---------------------------------------- Begin PBS Prologue Wed Oct 16 19:15:51 EDT 2013 1381965351 Job ID: 1706649.egeon2 Username: mehdizde Group: etienne Nodes: node-c3-47 End PBS Prologue Wed Oct 16 19:15:51 EDT 2013 1381965351 ---------------------------------------- Code_Saturne is running *********************** Version: 3.0.0 Path: /home/apps/Logiciels/saturne/saturne-dev/installation/code_saturne-3.0.0 Result directory: /exec5/GROUP/etienne/mehdizde/CANDUtransient.02/RESU/_6 Parallel code_saturne on 6 processes. **************************** Preparing calculation data **************************** *************************** Preprocessing calculation *************************** sh: module: line 1: syntax error: unexpected end of file sh: error importing function definition for `module' /bin/bash: module: line 1: syntax error: unexpected end of file /bin/bash: error importing function definition for `module' ********************** Starting calculation ********************** /bin/bash: module: line 1: syntax error: unexpected end of file /bin/bash: error importing function definition for `module' /exec5/GROUP/etienne/mehdizde/CANDUtransient.02/RESU/_6/run_solver.sh: line 10: module: command not found command: command: command: /home/apps/Logiciels/saturne/saturne-dev/installation/code_saturne-3.0.0/libexec/code_saturne/cs_solver --param fm --log 0 --logp 0 --mpi *************************************************************** (R) Code_Saturne Version 3.0.0 Copyright (C) 1998-2013 EDF S.A., France build Wed Oct 16 10:15:53 2013 MPI version 2.1 (Open MPI 1.6.4) 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: Wed Oct 16 19:16:22 2013 System: Linux 2.6.32-279.el6.x86_64 Machine: node-c3-47 /home/apps/Logiciels/saturne/saturne-dev/installation/code_saturne-3.0.0/libexec/code_saturne/cs_solver --param fm --log 0 --logp 0 --mpi *************************************************************** (R) Code_Saturne Version 3.0.0 Copyright (C) 1998-2013 EDF S.A., France build Wed Oct 16 10:15:53 2013 MPI version 2.1 (Open MPI 1.6.4) 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: Wed Oct 16 19:16:22 2013 System: Linux 2.6.32-279.el6.x86_64 Machine: node-c3-47 /home/apps/Logiciels/saturne/saturne-dev/installation/code_saturne-3.0.0/libexec/code_saturne/cs_solver --param fm --log 0 --logp 0 --mpi *************************************************************** (R) Code_Saturne Version 3.0.0 Copyright (C) 1998-2013 EDF S.A., France build Wed Oct 16 10:15:53 2013 MPI version 2.1 (Open MPI 1.6.4) 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: Wed Oct 16 19:16:22 2013 System: Linux 2.6.32-279.el6.x86_64 Machine: node-c3-47 command: /home/apps/Logiciels/saturne/saturne-dev/installation/code_saturne-3.0.0/libexec/code_saturne/cs_solver --param fm --log 0 --logp 0 --mpi *************************************************************** (R) Code_Saturne Version 3.0.0 Copyright (C) 1998-2013 EDF S.A., France build Wed Oct 16 10:15:53 2013 MPI version 2.1 (Open MPI 1.6.4) 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: Wed Oct 16 19:16:22 2013 System: Linux 2.6.32-279.el6.x86_64 Machine: node-c3-47 Processor: model name : Intel(R) Xeon(R) CPU X5650 @ 2.67GHz Memory: 48256 MB Processor: model name : Intel(R) Xeon(R) CPU X5650 @ 2.67GHz Memory: 48256 MB command: /home/apps/Logiciels/saturne/saturne-dev/installation/code_saturne-3.0.0/libexec/code_saturne/cs_solver --param fm --log 0 --logp 0 --mpi *************************************************************** (R) Code_Saturne Version 3.0.0 Copyright (C) 1998-2013 EDF S.A., France build Wed Oct 16 10:15:53 2013 MPI version 2.1 (Open MPI 1.6.4) 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: Wed Oct 16 19:16:22 2013 System: Linux 2.6.32-279.el6.x86_64 Machine: node-c3-47 Processor: model name : Intel(R) Xeon(R) CPU X5650 @ 2.67GHz Memory: 48256 MB command: /home/apps/Logiciels/saturne/saturne-dev/installation/code_saturne-3.0.0/libexec/code_saturne/cs_solver --param fm --log 0 --logp 0 --mpi *************************************************************** (R) Code_Saturne Version 3.0.0 Copyright (C) 1998-2013 EDF S.A., France build Wed Oct 16 10:15:53 2013 MPI version 2.1 (Open MPI 1.6.4) 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: Wed Oct 16 19:16:22 2013 System: Linux 2.6.32-279.el6.x86_64 Machine: node-c3-47 Processor: model name : Intel(R) Xeon(R) CPU X5650 @ 2.67GHz Memory: 48256 MB Processor: model name : Intel(R) Xeon(R) CPU X5650 @ 2.67GHz Memory: 48256 MB Processor: model name : Intel(R) Xeon(R) CPU X5650 @ 2.67GHz Memory: 48256 MB User: mehdizde (Foad Mehdi zdeh) Directory: /exec5/GROUP/etienne/mehdizde/CANDUtransient.02/RESU/_6 MPI ranks: 6 (appnum attribute: 0) User: mehdizde (Foad Mehdi zdeh) Directory: /exec5/GROUP/etienne/mehdizde/CANDUtransient.02/RESU/_6 MPI ranks: 6 (appnum attribute: 0) User: mehdizde (Foad Mehdi zdeh) Directory: /exec5/GROUP/etienne/mehdizde/CANDUtransient.02/RESU/_6 MPI ranks: 6 (appnum attribute: 0) User: mehdizde (Foad Mehdi zdeh) Directory: /exec5/GROUP/etienne/mehdizde/CANDUtransient.02/RESU/_6 MPI ranks: 6 (appnum attribute: 0) User: mehdizde (Foad Mehdi zdeh) Directory: /exec5/GROUP/etienne/mehdizde/CANDUtransient.02/RESU/_6 MPI ranks: 6 (appnum attribute: 0) User: mehdizde (Foad Mehdi zdeh) Directory: /exec5/GROUP/etienne/mehdizde/CANDUtransient.02/RESU/_6 MPI ranks: 6 (appnum attribute: 0) I/O read method: standard input and output, parallel access I/O write method: standard input and output, serial access I/O rank step: 1 I/O read method: standard input and output, parallel