 9.2533e-06 9.9085 2.5726 2.5726 v Density 0.9793 1 0.99771 0.99771 v TurbVisc 0 1.1844e-05 9.1321e-08 9.1321e-08 v CourantNb 7.9211e-10 1.0156 0.084426 0.084426 v FourierNb 0.0366 0.09068 0.072227 0.072227 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Csdyn2 0 0.004225 0.0028563 0.0028563 v SpecHeat 1017.2 1017.2 1017.2 1017.2 v ThermalCond 0.2 1 0.6 0.6 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 9.0478e-06 10 2.6002 2.6002 v Boundary Density 0.9793 1 0.99768 0.99768 v Yplus 0.00018988 5.2284 0.9279 0.9279 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.0366 1.0897 0.15665 0.15665 INSTANT 0.561000000E+02 TIME STEP NUMBER 561 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 20800 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00 Friction velocity uet : 0.71518E-06 0.19351E-01 Friction velocity uk : 0.71518E-06 0.19351E-01 Dimensionless distance yplus : 0.19540E-03 0.52269E+01 Friction thermal sca. tstar : -0.59852E+04 0.11598E+05 Rough dim-less th. sca. tplus : 0.36374E-05 0.48648E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 20800 Total number of wall faces : 20800 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.16339E-04 2 0.34869E-05 0.22335E-08 0.94535E-02 c Velocity[X] 0.36444E-09 c Velocity[Y] 0.18690E-08 c Velocity[Z] 0.33606E-15 c Pressure 0.18439E-07 7 0.76836E-05 0.17510E-02 0.28137E-01 c TempC 0.44308E+01 2 0.82462E-05 0.95707E-04 0.77049E-02 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a TempC ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.019623 0.030014 1.6208e-05 1.6208e-05 v Velocity[Y] -0.041382 0.10108 0.00012671 0.00012671 v Velocity[Z] -1.9384e-07 2.0142e-07 -3.1717e-09 -3.1717e-09 v ǁVelocityǁ 2.1372e-09 0.10109 0.0074614 0.0074614 v Pressure -0.012129 0.039689 3.2863e-18 -7.8774e-18 v TempC 9.465e-06 9.9086 2.5748 2.5748 v Density 0.97928 1 0.99771 0.99771 v TurbVisc 0 1.1845e-05 9.1277e-08 9.1277e-08 v CourantNb 7.6287e-10 1.015 0.084365 0.084365 v FourierNb 0.0366 0.090682 0.072227 0.072227 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Csdyn2 0 0.004225 0.0028563 0.0028563 v SpecHeat 1017.2 1017.2 1017.2 1017.2 v ThermalCond 0.2 1 0.6 0.6 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 9.2533e-06 10 2.6024 2.6024 v Boundary Density 0.97928 1 0.99768 0.99768 v Yplus 0.0001954 5.2269 0.92752 0.92752 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.0366 1.0891 0.15659 0.15659 INSTANT 0.562000000E+02 TIME STEP NUMBER 562 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 20800 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00 Friction velocity uet : 0.59776E-06 0.19346E-01 Friction velocity uk : 0.59776E-06 0.19346E-01 Dimensionless distance yplus : 0.16332E-03 0.52254E+01 Friction thermal sca. tstar : -0.61896E+04 0.11925E+05 Rough dim-less th. sca. tplus : 0.30402E-05 0.48634E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 20800 Total number of wall faces : 20800 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.16330E-04 2 0.34859E-05 0.22250E-08 0.94407E-02 c Velocity[X] 0.36101E-09 c Velocity[Y] 0.18640E-08 c Velocity[Z] 0.28154E-15 c Pressure 0.18444E-07 7 0.76137E-05 0.17498E-02 0.28052E-01 c TempC 0.44320E+01 2 0.77984E-05 0.95444E-04 0.76917E-02 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a TempC ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.019624 0.02997 1.6214e-05 1.6214e-05 v Velocity[Y] -0.041392 0.10102 0.00012679 0.00012679 v Velocity[Z] -1.7697e-07 1.8395e-07 -2.9444e-09 -2.9444e-09 v ǁVelocityǁ 1.9472e-09 0.10102 0.0074566 0.0074566 v Pressure -0.01216 0.039753 1.1235e-17 5.5057e-19 v TempC 9.6814e-06 9.9087 2.577 2.577 v Density 0.97927 1 0.9977 0.9977 v TurbVisc 0 1.1845e-05 9.1247e-08 9.1247e-08 v CourantNb 4.7736e-10 1.0145 0.084305 0.084305 v FourierNb 0.0366 0.090684 0.072227 0.072227 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Csdyn2 0 0.004225 0.0028571 0.0028571 v SpecHeat 1017.2 1017.2 1017.2 1017.2 v ThermalCond 0.2 1 0.6 0.6 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 9.465e-06 10 2.6045 2.6045 v Boundary Density 0.97927 1 0.99767 0.99767 v Yplus 0.00016332 5.2254 0.92715 0.92715 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.0366 1.0885 0.15653 0.15653 INSTANT 0.563000000E+02 TIME STEP NUMBER 563 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 20800 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00 Friction velocity uet : 0.60470E-06 0.19340E-01 Friction velocity uk : 0.60470E-06 0.19340E-01 Dimensionless distance yplus : 0.16522E-03 0.52238E+01 Friction thermal sca. tstar : -0.64296E+04 0.12277E+05 Rough dim-less th. sca. tplus : 0.30755E-05 0.48620E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 20800 Total number of wall faces : 20800 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.16321E-04 2 0.34858E-05 0.22161E-08 0.94270E-02 c Velocity[X] 0.35760E-09 c Velocity[Y] 0.18585E-08 c Velocity[Z] 0.23597E-15 c Pressure 0.18437E-07 7 0.75594E-05 0.17475E-02 0.27960E-01 c TempC 0.44333E+01 2 0.93830E-05 0.95099E-04 0.76752E-02 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a TempC ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.019626 0.029927 1.622e-05 1.622e-05 v Velocity[Y] -0.041402 0.10096 0.00012688 0.00012688 v Velocity[Z] -1.8226e-07 1.6769e-07 -2.7335e-09 -2.7335e-09 v ǁVelocityǁ 1.774e-09 0.10096 0.0074519 0.0074519 v Pressure -0.012192 0.039816 9.6367e-18 -1.3976e-18 v TempC 9.9055e-06 9.9088 2.5792 2.5792 v Density 0.97926 1 0.9977 0.9977 v TurbVisc 0 1.1846e-05 9.1219e-08 9.1219e-08 v CourantNb 6.8857e-10 1.0139 0.084245 0.084245 v FourierNb 0.0366 0.090686 0.072228 0.072228 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Csdyn2 0 0.004225 0.0028579 0.0028579 v SpecHeat 1017.2 1017.2 1017.2 1017.2 v ThermalCond 0.2 1 0.6 0.6 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 9.6814e-06 10 2.6067 2.6067 v Boundary Density 0.97926 1 0.99767 0.99767 v Yplus 0.00016522 5.2238 0.92677 0.92677 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.0366 1.0879 0.15647 0.15647 INSTANT 0.564000000E+02 TIME STEP NUMBER 564 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 20800 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00 Friction velocity uet : 0.73291E-06 0.19334E-01 Friction velocity uk : 0.73291E-06 0.19334E-01 Dimensionless distance yplus : 0.20025E-03 0.52223E+01 Friction thermal sca. tstar : -0.67513E+04 0.12654E+05 Rough dim-less th. sca. tplus : 0.37276E-05 0.48606E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 20800 Total number of wall faces : 20800 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.16312E-04 2 0.34842E-05 0.22064E-08 0.94116E-02 c Velocity[X] 0.35422E-09 c Velocity[Y] 0.18522E-08 c Velocity[Z] 0.19786E-15 c Pressure 0.18391E-07 7 0.75026E-05 0.17416E-02 0.27874E-01 c TempC 0.44345E+01 2 0.44137E-05 0.94910E-04 0.76650E-02 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a TempC ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.019627 0.029884 1.6226e-05 1.6226e-05 v Velocity[Y] -0.041412 0.1009 0.00012696 0.00012696 v Velocity[Z] -1.4811e-07 1.5259e-07 -2.5379e-09 -2.5379e-09 v ǁVelocityǁ 1.5805e-09 0.1009 0.0074472 0.0074472 v Pressure -0.012224 0.039879 4.2188e-18 -6.5222e-18 v TempC 1.0133e-05 9.9089 2.5814 2.5814 v Density 0.97925 1 0.99769 0.99769 v TurbVisc 0 1.1847e-05 9.1193e-08 9.1193e-08 v CourantNb 6.4704e-10 1.0132 0.084185 0.084185 v FourierNb 0.0366 0.090688 0.072228 0.072228 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Csdyn2 0 0.004225 0.0028587 0.0028587 v SpecHeat 1017.2 1017.2 1017.2 1017.2 v ThermalCond 0.2 1 0.6 0.6 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 9.9055e-06 10 2.6089 2.6089 v Boundary Density 0.97925 1 0.99766 0.99766 v Yplus 0.00020025 5.2223 0.9264 0.9264 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.0366 1.0873 0.15641 0.15641 INSTANT 0.565000000E+02 TIME STEP NUMBER 565 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 20800 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00 Friction velocity uet : 0.72935E-06 0.19328E-01 Friction velocity uk : 0.72935E-06 0.19328E-01 Dimensionless distance yplus : 0.19928E-03 0.52208E+01 Friction thermal sca. tstar : -0.71746E+04 0.13054E+05 Rough dim-less th. sca. tplus : 0.37095E-05 0.48592E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 20800 Total number of wall faces : 20800 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.16303E-04 2 0.34950E-05 0.21961E-08 0.93947E-02 c Velocity[X] 0.35080E-09 c Velocity[Y] 0.18453E-08 c Velocity[Z] 0.16597E-15 c Pressure 0.18345E-07 7 0.74442E-05 0.17356E-02 0.27783E-01 c TempC 0.44358E+01 2 0.77104E-05 0.94792E-04 0.76576E-02 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a TempC ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.019628 0.029841 1.6232e-05 1.6232e-05 v Velocity[Y] -0.041422 0.10084 0.00012704 0.00012704 v Velocity[Z] -1.3767e-07 1.4228e-07 -2.3563e-09 -2.3563e-09 v ǁVelocityǁ 1.4042e-09 0.10084 0.0074424 0.0074424 v Pressure -0.012256 0.039943 3.5971e-18 -8.1315e-18 v TempC 1.0373e-05 9.909 2.5836 2.5836 v Density 0.97923 1 0.99769 0.99769 v TurbVisc 0 1.1847e-05 9.1156e-08 9.1156e-08 v CourantNb 6.0434e-10 1.0126 0.084124 0.084124 v FourierNb 0.0366 0.09069 0.072228 0.072228 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Csdyn2 0 0.004225 0.0028587 0.0028587 v SpecHeat 1017.2 1017.2 