access I/O write method: standard input and output, serial access I/O rank step: 1 I/O read method: standard input and output, parallel access I/O write method: standard input and output, serial access I/O rank step: 1 I/O read method: standard input and output, parallel access I/O write method: standard input and output, serial access I/O rank step: 1 I/O read method: standard input and output, parallel access I/O write method: standard input and output, serial access I/O rank step: 1 I/O read method: standard input and output, parallel access I/O write method: standard input and output, serial access I/O rank step: 1 External libraries for partitioning: PT-SCOTCH 6.0.0 Reading metadata from file: "mesh_input" Reading metadata from file: "mesh_input" Reading metadata from file: "mesh_input" Reading metadata from file: "mesh_input" Reading metadata from file: "mesh_input" Reading metadata from file: "mesh_input" =============================================================== CALCULATION PREPARATION ======================= =========================================================== =============================================================== CALCULATION PREPARATION ======================= =========================================================== =============================================================== CALCULATION PREPARATION ======================= =========================================================== =============================================================== CALCULATION PREPARATION ======================= =========================================================== =============================================================== CALCULATION PREPARATION ======================= =========================================================== =============================================================== CALCULATION PREPARATION ======================= =========================================================== No error detected during the data verification cs_user_parameters.f90 and others). =========================================================== CALCULATION PARAMETERS SUMMARY ============================== ----------------------------------------------------------- ** DIMENSIONS ---------- --- Geometry NPRFML = 1 (Nb max. family properties ) NFML = 10 (Nb families ) --- Physics NVAR = 7 (Nb variables ) NSCAL = 1 (Nb scalars ) NSCAUS = 1 (Nb user scalars ) NSCAPP = 0 (Nb specific physics scalars ) NPROCE = 8 (Nb cell properties ) NPROFA = 1 (Nb internal face properties ) NPROFB = 2 (Nb boundary face properties ) ----------------------------------------------------------- ** PHYSICAL PROPERTIES ------------------- GX = 0.00000E+00 (Gravity x component ) GY = -0.98100E+01 (Gravity y component ) GZ = 0.00000E+00 (Gravity z component ) OMEGAX = 0.00000E+00 (Rotation vector x component ) OMEGAY = 0.00000E+00 (Rotation vector y component ) OMEGAZ = 0.00000E+00 (Rotation vector z component ) ICORIO = 0 (Coriolis source terms ) -- Continuous phase: RO0 = 0.99829E+03 (Reference density ) VISCL0 = 0.10050E-02 (Ref. molecular dyn. visc. ) CP0 = 0.41800E+04 (Ref. specific heat ) ICP = 7 (> 0: variable CP (usphyv) ) P0 = 0.10132E+06 (Ref. total pressure ) PRED0 = 0.00000E+00 (Ref. reduced pressure ) T0 = 0.29315E+03 (Ref. temperature ) IROVAR = 1 (Density constant(0) or not(1) IVIVAR = 1 (Molec. visc cst.(0) or not(1) Initial reference point for pressure XYZP0 = 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------- ** TURBULENCE ---------- --- Continuous phase: - Commons No error detected during the data verification cs_user_parameters.f90 and others). =========================================================== CALCULATION PARAMETERS SUMMARY ============================== ----------------------------------------------------------- ** DIMENSIONS ---------- --- Geometry NPRFML = 1 (Nb max. family properties ) NFML = 10 (Nb families ) --- Physics NVAR = 7 (Nb variables ) NSCAL = 1 (Nb scalars ) NSCAUS = 1 (Nb user scalars ) NSCAPP = 0 (Nb specific physics scalars ) NPROCE = 8 (Nb cell properties ) NPROFA = 1 (Nb internal face properties ) NPROFB = 2 (Nb boundary face properties ) ----------------------------------------------------------- ** PHYSICAL PROPERTIES ------------------- GX = 0.00000E+00 (Gravity x component ) GY = -0.98100E+01 (Gravity y component ) GZ = 0.00000E+00 (Gravity z component ) OMEGAX = 0.00000E+00 (Rotation vector x component ) OMEGAY = 0.00000E+00 (Rotation vector y component ) OMEGAZ = 0.00000E+00 (Rotation vector z component ) ICORIO = 0 (Coriolis source terms ) -- Continuous phase: RO0 = 0.99829E+03 (Reference density ) VISCL0 = 0.10050E-02 (Ref. molecular dyn. visc. ) CP0 = 0.41800E+04 (Ref. specific heat ) ICP = 7 (> 0: variable CP (usphyv) ) P0 = 0.10132E+06 (Ref. total pressure ) PRED0 = 0.00000E+00 (Ref. reduced pressure ) T0 = 0.29315E+03 (Ref. temperature ) IROVAR = 1 (Density constant(0) or not(1) IVIVAR = 1 (Molec. visc cst.