1017.2 1017.2 v ThermalCond 0.2 1 0.6 0.6 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 1.0133e-05 10 2.6111 2.6111 v Boundary Density 0.97923 1 0.99766 0.99766 v Yplus 0.00019928 5.2208 0.92603 0.92603 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.0366 1.0867 0.15635 0.15635 INSTANT 0.566000000E+02 TIME STEP NUMBER 566 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 20800 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00 Friction velocity uet : 0.72280E-06 0.19322E-01 Friction velocity uk : 0.72280E-06 0.19322E-01 Dimensionless distance yplus : 0.19749E-03 0.52192E+01 Friction thermal sca. tstar : -0.76261E+04 0.13481E+05 Rough dim-less th. sca. tplus : 0.36761E-05 0.48577E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 20800 Total number of wall faces : 20800 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.16294E-04 2 0.34930E-05 0.21860E-08 0.93783E-02 c Velocity[X] 0.34749E-09 c Velocity[Y] 0.18385E-08 c Velocity[Z] 0.13927E-15 c Pressure 0.18276E-07 7 0.74132E-05 0.17275E-02 0.27698E-01 c TempC 0.44370E+01 2 0.90204E-05 0.94481E-04 0.76425E-02 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a TempC ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.019629 0.029799 1.6237e-05 1.6237e-05 v Velocity[Y] -0.041432 0.10078 0.00012712 0.00012712 v Velocity[Z] -1.2882e-07 1.3421e-07 -2.1879e-09 -2.1879e-09 v ǁVelocityǁ 1.248e-09 0.10078 0.0074377 0.0074377 v Pressure -0.012288 0.040006 9.2371e-18 -1.7364e-18 v TempC 1.0621e-05 9.9091 2.5858 2.5858 v Density 0.97922 1 0.99768 0.99768 v TurbVisc 0 1.1848e-05 9.1124e-08 9.1124e-08 v CourantNb 5.6143e-10 1.012 0.084064 0.084064 v FourierNb 0.0366 0.090692 0.072229 0.072229 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Csdyn2 0 0.004225 0.0028591 0.0028591 v SpecHeat 1017.2 1017.2 1017.2 1017.2 v ThermalCond 0.2 1 0.6 0.6 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 1.0373e-05 10 2.6132 2.6132 v Boundary Density 0.97922 1 0.99765 0.99765 v Yplus 0.00019749 5.2192 0.92567 0.92567 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.0366 1.0861 0.15629 0.15629 INSTANT 0.567000000E+02 TIME STEP NUMBER 567 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 20800 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00 Friction velocity uet : 0.44684E-06 0.19316E-01 Friction velocity uk : 0.44684E-06 0.19316E-01 Dimensionless distance yplus : 0.12209E-03 0.52176E+01 Friction thermal sca. tstar : -0.81042E+04 0.13931E+05 Rough dim-less th. sca. tplus : 0.22726E-05 0.48562E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 20800 Total number of wall faces : 20800 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.16285E-04 2 0.34953E-05 0.21786E-08 0.93675E-02 c Velocity[X] 0.34448E-09 c Velocity[Y] 0.18341E-08 c Velocity[Z] 0.11692E-15 c Pressure 0.18256E-07 7 0.73556E-05 0.17239E-02 0.27630E-01 c TempC 0.44383E+01 2 0.81560E-05 0.94230E-04 0.76298E-02 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a TempC ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.01963 0.029757 1.6243e-05 1.6243e-05 v Velocity[Y] -0.041442 0.10072 0.00012721 0.00012721 v Velocity[Z] -1.2012e-07 1.2291e-07 -2.0315e-09 -2.0315e-09 v ǁVelocityǁ 1.0991e-09 0.10072 0.007433 0.007433 v Pressure -0.01232 0.040069 6.6169e-18 -4.3199e-18 v TempC 1.0874e-05 9.9092 2.588 2.588 v Density 0.97921 1 0.99767 0.99767 v TurbVisc 0 1.1849e-05 9.1091e-08 9.1091e-08 v CourantNb 5.1903e-10 1.0114 0.084004 0.084004 v FourierNb 0.0366 0.090694 0.072229 0.072229 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Csdyn2 0 0.004225 0.0028595 0.0028595 v SpecHeat 1017.2 1017.2 1017.2 1017.2 v ThermalCond 0.2 1 0.6 0.6 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 1.0621e-05 10 2.6154 2.6154 v Boundary Density 0.97921 1 0.99765 0.99765 v Yplus 0.00012209 5.2176 0.9253 0.9253 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.0366 1.0855 0.15623 0.15623 INSTANT 0.568000000E+02 TIME STEP NUMBER 568 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 20800 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00 Friction velocity uet : 0.70348E-06 0.19310E-01 Friction velocity uk : 0.70348E-06 0.19310E-01 Dimensionless distance yplus : 0.19221E-03 0.52160E+01 Friction thermal sca. tstar : -0.86098E+04 0.14408E+05 Rough dim-less th. sca. tplus : 0.35779E-05 0.48548E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 20800 Total number of wall faces : 20800 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.16276E-04 2 0.34885E-05 0.21704E-08 0.93552E-02 c Velocity[X] 0.34147E-09 c Velocity[Y] 0.18290E-08 c Velocity[Z] 0.98190E-16 c Pressure 0.18223E-07 7 0.72995E-05 0.17193E-02 0.27539E-01 c TempC 0.44395E+01 2 0.97210E-05 0.93881E-04 0.76130E-02 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a TempC ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.01963 0.029715 1.6249e-05 1.6249e-05 v Velocity[Y] -0.041452 0.10066 0.00012729 0.00012729 v Velocity[Z] -1.1162e-07 1.1386e-07 -1.8865e-09 -1.8865e-09 v ǁVelocityǁ 9.5248e-10 0.10066 0.0074282 0.0074282 v Pressure -0.012352 0.040132 1.0258e-17 -4.6587e-19 v TempC 1.1137e-05 9.9093 2.5902 2.5902 v Density 0.9792 1 0.99767 0.99767 v TurbVisc 0 1.1849e-05 9.1065e-08 9.1065e-08 v CourantNb 4.777e-10 1.0108 0.083944 0.083944 v FourierNb 0.0366 0.090696 0.072229 0.072229 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Csdyn2 0 0.004225 0.0028603 0.0028603 v SpecHeat 1017.2 1017.2 1017.2 1017.2 v ThermalCond 0.2 1 0.6 0.6 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 1.0874e-05 10 2.6176 2.6176 v Boundary Density 0.9792 1 0.99764 0.99764 v Yplus 0.00019221 5.216 0.92494 0.92494 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.0366 1.0848 0.15617 0.15617 INSTANT 0.569000000E+02 TIME STEP NUMBER 569 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 20800 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00 Friction velocity uet : 0.69173E-06 0.19304E-01 Friction velocity uk : 0.69173E-06 0.19304E-01 Dimensionless distance yplus : 0.18900E-03 0.52145E+01 Friction thermal sca. tstar : -0.91462E+04 0.14910E+05 Rough dim-less th. sca. tplus : 0.35182E-05 0.48533E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 20800 Total number of wall faces : 20800 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.16267E-04 2 0.34704E-05 0.21618E-08 0.93416E-02 c Velocity[X] 0.33849E-09 c Velocity[Y] 0.18233E-08 c Velocity[Z] 0.82497E-16 c Pressure 0.18163E-07 7 0.72451E-05 0.17121E-02 0.27453E-01 c TempC 0.44408E+01 2 0.49066E-05 0.93722E-04 0.76041E-02 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a TempC ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.019631 0.029673 1.6255e-05 1.6255e-05 v Velocity[Y] -0.041462 0.1006 0.00012737 0.00012737 v Velocity[Z] -1.0338e-07 1.0524e-07 -1.7518e-09 -1.7518e-09 v ǁVelocityǁ 8.2551e-10 0.1006 0.0074235 0.0074235 v Pressure -0.012384 0.040195 1.3056e-17 2.5411e-18 v TempC 1.1407e-05 9.9094 2.5924 2.5924 v Density 0.97918 1 0.99766 0.99766 v TurbVisc 0 1.185e-05 9.1031e-08 9.1031e-08 v CourantNb 4.3786e-10 1.0102 0.083884 0.083884 v FourierNb 0.0366 0.090697 0.072229 0.072229 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Csdyn2 0 0.004225 0.0028608 0.0028608 v SpecHeat 1017.2 1017.2 1017.2 1017.2 v ThermalCond 0.2 1 0.6 0.6 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 1.1137e-05 10 2.6197 2.6197 v Boundary Density 0.97918 1 0.99764 0.99764 v Yplus 0.000189 5.2145 0.92458 0.92458 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.0366 1.0842 0.15611 0.15611 INSTANT 0.570000000E+02 TIME STEP NUMBER 570 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 20800 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00 Friction velocity uet : 0.67908E-06 0.19299E-01 Friction velocity uk : 0.67908E-06 0.19299E-01 Dimensionless distance yplus : 0.18554E-03 0.52128E+01 Friction thermal sca. tstar : -0.97135E+04 0.15440E+05 Rough dim-less th. sca. tplus : 0.34538E-05 0.48518E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 20800 Total number of wall faces : 20800 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.16258E-04 2 0.34539E-05 0.21523E-08 0.93262E-02 c Velocity[X] 0.33545E-09 c Velocity[Y] 0.18168E-08 c Velocity[Z] 0.69340E-16 c Pressure 0.18110E-07 7 0.71896E-05 0.17055E-02 0.27366E-01 c TempC 0.44420E+01 2 0.85449E-05 0.93586E-04 0.75960E-02 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a TempC ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.019632 0.029632 1.626e-05 1.626e-05 v Velocity[Y] -0.041471 0.10054 0.00012745 0.00012745 v Velocity[Z] -9.5457e-08 9.7062e-08 -1.6268e-09 -1.6268e-09 v ǁVelocityǁ 7.1618e-10 0.10054 0.0074188 0.0074188 v Pressure -0.012416 0.040258 9.4147e-18 -1.6517e-18 v TempC 1.1651e-05 9.9095 2.5946 2.5946 v Density 0.97917 1 0.99766 0.99766 v TurbVisc 0 1.1851e-05 9.0999e-08 9.0999e-08 v CourantNb 3.9979e-10 1.0095 0.083824 0.083824 v FourierNb 0.0366 0.090699 0.07223 0.07223 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Csdyn2 0 0.004225 0.0028612 0.0028612 v SpecHeat 1017.2 1017.2 1017.2 1017.2 v ThermalCond 0.2 1 0.6 0.6 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 1.1407e-05 10 2.6219 2.6219 v Boundary Density 0.97917 1 0.99763 0.99763 v Yplus 0.00018554 5.2128 0.92422 0.92422 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.0366 1.0836 0.15605 0.15605 INSTANT 0.571000000E+02 TIME STEP NUMBER 571 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 20800 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00 Friction velocity uet : 0.66580E-06 0.19293E-01 Friction velocity uk : 0.66580E-06 0.19293E-01 Dimensionless distance yplus : 0.18191E-03 0.52112E+01 Friction thermal sca. tstar : -0.10317E+05 0.15996E+05 Rough dim-less th. sca. tplus : 0.33862E-05 0.48503E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 20800 Total number of wall faces : 20800 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.16249E-04 2 0.34299E-05 0.21434E-08 0.93122E-02 c Velocity[X] 0.33256E-09 c Velocity[Y] 0.18109E-08 c Velocity[Z] 0.58305E-16 c Pressure 0.18043E-07 7 0.71365E-05 0.16977E-02 0.27286E-01 c TempC 0.44433E+01 2 0.91820E-05 0.93321E-04 0.75827E-02 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a TempC ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.019633 0.029591 1.6266e-05 1.6266e-05 v Velocity[Y] -0.041481 0.10048 0.00012753 0.00012753 v Velocity[Z] -8.7872e-08 8.9338e-08 -1.5108e-09 -1.5108e-09 v ǁVelocityǁ 6.1643e-10 0.10048 0.0074141 0.0074141 v Pressure -0.012448 0.040321 1.4566e-17 3.0493e-18 v TempC 1.1891e-05 9.9096 2.5968 2.5968 v Density 0.97916 1 0.99765 0.99765 v TurbVisc 0 1.1851e-05 9.0965e-08 9.0965e-08 v CourantNb 3.6368e-10 1.0089 0.083764 0.083764 v FourierNb 0.0366 0.090701 0.07223 0.07223 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Csdyn2 0 0.004225 0.0028616 0.0028616 v SpecHeat 1017.2 1017.2 1017.2 1017.2 v ThermalCond 0.2 1 0.6 0.6 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 1.1651e-05 10 2.6241 2.6241 v Boundary Density 0.97916 1 0.99763 0.99763 v Yplus 0.00018191 5.2112 0.92387 0.92387 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.0366 1.083 0.15599 0.15599 INSTANT 0.572000000E+02 TIME STEP NUMBER 572 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 20800 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00 Friction velocity uet : 0.64741E-06 0.19287E-01 Friction velocity uk : 0.64741E-06 0.19287E-01 Dimensionless distance yplus : 0.17689E-03 0.52096E+01 Friction thermal sca. tstar : -0.10955E+05 0.16582E+05 Rough dim-less th. sca. tplus : 0.32927E-05 0.48488E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 20800 Total number of wall faces : 20800 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.16240E-04 2 0.34178E-05 0.21370E-08 0.93034E-02 c Velocity[X] 0.32994E-09 c Velocity[Y] 0.18071E-08 c Velocity[Z] 0.49046E-16 c Pressure 0.18028E-07 7 0.70825E-05 0.16947E-02 0.27214E-01 c TempC 0.44445E+01 3 0.91364E-06 0.93269E-04 0.75780E-02 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a TempC ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.019634 0.02955 1.6272e-05 1.6272e-05 v Velocity[Y] -0.04149 0.10041 0.00012761 0.00012761 v Velocity[Z] -8.0653e-08 8.2063e-08 -1.403e-09 -1.403e-09 v ǁVelocityǁ 5.281e-10 0.10041 0.0074093 0.0074093 v Pressure -0.01248 0.040384 1.0836e-17 1.2705e-19 v TempC 1.2134e-05 9.9097 2.599 2.599 v Density 0.97915 1 0.99765 0.99765 v TurbVisc 0 1.1852e-05 9.0937e-08 9.0937e-08 v CourantNb 3.2966e-10 1.0083 0.083704 0.083704 v FourierNb 0.0366 0.090703 0.07223 0.07223 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Csdyn2 0 0.004225 0.0028624 0.0028624 v SpecHeat 1017.2 1017.2 1017.2 1017.2 v ThermalCond 0.2 1 0.6 0.6 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 1.1891e-05 10 2.6263 2.6263 v Boundary Density 0.97915 1 0.99762 0.99762 v Yplus 0.00017689 5.2096 0.92351 0.92351 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.0366 1.0823 0.15593 0.15593 INSTANT 0.573000000E+02 TIME STEP NUMBER 573 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 20800 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00 Friction velocity uet : 0.60292E-06 0.19281E-01 Friction velocity uk : 0.60292E-06 0.19281E-01 Dimensionless distance yplus : 0.16473E-03 0.52080E+01 Friction thermal sca. tstar : -0.11624E+05 0.17195E+05 Rough dim-less th. sca. tplus : 0.30665E-05 0.48472E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 20800 Total number of wall faces : 20800 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.16231E-04 2 0.34000E-05 0.21300E-08 0.92932E-02 c Velocity[X] 0.32735E-09 c Velocity[Y] 0.18026E-08 c Velocity[Z] 0.41274E-16 c Pressure 0.17993E-07 7 0.70300E-05 0.16899E-02 0.27128E-01 c TempC 0.44458E+01 2 0.75365E-05 0.92944E-04 0.75623E-02 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a TempC ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.019635 0.029509 1.6277e-05 1.6277e-05 v Velocity[Y] -0.041499 0.10035 0.00012769 0.00012769 v Velocity[Z] -7.3818e-08 7.5586e-08 -1.303e-09 -1.303e-09 v ǁVelocityǁ 4.5077e-10 0.10035 0.0074046 0.0074046 v Pressure -0.012513 0.040447 1.4388e-17 2.8799e-18 v TempC 1.2394e-05 9.9098 2.6012 2.6012 v Density 0.97914 1 0.99764 0.99764 v TurbVisc 0 1.1853e-05 9.0895e-08 9.0895e-08 v CourantNb 2.9778e-10 1.0076 0.083644 0.083644 v FourierNb 0.0366 0.090704 0.07223 0.07223 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Csdyn2 0 0.004225 0.0028624 0.0028624 v SpecHeat 1017.2 1017.2 1017.2 1017.2 v ThermalCond 0.2 1 0.6 0.6 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 1.2134e-05 10 2.6284 2.6284 v Boundary Density 0.97914 1 0.99762 0.99762 v Yplus 0.00016473 5.208 0.92316 0.92316 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.0366 1.0817 0.15587 0.15587 INSTANT 0.574000000E+02 TIME STEP NUMBER 574 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 20800 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00 Friction velocity uet : 0.47237E-06 0.19275E-01 Friction velocity uk : 0.47237E-06 0.19275E-01 Dimensionless distance yplus : 0.12906E-03 0.52063E+01 Friction thermal sca. tstar : -0.12341E+05 0.17839E+05 Rough dim-less th. sca. tplus : 0.24025E-05 0.48457E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 20800 Total number of wall faces : 20800 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.16222E-04 2 0.33670E-05 0.21191E-08 0.92746E-02 c Velocity[X] 0.32446E-09 c Velocity[Y] 0.17946E-08 c Velocity[Z] 0.34748E-16 c Pressure 0.17863E-07 7 0.69876E-05 0.16761E-02 0.27059E-01 c TempC 0.44470E+01 2 0.80198E-05 0.92689E-04 0.75494E-02 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a TempC ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.019636 0.029469 1.6283e-05 1.6283e-05 v Velocity[Y] -0.041509 0.10029 0.00012777 0.00012777 v Velocity[Z] -6.7379e-08 6.9589e-08 -1.2101e-09 -1.2101e-09 v ǁVelocityǁ 3.8322e-10 0.10029 0.0073999 0.0073999 v Pressure -0.012545 0.040509 1.0303e-17 -1.2282e-18 v TempC 1.2658e-05 9.9099 2.6033 2.6033 v Density 0.97912 1 0.99764 0.99764 v TurbVisc 0 1.1853e-05 9.0868e-08 9.0868e-08 v CourantNb 2.6807e-10 1.007 0.083584 0.083584 v FourierNb 0.0366 0.090706 0.072231 0.072231 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Csdyn2 0 0.004225 0.0028634 0.0028634 v SpecHeat 1017.2 1017.2 1017.2 1017.2 v ThermalCond 0.2 1 0.6 0.6 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 1.2394e-05 10 2.6306 2.6306 v Boundary Density 0.97912 1 0.99761 0.99761 v Yplus 0.00012906 5.2063 0.92281 0.92281 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.0366 1.0811 0.15581 0.15581 INSTANT 0.575000000E+02 TIME STEP NUMBER 575 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 20800 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00 Friction velocity uet : 0.52324E-06 0.19269E-01 Friction velocity uk : 0.52324E-06 0.19269E-01 Dimensionless distance yplus : 0.14296E-03 0.52046E+01 Friction thermal sca. tstar : -0.13096E+05 0.18514E+05 Rough dim-less th. sca. tplus : 0.26612E-05 0.48441E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 20800 Total number of wall faces : 20800 ------------------------------------------------------------ Write intermediate restart files checkpoint at iteration 575, Physical time 0.57500E+02 ** Writing the main restart file ----------------------------- Start writing Wrote field names and types to checkpoint at iteration 575: checkpoint/main End writing the options Wrote main variables to checkpoint: checkpoint/main End writing ** Writing the auxiliary restart file ---------------------------------- Start writing End writing the dimensions and options End writing the physical properties End writing the time step Wrote boundary condition coefficients to checkpoint: checkpoint/auxiliary End writing the source terms End writing ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.16213E-04 2 0.33605E-05 0.21141E-08 0.92689E-02 c Velocity[X] 0.32214E-09 c Velocity[Y] 0.17920E-08 c Velocity[Z] 0.29264E-16 c Pressure 0.17875E-07 7 0.69260E-05 0.16758E-02 0.26978E-01 c TempC 0.44482E+01 2 0.95958E-05 0.92373E-04 0.75340E-02 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a TempC ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.019637 0.029428 1.6288e-05 1.6288e-05 v Velocity[Y] -0.041518 0.10022 0.00012785 0.00012785 v Velocity[Z] -6.134e-08 6.3947e-08 -1.1239e-09 -1.1239e-09 v ǁVelocityǁ 3.2439e-10 0.10022 0.0073952 0.0073952 v Pressure -0.012577 0.040572 1.1546e-17 7.1998e-19 v TempC 1.293e-05 9.91 2.6055 2.6055 v Density 0.97911 1 0.99763 0.99763 v TurbVisc 0 1.1854e-05 9.0848e-08 9.0848e-08 v CourantNb 2.4049e-10 1.0064 0.083524 0.083524 v FourierNb 0.0366 0.090708 0.072231 0.072231 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Csdyn2 0 0.004225 