(0) or not(1) Initial reference point for pressure XYZP0 = 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------- ** TURBULENCE ---------- --- Continuous phase: - Commons ITURB = 20 (Turbulence model ) IDEUCH = 2 (0: one-scale model ) (1: two-scale model ) (2: invariant wall function ) IWALLT = 0 (Exch. coeff. correlation ) (0: not activated ) (1: activated ) YPLULI = 0.10880E+02 (Limit Y+ ) ILOGPO = 1 (0: power law (forbidden for k-epsilon) ) (1: one-scale log law ) IGRHOK = 0 (1: computed Grad(rho k) ) ISCALT = 1 (Temperature salar number ) - k-epsilon (ITURB = 20) ALMAX = -0.99900E+03 (Characteristic length ) UREF = 0.53000E+01 (Characteristic velocity ) ICLKEP = 0 (k-epsilon clipping model ) IKECOU = 1 (k-epsilon coupling mode ) IGRAKE = 0 (Account for gravity ) - Rotation/curvature correction IRCCOR = 0 (0: desactivated ) (1: activated ) --- Constants - Commons XKAPPA = 0.42000E+00 (Von Karman constant ) CSTLOG = 0.52000E+01 (U+=Log(y+)/kappa +CSTLOG ) APOW = 0.83000E+01 (U+=APOW (y+)**BPOW (W&W law)) BPOW = 0.14286E+00 (U+=APOW (y+)**BPOW (W&W law)) - k-epsilon (ITURB = 20) Ce1 = 0.14400E+01 (Cepsilon 1: production coef.) CE2 = 0.19200E+01 (Cepsilon 2: dissipat. coef.) SIGMAK = 0.10000E+01 (Prandtl relative to k ) SIGMAE = 0.13000E+01 (Prandtl relative to epsilon ) CMU = 0.90000E-01 (Cmu constant ) ----------------------------------------------------------- ** SECONDARY VISCOSITY ------------------- --- Continuous phase: IVISSE = 1 (1: accounted for ) ----------------------------------------------------------- ITURB = 20 (Turbulence model ) IDEUCH = 2 (0: one-scale model ) (1: two-scale model ) (2: invariant wall function ) IWALLT = 0 (Exch. coeff. correlation ) (0: not activated ) (1: activated ) YPLULI = 0.10880E+02 (Limit Y+ ) ILOGPO = 1 (0: power law (forbidden for k-epsilon) ) (1: one-scale log law ) IGRHOK = 0 (1: computed Grad(rho k) ) ISCALT = 1 (Temperature salar number ) - k-epsilon (ITURB = 20) ALMAX = -0.99900E+03 (Characteristic length ) UREF = 0.53000E+01 (Characteristic velocity ) ICLKEP = 0 (k-epsilon clipping model ) IKECOU = 1 (k-epsilon coupling mode ) IGRAKE = 0 (Account for gravity ) - Rotation/curvature correction IRCCOR = 0 (0: desactivated ) (1: activated ) --- Constants - Commons XKAPPA = 0.42000E+00 (Von Karman constant ) CSTLOG = 0.52000E+01 (U+=Log(y+)/kappa +CSTLOG ) APOW = 0.83000E+01 (U+=APOW (y+)**BPOW (W&W law)) BPOW = 0.14286E+00 (U+=APOW (y+)**BPOW (W&W law)) - k-epsilon (ITURB = 20) Ce1 = 0.14400E+01 (Cepsilon 1: production coef.) CE2 = 0.19200E+01 (Cepsilon 2: dissipat. coef.) SIGMAK = 0.10000E+01 (Prandtl relative to k ) SIGMAE = 0.13000E+01 (Prandtl relative to epsilon ) CMU = 0.90000E-01 (Cmu constant ) ----------------------------------------------------------- ** SECONDARY VISCOSITY ------------------- --- Continuous phase: IVISSE = 1 (1: accounted for ) ----------------------------------------------------------- ** TIME STEPPING ------------- UNSTEADY ALGORITHM --- Time step parameters IDTVAR = 2 (0 cst; 1,2 var (t, t-space ) IPTLRO = 0 (1: rho-related DT clipping ) COUMAX = 0.10000E+01 (Maximum target CFL ) FOUMAX = 0.10000E+02 (Maximum target Fourier ) VARRDT = 0.10000E+00 (For var. DT, max. increase ) DTMIN = 0.10000E-03 (Minimum time step ) DTMAX = 0.10000E+01 (Maximum time step ) DTREF = 0.10000E-02 (Reference time step ) With a non-constant time step (IDTVAR = 1 or 2), when the value of COUMAX or FOUMAX is negative or zero, the associated time step limitation (for CFL and Fourier respectively) is ignored. --- Frozen velocity field ICCVFG = 0 (1: frozen velocity field ) --- Per-variable properties ------------------------------------ Variable ISTAT CDTVAR ------------------------------------ Pressure 0 0.1000E+01 VelocityX 1 0.1000E+01 VelocityY 1 0.1000E+01 VelocityZ 1 0.1000E+01 TurbEner 1 0.1000E+01 Dissip 1 0.1000E+01 TempK 1 0.1000E+01 ---------------------------- ISTAT = 0 ou 1 (1 for unsteady ) CDTVAR > 0 (time step multiplier ) --- Order of base time stepping scheme ISCHTP = 1 (1: order 1; 2: order 2 ) ----------------------------------------------------------- ** CONVECTION - DIFFUSION ---------------------- --------------------------------------------------------------------- Variable ICONV IDIFF IDIFFT ISCHCV ISSTPC BLENCV THETAV --------------------------------------------------------------------- Pressure 0 1 1 1 0 0.00E+00 0.10E+01 VelocityX 1 1 1 0 0 0.10E+01 0.10E+01 VelocityY 1 1 1 0 0 0.10E+01 0.10E+01 VelocityZ 1 1 1 0 0 0.10E+01 0.10E+01 TurbEner 1 1 1 1 0 0.00E+00 0.10E+01 Dissip 1 1 1 1 0 0.00E+00 0.10E+01 TempK 1 1 1 0 0 0.10E+01 0.10E+01 ------------------------------------------------------------- ICONV = 0 ou 1 (1 for convection active ) IDIFF = 0 ou 1 (1 for total diffusion active) IDIFFT = 0 ou 1 (1 for turbulent diff. active) ISCHCV = 0 ou 1 (SOLU or CD ) ISSTPC = 0 ou 1 (1: no slope test ) BLENCV = [0.;1.] (1-upwind proportion ) THETAV = [0.;1.] (0.5 Crank-Nicolson/AB ) (theta for convection- ) (diffusion terms uses ) ((1-theta).old+theta.new ) ----------------------------------------------------------- ** STOKES ------ IVELCO = 1 (0: segregated solving of the velocity components during the prediction step 1: coupled solving of the velocity components ) IPHYDR = 0 (1: account for explicit balance between pressure gradient, gravity source terms, and head losses ) ICALHY = 0 (1: compute hydrastatic pressure for Dirichlet conditions for pressure on outlet ) IPRCO = 1 (1: pressure-continuity ) IPUCOU = 0 (1: reinfo No error detected during the data verification cs_user_parameters.f90 and others). =========================================================== CALCULATION PARAMETERS SUMMARY ============================== ----------------------------------------------------------- ** DIMENSIONS ---------- --- Geometry NPRFML = 1 (Nb max. family properties ) NFML = 10 (Nb families ) --- Physics NVAR = 7 (Nb variables ) NSCAL = 1 (Nb scalars ) NSCAUS = 1 (Nb user scalars ) NSCAPP = 0 (Nb specific physics scalars ) NPROCE = 8 (Nb cell properties ) NPROFA = 1 (Nb internal face properties ) NPROFB = 2 (Nb boundary face properties ) ----------------------------------------------------------- ** PHYSICAL PROPERTIES ------------------- GX = 0.00000E+00 (Gravity x component ) GY = -0.98100E+01 (Gravity y component ) GZ = 0.00000E+00 (Gravity z component ) OMEGAX = 0.00000E+00 (Rotation vector x component ) OMEGAY = 0.00000E+00 (Rotation vector y component ) OMEGAZ = 0.00000E+00 (Rotation vector z component ) ICORIO = 0 (Coriolis source terms ) -- Continuous phase: RO0 = 0.99829E+03 (Reference density ) VISCL0 = 0.10050E-02 (Ref. molecular dyn. visc. ) CP0 = 0.41800E+04 (Ref. specific heat ) ICP = 7 (> 0: variable CP (usphyv) ) P0 = 0.10132E+06 (Ref. total pressure ) PRED0 = 0.00000E+00 (Ref. reduced pressure ) T0 = 0.29315E+03 (Ref. temperature ) IROVAR = 1 (Density constant(0) or not(1) IVIVAR = 1 (Molec. visc cst.