0.0028649 0.0028649 v SpecHeat 1017.2 1017.2 1017.2 1017.2 v ThermalCond 0.2 1 0.6 0.6 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 1.2658e-05 10 2.6328 2.6328 v Boundary Density 0.97911 1 0.99761 0.99761 v Yplus 0.00014296 5.2046 0.92246 0.92246 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.0366 1.0805 0.15575 0.15575 INSTANT 0.576000000E+02 TIME STEP NUMBER 576 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 20800 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00 Friction velocity uet : 0.48776E-06 0.19263E-01 Friction velocity uk : 0.48776E-06 0.19263E-01 Dimensionless distance yplus : 0.13327E-03 0.52029E+01 Friction thermal sca. tstar : -0.13891E+05 0.19221E+05 Rough dim-less th. sca. tplus : 0.24807E-05 0.48426E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 20800 Total number of wall faces : 20800 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.16204E-04 2 0.33457E-05 0.21085E-08 0.92618E-02 c Velocity[X] 0.31983E-09 c Velocity[Y] 0.17887E-08 c Velocity[Z] 0.24655E-16 c Pressure 0.17862E-07 7 0.68750E-05 0.16730E-02 0.26893E-01 c TempC 0.44495E+01 2 0.90332E-05 0.92117E-04 0.75211E-02 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a TempC ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.019638 0.029389 1.6293e-05 1.6293e-05 v Velocity[Y] -0.041527 0.10016 0.00012793 0.00012793 v Velocity[Z] -5.5701e-08 5.8653e-08 -1.0438e-09 -1.0438e-09 v ǁVelocityǁ 2.7329e-10 0.10016 0.0073904 0.0073904 v Pressure -0.01261 0.040635 1.0703e-17 -9.3174e-19 v TempC 1.3208e-05 9.9101 2.6077 2.6077 v Density 0.9791 1 0.99763 0.99763 v TurbVisc 0 1.1855e-05 9.0821e-08 9.0821e-08 v CourantNb 2.0845e-10 1.0058 0.083464 0.083464 v FourierNb 0.0366 0.09071 0.072231 0.072231 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Csdyn2 0 0.004225 0.002866 0.002866 v SpecHeat 1017.2 1017.2 1017.2 1017.2 v ThermalCond 0.2 1 0.6 0.6 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 1.293e-05 10 2.6349 2.6349 v Boundary Density 0.9791 1 0.9976 0.9976 v Yplus 0.00013327 5.2029 0.92211 0.92211 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.0366 1.0798 0.15569 0.15569 INSTANT 0.577000000E+02 TIME STEP NUMBER 577 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 20800 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00 Friction velocity uet : 0.45500E-06 0.19257E-01 Friction velocity uk : 0.45500E-06 0.19257E-01 Dimensionless distance yplus : 0.12432E-03 0.52013E+01 Friction thermal sca. tstar : -0.14732E+05 0.19961E+05 Rough dim-less th. sca. tplus : 0.23141E-05 0.48410E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 20800 Total number of wall faces : 20800 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.16195E-04 2 0.33148E-05 0.21018E-08 0.92522E-02 c Velocity[X] 0.31747E-09 c Velocity[Y] 0.17843E-08 c Velocity[Z] 0.20780E-16 c Pressure 0.17827E-07 7 0.68243E-05 0.16683E-02 0.26807E-01 c TempC 0.44507E+01 3 0.85916E-06 0.92135E-04 0.75193E-02 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a TempC ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.019639 0.029349 1.6299e-05 1.6299e-05 v Velocity[Y] -0.041536 0.10009 0.00012801 0.00012801 v Velocity[Z] -5.0455e-08 5.4293e-08 -9.6948e-10 -9.6948e-10 v ǁVelocityǁ 2.2911e-10 0.10009 0.0073857 0.0073857 v Pressure -0.012642 0.040697 5.107e-18 -6.0139e-18 v TempC 1.3488e-05 9.9102 2.6099 2.6099 v Density 0.97909 1 0.99762 0.99762 v TurbVisc 0 1.1855e-05 9.0801e-08 9.0801e-08 v CourantNb 5.4372e-11 1.0051 0.083404 0.083404 v FourierNb 0.0366 0.090711 0.072232 0.072232 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Csdyn2 0 0.004225 0.0028676 0.0028676 v SpecHeat 1017.2 1017.2 1017.2 1017.2 v ThermalCond 0.2 1 0.6 0.6 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 1.3208e-05 10 2.6371 2.6371 v Boundary Density 0.97909 1 0.9976 0.9976 v Yplus 0.00012432 5.2013 0.92176 0.92176 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.0366 1.0792 0.15564 0.15564 INSTANT 0.578000000E+02 TIME STEP NUMBER 578 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 20800 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00 Friction velocity uet : 0.42486E-06 0.19250E-01 Friction velocity uk : 0.42486E-06 0.19250E-01 Dimensionless distance yplus : 0.11608E-03 0.51996E+01 Friction thermal sca. tstar : -0.15612E+05 0.20736E+05 Rough dim-less th. sca. tplus : 0.21608E-05 0.48394E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 20800 Total number of wall faces : 20800 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.16186E-04 2 0.32923E-05 0.20945E-08 0.92413E-02 c Velocity[X] 0.31513E-09 c Velocity[Y] 0.17794E-08 c Velocity[Z] 0.17520E-16 c Pressure 0.17773E-07 7 0.67751E-05 0.16618E-02 0.26723E-01 c TempC 0.44519E+01 2 0.77201E-05 0.91787E-04 0.75026E-02 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a TempC ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.01964 0.029309 1.6304e-05 1.6304e-05 v Velocity[Y] -0.041545 0.10003 0.00012809 0.00012809 v Velocity[Z] -4.5596e-08 5.0451e-08 -9.0042e-10 -9.0042e-10 v ǁVelocityǁ 1.9111e-10 0.10003 0.007381 0.007381 v Pressure -0.012674 0.040759 1.0569e-17 -6.3527e-19 v TempC 1.3789e-05 9.9103 2.6121 2.6121 v Density 0.97908 1 0.99762 0.99762 v TurbVisc 0 1.1856e-05 9.0753e-08 9.0753e-08 v CourantNb 7.1249e-11 1.0045 0.083344 0.083344 v FourierNb 0.0366 0.090713 0.072232 0.072232 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Csdyn2 0 0.004225 0.0028672 0.0028672 v SpecHeat 1017.2 1017.2 1017.2 1017.2 v ThermalCond 0.2 1 0.6 0.6 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 1.3488e-05 10 2.6392 2.6392 v Boundary Density 0.97908 1 0.99759 0.99759 v Yplus 0.00011608 5.1996 0.92141 0.92141 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.0366 1.0786 0.15558 0.15558 INSTANT 0.579000000E+02 TIME STEP NUMBER 579 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 20800 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00 Friction velocity uet : 0.39722E-06 0.19244E-01 Friction velocity uk : 0.39722E-06 0.19244E-01 Dimensionless distance yplus : 0.10853E-03 0.51978E+01 Friction thermal sca. tstar : -0.16552E+05 0.21546E+05 Rough dim-less th. sca. tplus : 0.20202E-05 0.48378E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 20800 Total number of wall faces : 20800 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.16177E-04 2 0.32718E-05 0.20843E-08 0.92238E-02 c Velocity[X] 0.31258E-09 c Velocity[Y] 0.17717E-08 c Velocity[Z] 0.14776E-16 c Pressure 0.17648E-07 7 0.67354E-05 0.16486E-02 0.26661E-01 c TempC 0.44532E+01 2 0.61632E-05 0.91560E-04 0.74908E-02 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a TempC ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.019641 0.02927 1.6309e-05 1.6309e-05 v Velocity[Y] -0.041553 0.099962 0.00012817 0.00012817 v Velocity[Z] -4.1111e-08 4.6782e-08 -8.3628e-10 -8.3628e-10 v ǁVelocityǁ 1.5865e-10 0.099963 0.0073763 0.0073763 v Pressure -0.012707 0.040822 1.0303e-17 -9.3174e-19 v TempC 1.4094e-05 9.9104 2.6143 2.6143 v Density 0.97906 1 0.99761 0.99761 v TurbVisc 0 1.1857e-05 9.0723e-08 9.0723e-08 v CourantNb 1.5026e-10 1.0039 0.083284 0.083284 v FourierNb 0.0366 0.090715 0.072232 0.072232 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Csdyn2 0 0.004225 0.002868 0.002868 v SpecHeat 1017.2 1017.2 1017.2 1017.2 v ThermalCond 0.2 1 0.6 0.6 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 1.3789e-05 10 2.6414 2.6414 v Boundary Density 0.97906 1 0.99759 0.99759 v Yplus 0.00010853 5.1978 0.92107 0.92107 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.0366 1.0779 0.15552 0.15552 INSTANT 0.580000000E+02 TIME STEP NUMBER 580 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 20800 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00 Friction velocity uet : 0.37196E-06 0.19238E-01 Friction velocity uk : 0.37196E-06 0.19238E-01 Dimensionless distance yplus : 0.10163E-03 0.51962E+01 Friction thermal sca. tstar : -0.17538E+05 0.22393E+05 Rough dim-less th. sca. tplus : 0.18918E-05 0.48363E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 20800 Total number of wall faces : 20800 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.16168E-04 2 0.32844E-05 0.20797E-08 0.92188E-02 c Velocity[X] 0.31053E-09 c Velocity[Y] 0.17691E-08 c Velocity[Z] 0.12465E-16 c Pressure 0.17663E-07 7 0.66769E-05 0.16485E-02 0.26579E-01 c TempC 0.44544E+01 2 0.81282E-05 0.91293E-04 0.74774E-02 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a TempC ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.019642 0.029231 1.6314e-05 1.6314e-05 v Velocity[Y] -0.041562 0.099895 0.00012825 0.00012825 v Velocity[Z] -3.7494e-08 4.3624e-08 -7.7671e-10 -7.7671e-10 v ǁVelocityǁ 1.3121e-10 0.099897 0.0073716 0.0073716 v Pressure -0.012739 0.040884 1.1546e-17 8.0468e-19 v TempC 1.4411e-05 9.9105 2.6164 2.6164 v Density 0.97905 1 0.99761 0.99761 v TurbVisc 0 1.1857e-05 9.0679e-08 9.0679e-08 v CourantNb 1.3228e-10 1.0032 0.083224 0.083224 v FourierNb 0.0366 0.090716 0.072232 0.072232 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Csdyn2 0 0.004225 0.002868 0.002868 v SpecHeat 1017.2 1017.2 1017.2 1017.2 v ThermalCond 0.2 1 0.6 0.6 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 1.4094e-05 10 2.6436 2.6436 v Boundary Density 0.97905 1 0.99758 0.99758 v Yplus 0.00010163 5.1962 0.92073 0.92073 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.0366 1.0773 0.15546 0.15546 INSTANT 0.581000000E+02 TIME STEP NUMBER 581 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 20800 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00 Friction velocity uet : 0.34897E-06 0.19232E-01 Friction velocity uk : 0.34897E-06 0.19232E-01 Dimensionless distance yplus : 0.95347E-04 0.51945E+01 Friction thermal sca. tstar : -0.18575E+05 0.23278E+05 Rough dim-less th. sca. tplus : 0.17749E-05 0.48347E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 20800 Total number of wall faces : 20800 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.16158E-04 2 0.32848E-05 0.20743E-08 0.92119E-02 c Velocity[X] 0.30847E-09 c Velocity[Y] 0.17658E-08 c Velocity[Z] 0.10519E-16 c Pressure 0.17638E-07 7 0.66297E-05 0.16448E-02 0.26497E-01 c TempC 0.44556E+01 2 0.47283E-05 0.91097E-04 0.74669E-02 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a TempC ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.019643 0.029192 1.6319e-05 1.6319e-05 v Velocity[Y] -0.041571 0.099829 0.00012833 0.00012833 v Velocity[Z] -3.4492e-08 4.0588e-08 -7.2138e-10 -7.2138e-10 v ǁVelocityǁ 1.0833e-10 0.09983 0.0073669 0.0073669 v Pressure -0.012772 0.040946 1.3767e-17 2.287e-18 v TempC 1.4736e-05 9.9106 2.6186 2.6186 v Density 0.97904 1 0.9976 0.9976 v TurbVisc 0 1.1858e-05 9.0634e-08 9.0634e-08 v CourantNb 1.1593e-10 1.0026 0.083164 0.083164 v FourierNb 0.0366 0.090718 0.072233 0.072233 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Csdyn2 0 0.004225 0.002868 0.002868 v SpecHeat 1017.2 1017.2 1017.2 1017.2 v ThermalCond 0.2 1 0.6 0.6 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 1.4411e-05 10 2.6457 2.6457 v Boundary Density 0.97904 1 0.99758 0.99758 v Yplus 9.5347e-05 5.1945 0.92038 0.92038 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.0366 1.0766 0.1554 0.1554 INSTANT 0.582000000E+02 TIME STEP NUMBER 582 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 20800 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00 Friction velocity uet : 0.32813E-06 0.19225E-01 Friction velocity uk : 0.32813E-06 0.19225E-01 Dimensionless distance yplus : 0.89653E-04 0.51929E+01 Friction thermal sca. tstar : -0.19664E+05 0.24204E+05 Rough dim-less th. sca. tplus : 0.16689E-05 0.48332E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 20800 Total number of wall faces : 20800 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.16149E-04 2 0.32865E-05 0.20687E-08 0.92048E-02 c Velocity[X] 0.30645E-09 c Velocity[Y] 0.17623E-08 c Velocity[Z] 0.88796E-17 c Pressure 0.17620E-07 7 0.65818E-05 0.16417E-02 0.26418E-01 c TempC 0.44569E+01 2 0.74993E-05 0.90926E-04 0.74575E-02 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a TempC ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.019643 0.029153 1.6324e-05 1.6324e-05 v Velocity[Y] -0.041579 0.099763 0.0001284 0.0001284 v Velocity[Z] -3.1639e-08 3.7681e-08 -6.6998e-10 -6.6998e-10 v ǁVelocityǁ 8.9661e-11 0.099764 0.0073622 0.0073622 v Pressure -0.012804 0.041009 1.2079e-17 6.3527e-19 v TempC 1.5075e-05 9.9107 2.6208 2.6208 v Density 0.97903 1 0.9976 0.9976 v TurbVisc 0 1.1858e-05 9.0608e-08 9.0608e-08 v CourantNb 1.0111e-10 1.0019 0.083105 0.083105 v FourierNb 0.0366 0.09072 0.072233 0.072233 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Csdyn2 0 0.004225 0.0028691 0.0028691 v SpecHeat 1017.2 1017.2 1017.2 1017.2 v ThermalCond 0.2 1 0.6 0.6 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 1.4736e-05 10 2.6479 2.6479 v Boundary Density 0.97903 1 0.99757 0.99757 v Yplus 8.9653e-05 5.1929 0.92004 0.92004 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.0366 1.076 0.15534 0.15534 INSTANT 0.583000000E+02 TIME STEP NUMBER 583 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 20800 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00 Friction velocity uet : 0.30931E-06 0.19219E-01 Friction velocity uk : 0.30931E-06 0.19219E-01 Dimensionless distance yplus : 0.84512E-04 0.51912E+01 Friction thermal sca. tstar : -0.20815E+05 0.25171E+05 Rough dim-less th. sca. tplus : 0.15732E-05 0.48316E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 20800 Total number of wall faces : 20800 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.16140E-04 2 0.32754E-05 0.20627E-08 0.91965E-02 c Velocity[X] 0.30443E-09 c Velocity[Y] 0.17582E-08 c Velocity[Z] 0.74972E-17 c Pressure 0.17564E-07 7 0.65366E-05 0.16349E-02 0.26340E-01 c TempC 0.44581E+01 2 0.82892E-05 0.90679E-04 0.74449E-02 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a TempC ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.019644 0.029115 1.6329e-05 1.6329e-05 v Velocity[Y] -0.041588 0.099699 0.00012848 0.00012848 v Velocity[Z] -2.8941e-08 3.4908e-08 -6.2224e-10 -6.2224e-10 v ǁVelocityǁ 7.4923e-11 0.0997 0.0073575 0.0073575 v Pressure -0.012837 0.041071 7.9492e-18 -3.3034e-18 v TempC 1.5424e-05 9.9108 2.623 2.623 v Density 0.97901 1 0.99759 0.99759 v TurbVisc 0 1.1859e-05 9.057e-08 9.057e-08 v CourantNb 8.7706e-11 1.0013 0.083045 0.083045 v FourierNb 0.0366 0.090721 0.072233 0.072233 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Csdyn2 0 0.004225 0.0028695 0.0028695 v SpecHeat 1017.2 1017.2 1017.2 1017.2 v ThermalCond 0.2 1 0.6 0.6 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 1.5075e-05 10 2.65 2.65 v Boundary Density 0.97901 1 0.99757 0.99757 v Yplus 8.4512e-05 5.1912 0.9197 0.9197 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.0366 1.0753 0.15528 0.15528 INSTANT 0.584000000E+02 TIME STEP NUMBER 584 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 20800 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00 Friction velocity uet : 0.29238E-06 0.19212E-01 Friction velocity uk : 0.29238E-06 0.19212E-01 Dimensionless distance yplus : 0.79884E-04 0.51895E+01 Friction thermal sca. tstar : -0.22022E+05 0.26181E+05 Rough dim-less th. sca. tplus : 0.14870E-05 0.48301E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 20800 Total number of wall faces : 20800 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.16131E-04 2 0.32721E-05 0.20581E-08 0.91914E-02 c Velocity[X] 0.30258E-09 c Velocity[Y] 0.17555E-08 c Velocity[Z] 0.63315E-17 c Pressure 0.17545E-07 7 0.64902E-05 0.16318E-02 0.26269E-01 c TempC 0.44593E+01 2 0.99611E-05 0.90369E-04 0.74297E-02 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a TempC ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.019645 0.029076 1.6334e-05 1.6334e-05 v Velocity[Y] -0.041596 0.099634 0.00012856 0.00012856 v Velocity[Z] -2.6403e-08 3.2273e-08 -5.779e-10 -5.779e-10 v ǁVelocityǁ 6.3852e-11 0.099635 0.0073528 0.0073528 v Pressure -0.012869 0.041133 1.39e-17 2.2446e-18 v TempC 1.5782e-05 9.9109 2.6252 2.6252 v Density 0.979 1 0.99759 0.99759 v TurbVisc 0 1.186e-05 9.054e-08 9.054e-08 v CourantNb 7.5621e-11 1.0006 0.082985 0.082985 v FourierNb 0.0366 0.090723 0.072233 0.072233 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Csdyn2 0 0.004225 0.0028704 0.0028704 v SpecHeat 1017.2 1017.2 1017.2 1017.2 v ThermalCond 0.2 1 0.6 0.6 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 1.5424e-05 10 2.6522 2.6522 v Boundary Density 0.979 1 0.99756 0.99756 v Yplus 7.9884e-05 5.1895 0.91936 0.91936 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.0366 1.0747 0.15522 0.15522 INSTANT 0.585000000E+02 TIME STEP NUMBER 585 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 20800 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00 Friction velocity uet : 0.27717E-06 0.19206E-01 Friction velocity uk : 0.27717E-06 0.19206E-01 Dimensionless distance yplus : 0.75729E-04 0.51878E+01 Friction thermal sca. tstar : -0.23285E+05 0.27236E+05 Rough dim-less th. sca. tplus : 0.14097E-05 0.48285E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 20800 Total number of wall faces : 20800 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.16122E-04 2 0.32616E-05 0.20528E-08 0.91848E-02 c Velocity[X] 0.30072E-09 c Velocity[Y] 0.17521E-08 c Velocity[Z] 0.53482E-17 c Pressure 0.17506E-07 7 0.64448E-05 0.16267E-02 0.26189E-01 c TempC 0.44605E+01 2 0.99751E-05 0.90109E-04 0.74166E-02 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a TempC ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.019646 0.029038 1.6339e-05 1.6339e-05 v Velocity[Y] -0.041604 0.09957 0.00012864 0.00012864 v Velocity[Z] -2.4463e-08 2.9777e-08 -5.3671e-10 -5.3671e-10 v ǁVelocityǁ 5.6134e-11 0.099571 0.0073481 0.0073481 v Pressure -0.012902 0.041195 9.992e-18 -1.1435e-18 v TempC 1.6114e-05 9.911 2.6273 2.6273 v Density 0.97899 1 0.99758 0.99758 v TurbVisc 0 1.186e-05 9.0514e-08 9.0514e-08 v CourantNb 6.4754e-11 0.99995 0.082925 0.082925 v FourierNb 0.0366 0.090724 0.072234 0.072234 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Csdyn2 0 0.004225 0.0028716 0.0028716 v SpecHeat 1017.2 1017.2 1017.2 1017.2 v ThermalCond 0.2 1 0.6 0.6 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 1.5782e-05 10 2.6543 2.6543 v Boundary Density 0.97899 1 0.99756 0.99756 v Yplus 7.5729e-05 5.1878 0.91903 0.91903 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.0366 1.074 0.15516 0.15516 INSTANT 0.586000000E+02 TIME STEP NUMBER 586 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 20800 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00 Friction velocity uet : 0.26352E-06 0.19200E-01 Friction velocity uk : 0.26352E-06 0.19200E-01 Dimensionless distance yplus : 0.72001E-04 0.51861E+01 