(0) or not(1) Initial reference point for pressure XYZP0 = 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------- ** TURBULENCE ---------- --- Continuous phase: - Commons ITURB = 20 (Turbulence model ) IDEUCH = 2 (0: one-scale model ) (1: two-scale model ) (2: invariant wall function ) IWALLT = 0 (Exch. coeff. correlation ) (0: not activated ) (1: activated ) YPLULI = 0.10880E+02 (Limit Y+ ) ILOGPO = 1 (0: power law (forbidden for k-epsilon) ) (1: one-scale log law ) IGRHOK = 0 (1: computed Grad(rho k) ) ISCALT = 1 (Temperature salar number ) - k-epsilon (ITURB = 20) ALMAX = -0.99900E+03 (Characteristic length ) UREF = 0.53000E+01 (Characteristic velocity ) ICLKEP = 0 (k-epsilon clipping model ) IKECOU = 1 (k-epsilon coupling mode ) IGRAKE = 0 (Account for gravity ) - Rotation/curvature correction IRCCOR = 0 (0: desactivated ) (1: activated ) --- Constants - Commons XKAPPA = 0.42000E+00 (Von Karman constant ) CSTLOG = 0.52000E+01 (U+=Log(y+)/kappa +CSTLOG ) APOW = 0.83000E+01 (U+=APOW (y+)**BPOW (W&W law)) BPOW = 0.14286E+00 (U+=APOW (y+)**BPOW (W&W law)) - k-epsilon (ITURB = 20) Ce1 = 0.14400E+01 (Cepsilon 1: production coef.) CE2 = 0.19200E+01 (Cepsilon 2: dissipat. coef.) SIGMAK = 0.10000E No error detected during the data verification cs_user_parameters.f90 and others). =========================================================== CALCULATION PARAMETERS SUMMARY ============================== ----------------------------------------------------------- ** DIMENSIONS ---------- --- Geometry NPRFML = 1 (Nb max. family properties ) NFML = 10 (Nb families ) --- Physics NVAR = 7 (Nb variables ) NSCAL = 1 (Nb scalars ) NSCAUS = 1 (Nb user scalars ) NSCAPP = 0 (Nb specific physics scalars ) NPROCE = 8 (Nb cell properties ) NPROFA = 1 (Nb internal face properties ) NPROFB = 2 (Nb boundary face properties ) ----------------------------------------------------------- ** PHYSICAL PROPERTIES ------------------- GX = 0.00000E+00 (Gravity x component ) GY = -0.98100E+01 (Gravity y component ) GZ = 0.00000E+00 (Gravity z component ) OMEGAX = 0.00000E+00 (Rotation vector x component ) OMEGAY = 0.00000E+00 (Rotation vector y component ) OMEGAZ = 0.00000E+00 (Rotation vector z component ) ICORIO = 0 (Coriolis source terms ) -- Continuous phase: RO0 = 0.99829E+03 (Reference density ) VISCL0 = 0.10050E-02 (Ref. molecular dyn. visc. ) CP0 = 0.41800E+04 (Ref. specific heat ) ICP = 7 (> 0: variable CP (usphyv) ) P0 = 0.10132E+06 (Ref. total pressure ) PRED0 = 0.00000E+00 (Ref. reduced pressure ) T0 = 0.29315E+03 (Ref. temperature ) IROVAR = 1 (Density constant(0) or not(1) IVIVAR = 1 (Molec. visc cst.(0) or not(1) Initial reference point for pressure XYZP0 = 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------- ** TURBULENCE ---------- --- Continuous phase: - Commons ITURB = 20 (Turbulence model ) IDEUCH = 2 (0: one-scale model ) (1: two-scale model ) (2: invariant wall function ) IWALLT = 0 (Exch. coeff. correlation ) (0: not activated ) (1: activated ) YPLULI = 0.10880E+02 (Limit Y+ ) ILOGPO = 1 (0: power law (forbidden for k-epsilon) ) (1: one-scale log law ) IGRHOK = 0 (1: computed Grad(rho k) ) ISCALT = 1 (Temperature salar number ) - k-epsilon (ITURB = 20) ALMAX = -0.99900E+03 (Characteristic length ) UREF = 0.53000E+01 (Characteristic velocity ) ICLKEP = 0 (k-epsilon clipping model ) IKECOU = 1 (k-epsilon coupling mode ) IGRAKE = 0 (Account for gravity ) - Rotation/curvature correction IRCCOR = 0 (0: desactivated ) (1: activated ) --- Constants - Commons XKAPPA = 0.42000E+00 (Von Karman constant ) CSTLOG = 0.52000E+01 (U+=Log(y+)/kappa +CSTLOG ) APOW = 0.83000E+01 (U+=APOW (y+)**BPOW (W&W law)) BPOW = 0.14286E+00 (U+=APOW (y+)**BPOW (W&W law)) - k-epsilon (ITURB = 20) Ce1 = 0.14400E+01 (Cepsilon 1: production coef.) CE2 = 0.19200E+01 (Cepsilon 2: dissipat. coef.) SIGMAK = 0.10000E No error detected during the data verification cs_user_parameters.f90 and others). =========================================================== CALCULATION PARAMETERS SUMMARY ============================== ----------------------------------------------------------- ** DIMENSIONS ---------- --- Geometry NPRFML = 1 (Nb max. family properties ) NFML = 10 (Nb families ) --- Physics NVAR = 7 (Nb variables ) NSCAL = 1 (Nb scalars ) NSCAUS = 1 (Nb user scalars ) NSCAPP = 0 (Nb specific physics scalars ) NPROCE = 8 (Nb cell properties ) NPROFA = 1 (Nb internal face properties ) NPROFB = 2 (Nb boundary face properties ) ----------------------------------------------------------- ** PHYSICAL PROPERTIES ------------------- GX = 0.00000E+00 (Gravity x component ) GY = -0.98100E+01 (Gravity y component ) GZ = 0.00000E+00 (Gravity z component ) OMEGAX = 0.00000E+00 (Rotation vector x component ) OMEGAY = 0.00000E+00 (Rotation vector y component ) OMEGAZ = 0.00000E+00 (Rotation vector z component ) ICORIO = 0 (Coriolis source terms ) -- Continuous phase: RO0 = 0.99829E+03 (Reference density ) VISCL0 = 0.10050E-02 (Ref. molecular dyn. visc. ) CP0 = 0.41800E+04 (Ref. specific heat ) ICP = 7 (> 0: variable CP (usphyv) ) P0 = 0.10132E+06 (Ref. total pressure ) PRED0 = 0.00000E+00 (Ref. reduced pressure ) T0 = 0.29315E+03 (Ref. temperature ) IROVAR = 1 (Density constant(0) or not(1) IVIVAR = 1 (Molec. visc cst.