Friction thermal sca. tstar : -0.24612E+05 0.28338E+05 Rough dim-less th. sca. tplus : 0.13403E-05 0.48269E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 20800 Total number of wall faces : 20800 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.16113E-04 2 0.32471E-05 0.20463E-08 0.91754E-02 c Velocity[X] 0.29877E-09 c Velocity[Y] 0.17475E-08 c Velocity[Z] 0.45184E-17 c Pressure 0.17455E-07 7 0.63993E-05 0.16206E-02 0.26105E-01 c TempC 0.44618E+01 3 0.87697E-06 0.90160E-04 0.74162E-02 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a TempC ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.019647 0.029 1.6344e-05 1.6344e-05 v Velocity[Y] -0.041612 0.099505 0.00012872 0.00012872 v Velocity[Z] -2.265e-08 2.742e-08 -4.9844e-10 -4.9844e-10 v ǁVelocityǁ 5.1309e-11 0.099505 0.0073434 0.0073434 v Pressure -0.012935 0.041256 1.2035e-17 5.9292e-19 v TempC 1.6424e-05 9.9111 2.6295 2.6295 v Density 0.97898 1 0.99758 0.99758 v TurbVisc 0 1.1861e-05 9.0478e-08 9.0478e-08 v CourantNb 5.501e-11 0.99928 0.082866 0.082866 v FourierNb 0.0366 0.090726 0.072234 0.072234 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Csdyn2 0 0.004225 0.0028722 0.0028722 v SpecHeat 1017.2 1017.2 1017.2 1017.2 v ThermalCond 0.2 1 0.6 0.6 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 1.6114e-05 10 2.6565 2.6565 v Boundary Density 0.97898 1 0.99755 0.99755 v Yplus 7.2001e-05 5.1861 0.91869 0.91869 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.0366 1.0733 0.1551 0.1551 INSTANT 0.587000000E+02 TIME STEP NUMBER 587 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 20800 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00 Friction velocity uet : 0.25127E-06 0.19193E-01 Friction velocity uk : 0.25127E-06 0.19193E-01 Dimensionless distance yplus : 0.68654E-04 0.51844E+01 Friction thermal sca. tstar : -0.25992E+05 0.29488E+05 Rough dim-less th. sca. tplus : 0.12780E-05 0.48253E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 20800 Total number of wall faces : 20800 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.16104E-04 2 0.32321E-05 0.20391E-08 0.91643E-02 c Velocity[X] 0.29680E-09 c Velocity[Y] 0.17423E-08 c Velocity[Z] 0.38181E-17 c Pressure 0.17394E-07 7 0.63553E-05 0.16135E-02 0.26024E-01 c TempC 0.44630E+01 2 0.81528E-05 0.89803E-04 0.73991E-02 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a TempC ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.019648 0.028962 1.6349e-05 1.6349e-05 v Velocity[Y] -0.04162 0.099439 0.00012879 0.00012879 v Velocity[Z] -2.0915e-08 2.5202e-08 -4.629e-10 -4.629e-10 v ǁVelocityǁ 4.8756e-11 0.09944 0.0073387 0.0073387 v Pressure -0.012967 0.041318 1.35e-17 1.567e-18 v TempC 1.6764e-05 9.9112 2.6317 2.6317 v Density 0.97897 1 0.99757 0.99757 v TurbVisc 0 1.1861e-05 9.0434e-08 9.0434e-08 v CourantNb 4.6298e-11 0.99861 0.082806 0.082806 v FourierNb 0.0366 0.090727 0.072234 0.072234 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Csdyn2 0 0.004225 0.0028725 0.0028725 v SpecHeat 1017.2 1017.2 1017.2 1017.2 v ThermalCond 0.2 1 0.6 0.6 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 1.6424e-05 10 2.6586 2.6586 v Boundary Density 0.97897 1 0.99755 0.99755 v Yplus 6.8654e-05 5.1844 0.91835 0.91835 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.0366 1.0727 0.15504 0.15504 INSTANT 0.588000000E+02 TIME STEP NUMBER 588 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 20800 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00 Friction velocity uet : 0.23525E-06 0.19187E-01 Friction velocity uk : 0.23525E-06 0.19187E-01 Dimensionless distance yplus : 0.64276E-04 0.51827E+01 Friction thermal sca. tstar : -0.27457E+05 0.30688E+05 Rough dim-less th. sca. tplus : 0.11965E-05 0.48237E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 20800 Total number of wall faces : 20800 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.16095E-04 2 0.32068E-05 0.20291E-08 0.91470E-02 c Velocity[X] 0.29462E-09 c Velocity[Y] 0.17345E-08 c Velocity[Z] 0.32269E-17 c Pressure 0.17270E-07 7 0.63204E-05 0.16006E-02 0.25967E-01 c TempC 0.44642E+01 2 0.69609E-05 0.89576E-04 0.73873E-02 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a TempC ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.019649 0.028925 1.6354e-05 1.6354e-05 v Velocity[Y] -0.041628 0.099374 0.00012887 0.00012887 v Velocity[Z] -1.9263e-08 2.3119e-08 -4.2988e-10 -4.2988e-10 v ǁVelocityǁ 4.7772e-11 0.099375 0.007334 0.007334 v Pressure -0.013 0.04138 6.9722e-18 -3.854e-18 v TempC 1.7104e-05 9.9113 2.6339 2.6339 v Density 0.97896 1 0.99757 0.99757 v TurbVisc 0 1.1862e-05 9.0385e-08 9.0385e-08 v CourantNb 3.8531e-11 0.99794 0.082746 0.082746 v FourierNb 0.0366 0.090729 0.072234 0.072234 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Csdyn2 0 0.004225 0.0028725 0.0028725 v SpecHeat 1017.2 1017.2 1017.2 1017.2 v ThermalCond 0.2 1 0.6 0.6 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 1.6764e-05 10 2.6608 2.6608 v Boundary Density 0.97896 1 0.99754 0.99754 v Yplus 6.4276e-05 5.1827 0.91802 0.91802 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.0366 1.072 0.15498 0.15498 INSTANT 0.589000000E+02 TIME STEP NUMBER 589 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 20800 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00 Friction velocity uet : 0.18555E-06 0.19181E-01 Friction velocity uk : 0.18555E-06 0.19181E-01 Dimensionless distance yplus : 0.50697E-04 0.51809E+01 Friction thermal sca. tstar : -0.28981E+05 0.31941E+05 Rough dim-less th. sca. tplus : 0.94372E-06 0.48221E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 20800 Total number of wall faces : 20800 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.16086E-04 2 0.32087E-05 0.20243E-08 0.91414E-02 c Velocity[X] 0.29288E-09 c Velocity[Y] 0.17315E-08 c Velocity[Z] 0.27277E-17 c Pressure 0.17280E-07 7 0.62679E-05 0.16002E-02 0.25886E-01 c TempC 0.44654E+01 2 0.88625E-05 0.89286E-04 0.73730E-02 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a TempC ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.019649 0.028887 1.6358e-05 1.6358e-05 v Velocity[Y] -0.041636 0.099308 0.00012895 0.00012895 v Velocity[Z] -1.7697e-08 2.1169e-08 -3.9921e-10 -3.9921e-10 v ǁVelocityǁ 4.772e-11 0.099309 0.0073293 0.0073293 v Pressure -0.013033 0.041442 1.4166e-17 2.6258e-18 v TempC 1.7456e-05 9.9114 2.636 2.636 v Density 0.97894 1 0.99756 0.99756 v TurbVisc 0 1.1862e-05 9.0341e-08 9.0341e-08 v CourantNb 3.1627e-11 0.99726 0.082687 0.082687 v FourierNb 0.0366 0.09073 0.072235 0.072235 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Csdyn2 0 0.004225 0.0028729 0.0028729 v SpecHeat 1017.2 1017.2 1017.2 1017.2 v ThermalCond 0.2 1 0.6 0.6 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 1.7104e-05 10 2.6629 2.6629 v Boundary Density 0.97894 1 0.99754 0.99754 v Yplus 5.0697e-05 5.1809 0.91768 0.91768 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.0366 1.0713 0.15492 0.15492 INSTANT 0.590000000E+02 TIME STEP NUMBER 590 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 20800 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00 Friction velocity uet : 0.16027E-06 0.19174E-01 Friction velocity uk : 0.16027E-06 0.19174E-01 Dimensionless distance yplus : 0.43789E-04 0.51792E+01 Friction thermal sca. tstar : -0.30574E+05 0.33249E+05 Rough dim-less th. sca. tplus : 0.81511E-06 0.48205E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 20800 Total number of wall faces : 20800 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.16077E-04 2 0.31999E-05 0.20187E-08 0.91338E-02 c Velocity[X] 0.29110E-09 c Velocity[Y] 0.17276E-08 c Velocity[Z] 0.23061E-17 c Pressure 0.17255E-07 7 0.62256E-05 0.15965E-02 0.25807E-01 c TempC 0.44666E+01 2 0.41290E-05 0.89113E-04 0.73634E-02 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a TempC ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.01965 0.02885 1.6363e-05 1.6363e-05 v Velocity[Y] -0.041644 0.099241 0.00012902 0.00012902 v Velocity[Z] -1.6219e-08 1.9496e-08 -3.7072e-10 -3.7072e-10 v ǁVelocityǁ 4.811e-11 0.099242 0.0073246 0.0073246 v Pressure -0.013066 0.041503 5.862e-18 -5.3787e-18 v TempC 1.7814e-05 9.9115 2.6382 2.6382 v Density 0.97893 1 0.99756 0.99756 v TurbVisc 0 1.1863e-05 9.0296e-08 9.0296e-08 v CourantNb 2.5512e-11 0.99658 0.082627 0.082627 v FourierNb 0.0366 0.090732 0.072235 0.072235 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Csdyn2 0 0.004225 0.0028732 0.0028732 v SpecHeat 1017.2 1017.2 1017.2 1017.2 v ThermalCond 0.2 1 0.6 0.6 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 1.7456e-05 10 2.6651 2.6651 v Boundary Density 0.97893 1 0.99753 0.99753 v Yplus 4.3789e-05 5.1792 0.91735 0.91735 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.0366 1.0706 0.15486 0.15486 INSTANT 0.591000000E+02 TIME STEP NUMBER 591 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 20800 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00 Friction velocity uet : 0.12298E-06 0.19168E-01 Friction velocity uk : 0.12298E-06 0.19168E-01 Dimensionless distance yplus : 0.33602E-04 0.51775E+01 Friction thermal sca. tstar : -0.32235E+05 0.34613E+05 Rough dim-less th. sca. tplus : 0.62549E-06 0.48189E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 20800 Total number of wall faces : 20800 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.16068E-04 2 0.31942E-05 0.20123E-08 0.91245E-02 c Velocity[X] 0.28926E-09 c Velocity[Y] 0.17231E-08 c Velocity[Z] 0.19499E-17 c Pressure 0.17231E-07 7 0.61832E-05 0.15929E-02 0.25728E-01 c TempC 0.44679E+01 2 0.65131E-05 0.89009E-04 0.73567E-02 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a TempC ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.019651 0.028813 1.6368e-05 1.6368e-05 v Velocity[Y] -0.041651 0.099175 0.0001291 0.0001291 v Velocity[Z] -1.4831e-08 1.82e-08 -3.4425e-10 -3.4425e-10 v ǁVelocityǁ 4.8615e-11 0.099176 0.0073199 0.0073199 v Pressure -0.013099 0.041565 9.8144e-18 -1.5247e-18 v TempC 1.8188e-05 9.9116 2.6404 2.6404 v Density 0.97892 1 0.99755 0.99755 v TurbVisc 0 1.1864e-05 9.0264e-08 9.0264e-08 v CourantNb 2.0113e-11 0.99591 0.082568 0.082568 v FourierNb 0.0366 0.090733 0.072235 0.072235 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Csdyn2 0 0.004225 0.0028744 0.0028744 v SpecHeat 1017.2 1017.2 1017.2 1017.2 v ThermalCond 0.2 1 0.6 0.6 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 1.7814e-05 10 2.6672 2.6672 v Boundary Density 0.97892 1 0.99753 0.99753 v Yplus 3.3602e-05 5.1775 0.91702 0.91702 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.0366 1.07 0.1548 0.1548 INSTANT 0.592000000E+02 TIME STEP NUMBER 592 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 20800 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00 Friction velocity uet : 0.83343E-07 0.19162E-01 Friction velocity uk : 0.83343E-07 0.19162E-01 Dimensionless distance yplus : 0.22771E-04 0.51757E+01 Friction thermal sca. tstar : -0.33975E+05 0.36036E+05 Rough dim-less th. sca. tplus : 0.42388E-06 0.48172E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 20800 Total number of wall faces : 20800 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.16059E-04 2 0.31811E-05 0.20057E-08 0.91145E-02 c Velocity[X] 0.28745E-09 c Velocity[Y] 0.17182E-08 c Velocity[Z] 0.16490E-17 c Pressure 0.17176E-07 7 0.61431E-05 0.15865E-02 0.25654E-01 c TempC 0.44691E+01 2 0.77955E-05 0.88748E-04 0.73435E-02 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a TempC ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.019652 0.028776 1.6372e-05 1.6372e-05 v Velocity[Y] -0.041659 0.099108 0.00012917 0.00012917 v Velocity[Z] -1.3531e-08 1.6952e-08 -3.1967e-10 -3.1967e-10 v ǁVelocityǁ 4.904e-11 0.099109 0.0073153 0.0073153 v Pressure -0.013132 0.041626 1.0791e-17 -1.1858e-18 v TempC 1.8573e-05 9.9116 2.6425 2.6425 v Density 0.97891 1 0.99755 0.99755 v TurbVisc 0 1.1864e-05 9.0228e-08 9.0228e-08 v CourantNb 1.5363e-11 0.99525 0.082508 0.082508 v FourierNb 0.0366 0.090735 0.072235 0.072235 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Csdyn2 0 0.004225 0.0028754 0.0028754 v SpecHeat 1017.2 1017.2 1017.2 1017.2 v ThermalCond 0.2 1 0.6 0.6 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 1.8188e-05 10 2.6694 2.6694 v Boundary Density 0.97891 1 0.99752 0.99752 v Yplus 2.2771e-05 5.1757 0.91668 0.91668 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.0366 1.0693 0.15474 0.15474 INSTANT 0.593000000E+02 TIME STEP NUMBER 593 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 20800 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00 Friction velocity uet : 0.48985E-07 0.19155E-01 Friction velocity uk : 0.48985E-07 0.19155E-01 Dimensionless distance yplus : 0.13384E-04 0.51740E+01 Friction thermal sca. tstar : -0.35792E+05 0.37521E+05 Rough dim-less th. sca. tplus : 0.24914E-06 0.48156E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 20800 Total number of wall faces : 20800 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.16050E-04 2 0.31765E-05 0.20008E-08 0.91085E-02 c Velocity[X] 0.28582E-09 c Velocity[Y] 0.17150E-08 c Velocity[Z] 0.13948E-17 c Pressure 0.17154E-07 7 0.61029E-05 0.15831E-02 0.25590E-01 c TempC 0.44703E+01 2 0.68227E-05 0.88539E-04 0.73325E-02 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a TempC ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.019653 0.028739 1.6377e-05 1.6377e-05 v Velocity[Y] -0.041666 0.099041 0.00012925 0.00012925 v Velocity[Z] -1.2394e-08 1.5754e-08 -2.9684e-10 -2.9684e-10 v ǁVelocityǁ 4.9276e-11 0.099042 0.0073106 0.0073106 v Pressure -0.013165 0.041687 8.4377e-18 -2.8799e-18 v TempC 1.8967e-05 9.9117 2.6447 2.6447 v Density 0.9789 1 0.99754 0.99754 v TurbVisc 0 1.1865e-05 9.0179e-08 9.0179e-08 v CourantNb 1.1202e-11 0.9946 0.082449 0.082449 v FourierNb 0.0366 0.090736 0.072236 0.072236 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Csdyn2 0 0.004225 0.0028753 0.0028753 v SpecHeat 1017.2 1017.2 1017.2 1017.2 v ThermalCond 0.2 1 0.6 0.6 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 1.8573e-05 10 2.6715 2.6715 v Boundary Density 0.9789 1 0.99752 0.99752 v Yplus 1.3384e-05 5.174 0.91635 0.91635 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.0366 1.0687 0.15468 0.15468 INSTANT 0.594000000E+02 TIME STEP NUMBER 594 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 20800 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00 Friction velocity uet : 0.74735E-07 0.19149E-01 Friction velocity uk : 0.74735E-07 0.19149E-01 Dimensionless distance yplus : 0.20420E-04 0.51722E+01 Friction thermal sca. tstar : -0.38864E+05 0.39070E+05 Rough dim-less th. sca. tplus : 0.38010E-06 0.48140E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 20800 Total number of wall faces : 20800 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.16040E-04 2 0.31728E-05 0.19955E-08 0.91015E-02 c Velocity[X] 0.28415E-09 c Velocity[Y] 0.17113E-08 c Velocity[Z] 0.11799E-17 c Pressure 0.17132E-07 7 0.60620E-05 0.15797E-02 0.25513E-01 c TempC 0.44715E+01 2 0.84611E-05 0.88256E-04 0.73184E-02 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a TempC ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.019654 0.028702 1.6381e-05 1.6381e-05 v Velocity[Y] -0.041674 0.098974 0.00012933 0.00012933 v Velocity[Z] -1.1379e-08 1.461e-08 -2.7563e-10 -2.7563e-10 v ǁVelocityǁ 4.9278e-11 0.098975 0.0073059 0.0073059 v Pressure -0.013197 0.041749 1.2568e-17 3.3881e-19 v TempC 1.9371e-05 9.9118 2.6469 2.6469 v Density 0.97889 1 0.99754 0.99754 v TurbVisc 0 1.1865e-05 9.0135e-08 9.0135e-08 v CourantNb 7.5715e-12 0.99394 0.08239 0.08239 v FourierNb 0.0366 0.090738 0.072236 0.072236 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Csdyn2 0 0.004225 0.0028757 0.0028757 v SpecHeat 1017.2 1017.2 1017.2 1017.2 v ThermalCond 0.2 1 0.6 0.6 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 1.8967e-05 10 2.6737 2.6737 v Boundary Density 0.97889 1 0.99752 0.99752 v Yplus 2.042e-05 5.1722 0.91602 0.91602 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.0366 1.068 0.15463 0.15463 INSTANT 0.595000000E+02 TIME STEP NUMBER 595 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 20800 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00 Friction velocity uet : 0.95363E-07 0.19143E-01 Friction velocity uk : 0.95363E-07 0.19143E-01 Dimensionless distance yplus : 0.26055E-04 0.51704E+01 Friction thermal sca. tstar : -0.42936E+05 0.40685E+05 Rough dim-less th. sca. tplus : 0.48501E-06 0.48123E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 20800 Total number of wall faces : 20800 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.16031E-04 2 0.31483E-05 0.19893E-08 0.90926E-02 c Velocity[X] 0.28246E-09 c Velocity[Y] 0.17068E-08 c Velocity[Z] 0.99835E-18 c Pressure 0.17080E-07 7 0.60234E-05 0.15736E-02 0.25437E-01 c TempC 0.44727E+01 2 0.68366E-05 0.88081E-04 0.73088E-02 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a TempC ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.019654 0.028665 1.6385e-05 1.6385e-05 v Velocity[Y] -0.041681 0.098907 0.0001294 0.0001294 v Velocity[Z] -1.0507e-08 1.352e-08 -2.5593e-10 -2.5593e-10 v ǁVelocityǁ 4.9032e-11 0.098908 0.0073012 0.0073012 v Pressure -0.01323 0.04181 8.0824e-18 -4.1081e-18 v TempC 1.9788e-05 9.9119 2.649 2.649 v Density 0.97887 1 0.99753 0.99753 v TurbVisc 0 1.1866e-05 9.0092e-08 9.0092e-08 v CourantNb 4.4196e-12 0.99328 0.08233 0.08233 v FourierNb 0.0366 0.090739 0.072236 0.072236 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Csdyn2 0 0.004225 0.0028761 0.0028761 v SpecHeat 1017.2 1017.2 1017.2 1017.2 v ThermalCond 0.2 1 0.6 0.6 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 1.9371e-05 10 2.6758 2.6758 v Boundary Density 0.97887 1 0.99751 0.99751 v Yplus 2.6055e-05 5.1704 0.91569 0.91569 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.0366 1.0673 0.15457 0.15457 INSTANT 0.596000000E+02 TIME STEP NUMBER 596 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 20800 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00 Friction velocity uet : 0.10816E-06 0.19136E-01 Friction velocity uk : 0.10816E-06 0.19136E-01 Dimensionless distance yplus : 0.29551E-04 0.51686E+01 Friction thermal sca. tstar : -0.47862E+05 0.42371E+05 Rough dim-less th. sca. tplus : 0.55008E-06 0.48107E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 20800 Total number of wall faces : 20800 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.16022E-04 2 0.31351E-05 0.19825E-08 0.90822E-02 c Velocity[X] 0.28071E-09 c Velocity[Y] 0.17018E-08 c Velocity[Z] 0.84484E-18 c Pressure 0.17039E-07 7 0.59835E-05 0.15685E-02 0.25361E-01 c TempC 0.44739E+01 2 0.88828E-05 0.87848E-04 0.72968E-02 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a TempC ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.019655 