(0) or not(1) Initial reference point for pressure XYZP0 = 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------- ** TURBULENCE ---------- --- Continuous phase: - Commons ITURB = 20 (Turbulence model ) IDEUCH = 2 (0: one-scale model ) (1: two-scale model ) (2: invariant wall function ) IWALLT = 0 (Exch. coeff. correlation ) (0: not activated ) (1: activated ) YPLULI = 0.10880E+02 (Limit Y+ ) ILOGPO = 1 (0: power law (forbidden for k-epsilon) ) (1: one-scale log law ) IGRHOK = 0 (1: computed Grad(rho k) ) ISCALT = 1 (Temperature salar number ) - k-epsilon (ITURB = 20) ALMAX = -0.99900E+03 (Characteristic length ) UREF = 0.53000E+01 (Characteristic velocity ) ICLKEP = 0 (k-epsilon clipping model ) IKECOU = 1 (k-epsilon coupling mode ) IGRAKE = 0 (Account for gravity ) - Rotation/curvature correction IRCCOR = 0 (0: desactivated ) (1: activated ) --- Constants - Commons XKAPPA = 0.42000E+00 (Von Karman constant ) CSTLOG = 0.52000E+01 (U+=Log(y+)/kappa +CSTLOG ) APOW = 0.83000E+01 (U+=APOW (y+)**BPOW (W&W law)) BPOW = 0.14286E+00 (U+=APOW (y+)**BPOW (W&W law)) - k-epsilon (ITURB = 20) Ce1 = 0.14400E+01 (Cepsilon 1: production coef.) CE2 = 0.19200E+01 (Cepsilon 2: dissipat. coef.) SIGMAK = 0.10000E ** TIME STEPPING ------------- UNSTEADY ALGORITHM --- Time step parameters IDTVAR = 2 (0 cst; 1,2 var (t, t-space ) IPTLRO = 0 (1: rho-related DT clipping ) COUMAX = 0.10000E+01 (Maximum target CFL ) FOUMAX = 0.10000E+02 (Maximum target Fourier ) VARRDT = 0.10000E+00 (For var. DT, max. increase ) DTMIN = 0.10000E-03 (Minimum time step ) DTMAX = 0.10000E+01 (Maximum time step ) DTREF = 0.10000E-02 (Reference time step ) With a non-constant time step (IDTVAR = 1 or 2), when the value of COUMAX or FOUMAX is negative or zero, the associated time step limitation (for CFL and Fourier respectively) is ignored. --- Frozen velocity field ICCVFG = 0 (1: frozen velocity field ) --- Per-variable properties ------------------------------------ Variable ISTAT CDTVAR ------------------------------------ Pressure 0 0.1000E+01 VelocityX 1 0.1000E+01 VelocityY 1 0.1000E+01 VelocityZ 1 0.1000E+01 TurbEner 1 0.1000E+01 Dissip 1 0.1000E+01 TempK 1 0.1000E+01 ---------------------------- ISTAT = 0 ou 1 (1 for unsteady ) CDTVAR > 0 (time step multiplier ) --- Order of base time stepping scheme ISCHTP = 1 (1: order 1; 2: order 2 ) ----------------------------------------------------------- ** CONVECTION - DIFFUSION ---------------------- --------------------------------------------------------------------- Variable ICONV IDIFF IDIFFT ISCHCV ISSTPC BLENCV THETAV --------------------------------------------------------------------- Pressure 0 1 1 1 0 0.00E+00 0.10E+01 VelocityX 1 1 1 0 0 0.10E+01 0.10E+01 VelocityY 1 1 1 0 0 0.10E+01 0.10E+01 VelocityZ 1 1 1 0 0 0.10E+01 0.10E+01 TurbEner 1 1 1 1 0 0.00E+00 0.10E+01 Dissip 1 1 1 1 0 0.00E+00 0.10E+01 TempK 1 1 1 0 0 0.10E+01 0.10E+01 ------------------------------------------------------------- ICONV = 0 ou 1 (1 for convection active ) IDIFF = 0 ou 1 (1 for total diffusion active) IDIFFT = 0 ou 1 (1 for turbulent diff. active) ISCHCV = 0 ou 1 (SOLU or CD ) ISSTPC = 0 ou 1 (1: no slope test ) BLENCV = [0.;1.] (1-upwind proportion ) THETAV = [0.;1.] (0.5 Crank-Nicolson/AB ) (theta for convection- ) (diffusion terms uses ) ((1-theta).old+theta.new ) ----------------------------------------------------------- ** STOKES ------ IVELCO = 1 (0: segregated solving of the velocity components during the prediction step 1: coupled solving of the velocity components ) IPHYDR = 0 (1: account for explicit balance between pressure gradient, gravity source terms, and head losses ) ICALHY = 0 (1: compute hydrastatic pressure for Dirichlet conditions for pressure on outlet ) IPRCO = 1 (1: pressure-continuity ) IPUCOU = 0 (1: reinfo No error detected during the data verification cs_user_parameters.f90 and others). =========================================================== CALCULATION PARAMETERS SUMMARY ============================== ----------------------------------------------------------- ** DIMENSIONS ---------- --- Geometry NPRFML = 1 (Nb max. family properties ) NFML = 10 (Nb families ) --- Physics NVAR = 7 (Nb variables ) NSCAL = 1 (Nb scalars ) NSCAUS = 1 (Nb user scalars ) NSCAPP = 0 (Nb specific physics scalars ) NPROCE = 8 (Nb cell properties ) NPROFA = 1 (Nb internal face properties ) NPROFB = 2 (Nb boundary face properties ) ----------------------------------------------------------- ** PHYSICAL PROPERTIES ------------------- GX = 0.00000E+00 (Gravity x component ) GY = -0.98100E+01 (Gravity y component ) GZ = 0.00000E+00 (Gravity z component ) OMEGAX = 0.00000E+00 (Rotation vector x component ) OMEGAY = 0.00000E+00 (Rotation vector y component ) OMEGAZ = 0.00000E+00 (Rotation vector z component ) ICORIO = 0 (Coriolis source terms ) -- Continuous phase: RO0 = 0.99829E+03 (Reference density ) VISCL0 = 0.10050E-02 (Ref. molecular dyn. visc. ) CP0 = 0.41800E+04 (Ref. specific heat ) ICP = 7 (> 0: variable CP (usphyv) ) P0 = 0.10132E+06 (Ref. total pressure ) PRED0 = 0.00000E+00 (Ref. reduced pressure ) T0 = 0.29315E+03 (Ref. temperature ) IROVAR = 1 (Density constant(0) or not(1) IVIVAR = 1 (Molec. visc cst.(0) or not(1) Initial reference point for pressure XYZP0 = 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------- ** TURBULENCE ---------- --- Continuous phase: - Commons ITURB = 20 (Turbulence model ) IDEUCH = 2 (0: one-scale model ) (1: two-scale model ) (2: invariant wall function ) IWALLT = 0 (Exch. coeff. correlation ) (0: not activated ) (1: activated ) YPLULI = 0.10880E+02 (Limit Y+ ) ILOGPO = 1 (0: power law (forbidden for k-epsilon) ) (1: one-scale log law ) IGRHOK = 0 (1: computed Grad(rho k) ) ISCALT = 1 (Temperature salar number ) - k-epsilon (ITURB = 20) ALMAX = -0.99900E+03 (Characteristic length ) UREF = 0.53000E+01 (Characteristic velocity ) ICLKEP = 0 (k-epsilon clipping model ) IKECOU = 1 (k-epsilon coupling mode ) IGRAKE = 0 (Account for gravity ) - Rotation/curvature correction IRCCOR = 0 (0: desactivated ) (1: activated ) --- Constants - Commons XKAPPA = 0.42000E+00 (Von Karman constant ) CSTLOG = 0.52000E+01 (U+=Log(y+)/kappa +CSTLOG ) APOW = 0.83000E+01 (U+=APOW (y+)**BPOW (W&W law)) BPOW = 0.14286E+00 (U+=APOW (y+)**BPOW (W&W law)) - k-epsilon (ITURB = 20) Ce1 = 0.14400E+01 (Cepsilon 1: production coef.) CE2 = 0.19200E+01 (Cepsilon 2: dissipat. coef.) SIGMAK = 0.10000Erced U-P coupling ) NTERUP = 1 (n: n sweeps on navsto for velocity/pressure coupling ) -- Continuous phase: IREVMC = 0 (Velocity reconstruction mode) RELAXV = 0.10000E+01 for pressure (relaxation) ARAK = 0.10000E+01 (Arakawa factor ) ISTMPF = 1 (time scheme for flow (0: explicit (THETFL = 0 ) (1: std scheme (Saturne 1.0 ) (2: 2nd-order (THETFL = 0.5 ) THETFL = -0.99900E+03 (theta for mass flow ) IROEXT = 0 (density extrapolation (0: explicit (1: n+thetro with thetro=1/2 (2: n+thetro with thetro=1 THETRO = 0.00000E+00 (theta for density ((1+theta).new-theta.old IVIEXT = 0 (total viscosity extrapolation (0: explicit (1: n+thetvi with thetro=1/2 (2: n+thetvi with thetro=1 THETVI = 0.00000E+00 (theta for total viscosity ((1+theta).new-theta.old ICPEXT = 0 (specific heat extrapolation (0: explicit (1: n+thetcp with thetro=1/2 (2: n+thetcp with thetro=1 THETCP = 0.00000E+00 (specific heat theta-scheme ((1+theta).new-theta.old THETSN = 0.00000E+00 (Nav-Stokes S.T. theta scheme) ((1+theta).new-theta.old THETST = 0.00000E+00 (Turbulence S.T. theta-scheme) ((1+theta).new-theta.old EPSUP = 0.10000E-04 (Velocity/pressure coupling stop test ) ----------------------------------------------------------- ** GRADIENTS CALCULATION --------------------- IMRGRA = 0 (Reconstruction mode ) ANOMAX = 0.78540E+00 (Non-ortho angle: limit for ) (least squares ext. neighbors) ------------------------------------------------------------------- Variable NSWRGR NSWRSM EPSRGR EPSRSM EXTRAG ------------------------------------------------------------------- Pressure 100 2 0.1000E-04 0.1000E-06 0.0000E+00 VelocityX 100 10 0.1000E-04 0.1000E-06 0.0000E+00 VelocityY 100 10 0.1000E-04 0.1000E-06 0.0000E+00 VelocityZ 100 10 0.1000E-04 0.1000E-06 0.0000E+00 TurbEner 100 1 0.1000E-04 0.1000E-06 0.0000E+00 Dissip 100 1 0.1000E-04 0.1000E-06 0.0000E+00 TempK 100 1 0.1000E-04 0.1000E-06 0.0000E+00 ----------------------------------------------------------- ------------------------------------------- Variable IRCFLU IMLIGR CLIMGR ------------------------------------------- Pressure 1 -1 0.1500E+01 VelocityX 1 -1 0.1500E+01 VelocityY 1 -1 0.1500E+01 VelocityZ 1 -1 0.1500E+01 TurbEner 1 -1 0.1500E+01 Dissip 1 -1 0.1500E+01 TempK 1 -1 0.1500E+01 ----------------------------------- NSWRGR = (nb sweep gradient reconstr. ) NSWRSM = (nb sweep rhs reconstrcution ) EPSRGR = (grad. reconstruction prec. ) EPSRSM = (rhs reconstruction prec. ) EXTRAG = [0.;1.] (gradients extrapolation ) IRCFLU = 0 ou 1 (flow reconstruction ) IMLIGR = < 0, 0 ou 1 (gradient limitation method ) CLIMGR = > 1 ou 1 (gradient limitation coeff. ) ----------------------------------------------------------- **+01 (Prandtl relative to k ) SIGMAE = 0.13000E+01 (Prandtl relative to epsilon ) CMU = 0.90000E-01 (Cmu constant ) ----------------------------------------------------------- ** SECONDARY VISCOSITY ------------------- --- Continuous phase: IVISSE = 1 (1: accounted for ) ----------------------------------------------------------- ** TIME STEPPING ------------- UNSTEADY ALGORITHM --- Time step parameters IDTVAR = 2 (0 cst; 1,2 var (t, t-space ) IPTLRO = 0 (1: rho-related DT clipping ) COUMAX = 0.10000E+01 (Maximum target CFL ) FOUMAX = 0.10000E+02 (Maximum target Fourier ) VARRDT = 0.10000E+00 (For var. DT, max. increase ) DTMIN = 0.10000E-03 (Minimum time step ) DTMAX = 0.10000E+01 (Maximum time step ) DTREF = 0.10000E-02 (Reference time step ) With a non-constant time step (IDTVAR = 1 or 2), when the value of COUMAX or FOUMAX is negative or zero, the associated time step limitation (for CFL and Fourier respectively) is ignored. --- Frozen velocity field ICCVFG = 0 (1: frozen velocity field ) --- Per-variable properties ------------------------------------ Variable ISTAT CDTVAR ------------------------------------ Pressure 0 0.1000E+01 +01 (Prandtl relative to k ) SIGMAE = 0.13000E+01 (Prandtl relative to epsilon ) CMU = 0.90000E-01 (Cmu constant ) ----------------------------------------------------------- ** SECONDARY VISCOSITY ------------------- --- Continuous phase: IVISSE = 1 (1: accounted for ) ----------------------------------------------------------- ** TIME STEPPING ------------- UNSTEADY ALGORITHM --- Time step parameters IDTVAR = 2 (0 cst; 1,2 var (t, t-space ) IPTLRO = 0 (1: rho-related DT clipping ) COUMAX = 0.10000E+01 (Maximum target CFL ) FOUMAX = 