0.028629 1.639e-05 1.639e-05 v Velocity[Y] -0.041688 0.098839 0.00012948 0.00012948 v Velocity[Z] -9.703e-09 1.2487e-08 -2.3763e-10 -2.3763e-10 v ǁVelocityǁ 4.6823e-11 0.09884 0.0072966 0.0072966 v Pressure -0.013263 0.041871 1.763e-17 6.0139e-18 v TempC 2.022e-05 9.912 2.6512 2.6512 v Density 0.97886 1 0.99753 0.99753 v TurbVisc 0 1.1866e-05 9.0042e-08 9.0042e-08 v CourantNb 1.6978e-12 0.99262 0.082271 0.082271 v FourierNb 0.0366 0.09074 0.072236 0.072236 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Csdyn2 0 0.004225 0.0028761 0.0028761 v SpecHeat 1017.2 1017.2 1017.2 1017.2 v ThermalCond 0.2 1 0.6 0.6 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 1.9788e-05 10 2.678 2.678 v Boundary Density 0.97886 1 0.99751 0.99751 v Yplus 2.9551e-05 5.1686 0.91536 0.91536 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.0366 1.0667 0.15451 0.15451 INSTANT 0.597000000E+02 TIME STEP NUMBER 597 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 20800 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00 Friction velocity uet : 0.11613E-06 0.19130E-01 Friction velocity uk : 0.11613E-06 0.19130E-01 Dimensionless distance yplus : 0.31729E-04 0.51669E+01 Friction thermal sca. tstar : -0.53709E+05 0.44127E+05 Rough dim-less th. sca. tplus : 0.59063E-06 0.48090E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 20800 Total number of wall faces : 20800 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.16013E-04 2 0.31278E-05 0.19757E-08 0.90716E-02 c Velocity[X] 0.27898E-09 c Velocity[Y] 0.16967E-08 c Velocity[Z] 0.71506E-18 c Pressure 0.16984E-07 7 0.59456E-05 0.15621E-02 0.25288E-01 c TempC 0.44751E+01 2 0.91151E-05 0.87640E-04 0.72858E-02 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a TempC ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.019656 0.028593 1.6394e-05 1.6394e-05 v Velocity[Y] -0.041695 0.098771 0.00012955 0.00012955 v Velocity[Z] -8.9604e-09 1.1509e-08 -2.2063e-10 -2.2063e-10 v ǁVelocityǁ 4.2434e-11 0.098772 0.0072919 0.0072919 v Pressure -0.013297 0.041932 8.9262e-18 -2.8799e-18 v TempC 2.0664e-05 9.9121 2.6533 2.6533 v Density 0.97885 1 0.99752 0.99752 v TurbVisc 0 1.1867e-05 9e-08 9e-08 v CourantNb 6.3228e-13 0.99196 0.082212 0.082212 v FourierNb 0.0366 0.090742 0.072237 0.072237 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Csdyn2 0 0.004225 0.0028769 0.0028769 v SpecHeat 1017.2 1017.2 1017.2 1017.2 v ThermalCond 0.2 1 0.6 0.6 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 2.022e-05 10 2.6801 2.6801 v Boundary Density 0.97885 1 0.9975 0.9975 v Yplus 3.1729e-05 5.1669 0.91504 0.91504 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.0366 1.066 0.15445 0.15445 INSTANT 0.598000000E+02 TIME STEP NUMBER 598 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 20800 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00 Friction velocity uet : 0.12083E-06 0.19123E-01 Friction velocity uk : 0.12083E-06 0.19123E-01 Dimensionless distance yplus : 0.33015E-04 0.51651E+01 Friction thermal sca. tstar : -0.61018E+05 0.45960E+05 Rough dim-less th. sca. tplus : 0.61456E-06 0.48073E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 20800 Total number of wall faces : 20800 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.16004E-04 2 0.31344E-05 0.19689E-08 0.90611E-02 c Velocity[X] 0.27726E-09 c Velocity[Y] 0.16916E-08 c Velocity[Z] 0.60532E-18 c Pressure 0.16949E-07 7 0.59070E-05 0.15576E-02 0.25215E-01 c TempC 0.44763E+01 3 0.86249E-06 0.87649E-04 0.72838E-02 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a TempC ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.019657 0.028557 1.6398e-05 1.6398e-05 v Velocity[Y] -0.041702 0.098703 0.00012963 0.00012963 v Velocity[Z] -8.2748e-09 1.0588e-08 -2.0485e-10 -2.0485e-10 v ǁVelocityǁ 3.6994e-11 0.098704 0.0072873 0.0072873 v Pressure -0.01333 0.041993 4.5297e-18 -7.8774e-18 v TempC 2.1109e-05 9.9122 2.6555 2.6555 v Density 0.97884 1 0.99752 0.99752 v TurbVisc 0 1.1867e-05 8.9962e-08 8.9962e-08 v CourantNb 2.6239e-12 0.99129 0.082153 0.082153 v FourierNb 0.0366 0.090743 0.072237 0.072237 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Csdyn2 0 0.004225 0.0028776 0.0028776 v SpecHeat 1017.2 1017.2 1017.2 1017.2 v ThermalCond 0.2 1 0.6 0.6 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 2.0664e-05 10 2.6822 2.6822 v Boundary Density 0.97884 1 0.9975 0.9975 v Yplus 3.3015e-05 5.1651 0.91471 0.91471 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.0366 1.0653 0.15439 0.15439 INSTANT 0.599000000E+02 TIME STEP NUMBER 599 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 20800 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00 Friction velocity uet : 0.11482E-06 0.19117E-01 Friction velocity uk : 0.11482E-06 0.19117E-01 Dimensionless distance yplus : 0.31372E-04 0.51633E+01 Friction thermal sca. tstar : -0.69966E+05 0.47871E+05 Rough dim-less th. sca. tplus : 0.58398E-06 0.48057E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 20800 Total number of wall faces : 20800 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.15995E-04 2 0.31371E-05 0.19618E-08 0.90499E-02 c Velocity[X] 0.27554E-09 c Velocity[Y] 0.16863E-08 c Velocity[Z] 0.51251E-18 c Pressure 0.16905E-07 7 0.58700E-05 0.15523E-02 0.25140E-01 c TempC 0.44775E+01 2 0.75692E-05 0.87333E-04 0.72683E-02 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a TempC ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.019657 0.028521 1.6403e-05 1.6403e-05 v Velocity[Y] -0.041709 0.098635 0.0001297 0.0001297 v Velocity[Z] -7.6418e-09 9.7219e-09 -1.9019e-10 -1.9019e-10 v ǁVelocityǁ 2.8052e-11 0.098636 0.0072826 0.0072826 v Pressure -0.013363 0.042054 1.0436e-17 -1.4823e-18 v TempC 2.1588e-05 9.9123 2.6577 2.6577 v Density 0.97883 1 0.99751 0.99751 v TurbVisc 0 1.1868e-05 8.9928e-08 8.9928e-08 v CourantNb 4.3077e-12 0.99062 0.082094 0.082094 v FourierNb 0.0366 0.090745 0.072237 0.072237 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Csdyn2 0 0.004225 0.0028787 0.0028787 v SpecHeat 1017.2 1017.2 1017.2 1017.2 v ThermalCond 0.2 1 0.6 0.6 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 2.1109e-05 10 2.6844 2.6844 v Boundary Density 0.97883 1 0.99749 0.99749 v Yplus 3.1372e-05 5.1633 0.91438 0.91438 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.0366 1.0647 0.15433 0.15433 INSTANT 0.600000000E+02 TIME STEP NUMBER 600 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 0 0.000000000E+00 Smooth wall 5 20800 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 0 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00 Friction velocity uet : 0.10987E-06 0.19110E-01 Friction velocity uk : 0.10987E-06 0.19110E-01 Dimensionless distance yplus : 0.30018E-04 0.51616E+01 Friction thermal sca. tstar : -0.81080E+05 0.49863E+05 Rough dim-less th. sca. tplus : 0.55878E-06 0.48041E+00 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 20800 Total number of wall faces : 20800 ------------------------------------------------------------ Write final restart files checkpoint at iteration 600, Physical time 0.60000E+02 ** Writing the main restart file ----------------------------- Start writing Wrote field names and types to checkpoint at iteration 600: checkpoint/main End writing the options Wrote main variables to checkpoint: checkpoint/main End writing ** Writing the auxiliary restart file ---------------------------------- Start writing End writing the dimensions and options End writing the physical properties End writing the time step Wrote boundary condition coefficients to checkpoint: checkpoint/auxiliary End writing the source terms End writing ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.15986E-04 2 0.31232E-05 0.19515E-08 0.90311E-02 c Velocity[X] 0.27358E-09 c Velocity[Y] 0.16779E-08 c Velocity[Z] 0.43400E-18 c Pressure 0.16789E-07 7 0.58407E-05 0.15403E-02 0.25083E-01 c TempC 0.44787E+01 2 0.74854E-05 0.87112E-04 0.72568E-02 ---------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----- -------------- -------------- ------------ ------------ a TempC ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.019658 0.028485 1.6407e-05 1.6407e-05 v Velocity[Y] -0.041716 0.098567 0.00012978 0.00012978 v Velocity[Z] -7.0574e-09 8.91e-09 -1.7657e-10 -1.7657e-10 v ǁVelocityǁ 2.1597e-11 0.098568 0.007278 0.007278 v Pressure -0.013396 0.042115 1.4655e-17 2.8799e-18 v TempC 2.2061e-05 9.9124 2.6598 2.6598 v Density 0.97882 1 0.99751 0.99751 v TurbVisc 0 1.1868e-05 8.9878e-08 8.9878e-08 v CourantNb 5.7174e-12 0.98995 0.082035 0.082035 v FourierNb 0.0366 0.090746 0.072237 0.072237 v total_pressure 1.0132e+05 1.0132e+05 1.0132e+05 1.0132e+05 v Csdyn2 0 0.004225 0.0028787 0.0028787 v SpecHeat 1017.2 1017.2 1017.2 1017.2 v ThermalCond 0.2 1 0.6 0.6 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 2.1588e-05 10 2.6865 2.6865 v Boundary Density 0.97882 1 0.99749 0.99749 v Yplus 3.0018e-05 5.1616 0.91406 0.91406 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.0366 1.064 0.15427 0.15427 =============================================================== FINAL STAGE OF THE CALCULATION ============================== =========================================================== =========================================================== END OF CALCULATION ================== =============================================================== Destroying structures and ending computation