0.10000E+02 (Maximum target Fourier ) VARRDT = 0.10000E+00 (For var. DT, max. increase ) DTMIN = 0.10000E-03 (Minimum time step ) DTMAX = 0.10000E+01 (Maximum time step ) DTREF = 0.10000E-02 (Reference time step ) With a non-constant time step (IDTVAR = 1 or 2), when the value of COUMAX or FOUMAX is negative or zero, the associated time step limitation (for CFL and Fourier respectively) is ignored. --- Frozen velocity field ICCVFG = 0 (1: frozen velocity field ) --- Per-variable properties ------------------------------------ Variable ISTAT CDTVAR ------------------------------------ Pressure 0 0.1000E+01 VelocityX 1 0.1000E+01 VelocityY 1 0.1000E+01 VelocityZ 1 0.1000E+01 TurbEner 1 0.1000E+01 Dissip 1 0.1000E+01 TempK 1 0.1000E+01 ---------------------------- ISTAT = 0 ou 1 (1 for unsteady ) CDTVAR > 0 (time step multiplier ) --- Order of base time stepping scheme ISCHTP = 1 (1: order 1; 2: order 2 ) ----------------------------------------------------------- ** CONVECTION - DIFFUSION ---------------------- --------------------------------------------------------------------- Variable ICONV IDIFF IDIFFT ISCHCV ISSTPC BLENCV THETAV --------------------------------------------------------------------- Pressure 0 1 1 1 0 0.00E+00 0.10E+01 VelocityX 1 1 1 0 0 0.10E+01 0.10E+01 VelocityY 1 1 1 0 0 0.10E+01 0.10E+01 VelocityZ 1 1 1 0 0 0.10E+01 0.10E+01 TurbEner 1 1 1 1 0 0.00E+00 0.10E+01 Dissip 1 1 1 1 0 0.00E+00 0.10E+01 TempK 1 1 1 0 0 0.10E+01 0.10E+01 ------------------------------------------------------------- ICONV = 0 ou 1 (1 for convection active ) IDIFF = 0 ou 1 (1 for total diffusion active) IDIFFT = 0 ou 1 (1 for turbulent diff. active) ISCHCV = 0 ou 1 (SOLU or CD ) ISSTPC = 0 ou 1 (1: no slope test ) BLENCV = [0.;1.] (1-upwind proportion ) THETAV = [0.;1.] (0.5 Crank-Nicolson/AB ) (theta for convection- ) (diffusion terms uses ) ((1-theta).old+theta.new ) ----------------------------------------------------------- ** STOKES ------ IVELCO = 1 (0: segregated solving of the velocity components during the prediction step 1: coupled solving of the velocity components ) IPHYDR = 0 (1: account for explicit balance between pressure gradient+01 (Prandtl relative to k ) SIGMAE = 0.13000E+01 (Prandtl relative to epsilon ) CMU = 0.90000E-01 (Cmu constant ) ----------------------------------------------------------- ** SECONDARY VISCOSITY ------------------- --- Continuous phase: IVISSE = 1 (1: accounted for ) ----------------------------------------------------------- ** TIME STEPPING ------------- UNSTEADY ALGORITHM --- Time step parameters IDTVAR = 2 (0 cst; 1,2 var (t, t-space ) IPTLRO = 0 (1: rho-related DT clipping ) COUMAX = 0.10000E+01 (Maximum target CFL ) FOUMAX = 0.10000E+02 (Maximum target Fourier ) VARRDT = 0.10000E+00 (For var. DT, max. increase ) DTMIN = 0.10000E-03 (Minimum time step ) DTMAX = 0.10000E+01 (Maximum time step ) DTREF = 0.10000E-02 (Reference time step ) With a non-constant time step (IDTVAR = 1 or 2), when the value of COUMAX or FOUMAX is negative or zero, the associated time step limitation (for CFL and Fourier respectively) is ignored. --- Frozen velocity field ICCVFG = 0 (1: frozen velocity field ) --- Per-variable properties ------------------------------------ Variable ISTAT CDTVAR ------------------------------------ Pressure 0 0.1000E+01 VelocityX 1 0.1000E+01 VelocityY 1 0.1000E+01 VelocityZ 1 0.1000E+01 TurbEner 1 0.1000E+01 Dissip 1 0.1000E+01 TempK 1 0.1000E+01 ---------------------------- ISTAT = 0 ou 1 (1 for unsteady ) CDTVAR > 0 (time step multiplier ) --- Order of base time stepping scheme ISCHTP = 1 (1: order 1; 2: order 2 ) ----------------------------------------------------------- ** CONVECTION - DIFFUSION ---------------------- --------------------------------------------------------------------- Variable ICONV IDIFF IDIFFT ISCHCV ISSTPC BLENCV THETAV --------------------------------------------------------------------- Pressure 0 1 1 1 0 0.00E+00 0.10E+01 VelocityX 1 1 1 0 0 0.10E+01 0.10E+01 VelocityY 1 1 1 0 0 0.10E+01 0.10E+01 VelocityZ 1 1 1 0 0 0.10E+01 0.10E+01 TurbEner 1 1 1 1 0 0.00E+00 0.10E+01 Dissip 1 1 1 1 0 0.00E+00 0.10E+01 TempK 1 1 1 0 0 0.10E+01 0.10E+01 ------------------------------------------------------------- ICONV = 0 ou 1 (1 for convection active ) IDIFF = 0 ou 1 (1 for total diffusion active) IDIFFT = 0 ou 1 (1 for turbulent diff. active) ISCHCV = 0 ou 1 (SOLU or CD ) ISSTPC = 0 ou 1 (1: no slope test ) BLENCV = [0.;1.] (1-upwind proportion ) THETAV = [0.;1.] (0.5 Crank-Nicolson/AB ) (theta for convection- ) (diffusion terms uses ) ((1-theta).old+theta.new ) ----------------------------------------------------------- ** STOKES ------ IVELCO = 1 (0: segregated solving of the velocity components during the prediction step 1: coupled solving of the velocity components ) IPHYDR = 0 (1: account for explicit balance between pressure gradientrced U-P coupling ) NTERUP = 1 (n: n sweeps on navsto for velocity/pressure coupling ) -- Continuous phase: IREVMC = 0 (Velocity reconstruction mode) RELAXV = 0.10000E+01 for pressure (relaxation) ARAK = 0.10000E+01 (Arakawa factor ) ISTMPF = 1 (time scheme for flow (0: explicit (THETFL = 0 ) (1: std scheme (Saturne 1.0 ) (2: 2nd-order (THETFL = 0.5 ) THETFL = -0.99900E+03 (theta for mass flow ) IROEXT = 0 (density extrapolation (0: explicit (1: n+thetro with thetro=1/2 (2: n+thetro with thetro=1 THETRO = 0.00000E+00 (theta for density ((1+theta).new-theta.old IVIEXT = 0 (total viscosity extrapolation (0: explicit (1: n+thetvi with thetro=1/2 (2: n+thetvi with thetro=1 THETVI = 0.00000E+00 (theta for total viscosity ((1+theta).new-theta.old ICPEXT = 0 (specific heat extrapolation (0: explicit (1: n+thetcp with thetro=1/2 (2: n+thetcp with thetro=1 THETCP = 0.00000E+00 (specific heat theta-scheme ((1+theta).new-theta.old THETSN = 0.00000E+00 (Nav-Stokes S.T. theta scheme) ((1+theta).new-theta.old THETST = 0.00000E+00 (Turbulence S.T. theta-scheme) ((1+theta).new-theta.old EPSUP = 0.10000E-04 (Velocity/pressure coupling stop test ) ----------------------------------------------------------- ** GRADIENTS CALCULATION --------------------- IMRGRA = 0 (Reconstruction mode ) ANOMAX = 0.78540E+00 (Non-ortho angle: limit for ) (least squares ext. neighbors) ------------------------------------------------------------------- Variable NSWRGR NSWRSM EPSRGR EPSRSM EXTRAG ------------------------------------------------------------------- Pressure 100 2 0.1000E-04 0.1000E-06 0.0000E+00 VelocityX 100 10 0.1000E-04 0.1000E-06 0.0000E+00 VelocityY 100 10 0.1000E-04 0.1000E-06 0.0000E+00 VelocityZ 100 10 0.1000E-04 0.1000E-06 0.0000E+00 TurbEner 100 1 0.1000E-04 0.1000E-06 0.0000E+00 Dissip 100 1 0.1000E-04 0.1000E-06 0.0000E+00 TempK 100 1 0.1000E-04 0.1000E-06 0.0000E+00 ----------------------------------------------------------- ------------------------------------------- Variable IRCFLU IMLIGR CLIMGR ------------------------------------------- Pressure 1 -1 0.1500E+01 VelocityX 1 -1 0.1500E+01 VelocityY 1 -1 0.1500E+01 VelocityZ 1 -1 0.1500E+01 TurbEner 1 -1 0.1500E+01 Dissip 1 -1 0.1500E+01 TempK 1 -1 0.1500E+01 ----------------------------------- NSWRGR = (nb sweep gradient reconstr. ) NSWRSM = (nb sweep rhs reconstrcution ) EPSRGR = (grad. reconstruction prec. ) EPSRSM = (rhs reconstruction prec. ) EXTRAG = [0.;1.] (gradients extrapolation ) IRCFLU = 0 ou 1 (flow reconstruction ) IMLIGR = < 0, 0 ou 1 (gradient limitation method ) CLIMGR = > 1 ou 1 (gradient limitation coeff. ) ----------------------------------------------------------- **+01 (Prandtl relative to k ) SIGMAE = 0.13000E+01 (Prandtl relative to epsilon ) CMU = 0.90000E-01 (Cmu constant ) ----------------------------------------------------------- ** SECONDARY VISCOSITY ------------------- --- Continuous phase: IVISSE = 1 (1: accounted for ) ----------------------------------------------------------- ** TIME STEPPING ------------- UNSTEADY ALGORITHM --- Time step parameters IDTVAR = 2 (0 cst; 1,2 var (t, t-space ) IPTLRO = 0 (1: rho-related DT clipping ) COUMAX = 0.10000E+01 (Maximum target CFL ) FOUMAX = 0.10000E+02 (Maximum target Fourier ) VARRDT = 0.10000E+00 (For var. DT, max. increase ) DTMIN = 0.10000E-03 (Minimum time step ) DTMAX = 0.10000E+01 (Maximum time step ) DTREF = 0.10000E-02 (Reference time step ) With a non-constant time step (IDTVAR = 1 or 2), when the value of COUMAX or FOUMAX is negative or zero, the associated time step limitation (for CFL and Fourier respectively) is ignored. --- Frozen velocity field ICCVFG = 0 (1: frozen velocity field ) --- Per-variable properties ------------------------------------ Variable ISTAT CDTVAR ------------------------------------ Pressure 0 0.1000E+01 VelocityX 1 0.1000E+01 VelocityY 1 0.1000E+01 VelocityZ 1 0.1000E+01 TurbEner 1 0.1000E+01 Dissip 1 0.1000E+01 TempK 1 0.1000E+01 ---------------------------- ISTAT = 0 ou 1 (1 for unsteady ) CDTVAR > 0 (time step multiplier ) --- Order of base time stepping scheme ISCHTP = 1 (1: order 1; 2: order 2 ) ----------------------------------------------------------- ** CONVECTION - DIFFUSION , gravity source terms, and head losses ) ICALHY = 0 (1: compute hydrastatic pressure for Dirichlet conditions for pressure on outlet ) IPRCO = 1 (1: pressure-continuity ) IPUCOU = 0 (1: reinforced U-P coupling ) NTERUP = 1 (n: n sweeps on navsto for velocity/pressure coupling ) -- Continuous phase: IREVMC = 0 (Velocity reconstruction mode) RELAXV = 0.10000E+01 for pressure (relaxation) ARAK = 0.10000E+01 (Arakawa factor ) ISTMPF = 1 (time scheme for flow (0: explicit (THETFL = 0 ) (1: std scheme (Saturne 1.0 ) (2: 2nd-order (THETFL = 0.5 ) THETFL = -0.99900E+03 (theta for mass flow ) IROEXT = 0 (density extrapolation (0: explicit (1: n+thetro with thetro=1/2 (2: n+thetro with thetro=1 THETRO = 0.00000E+00 (theta for density ((1+theta).new-theta.old IVIEXT = 0 (total viscosity extrapolation (0: explicit (1: n+thetvi with thetro=1/2 (2: n+thetvi with thetro=1 THETVI = 0.00000E+00 (theta for total viscosity ((1+theta).new-theta.old ICPEXT = 0 (specific heat extrapolation (0: explicit (1: n+thetcp with thetro=1/2 (2: n+thetcp with thetro=1 THETCP = 0.00000E+00 (specific heat theta-scheme ((1+theta).new-theta.old THETSN = 0.00000E+00 (Nav-Stokes S.T. theta scheme) ((1+theta).new-theta.old THETST = 0.00000E+00 (Turbulence S.T. theta-scheme) ((1+theta).new-theta.old EPSUP = 0.10000E-04 (Velocity/pressure coupling stop test ) ----------------------------------------------------------- ** GRADIENTS CALCULATION --------------------- IMRGRA = 0 (Reconstruction mode ) ANOMAX = 0.78540E+00 (Non-ortho angle: limit for ) (least squares ext. neighbors) ------------------------------------------------------------------- Variable NSWRGR NSWRSM EPSRGR EPSRSM EXTRAG ------------------------------------------------------------------- Pressure 100 2 0.1000E-04 0.1000E-06 0.0000E+00 VelocityX 100 10 0.1000E-04 0.1000E-06 0.0000E+00 VelocityY 100 10 0.1000E-04 0.1000E-06 0.0000E+00 VelocityZ 100 10 0.1000E-04 0.1000E-06 0.0000E+00 TurbEner 100 1 0.1000E-04 0.1000E-06 0.0000E+00 Dissip 100 1 0.1000E-04 0.1000E-06 0.0000E+00 TempK 100 1 0.1000E-04 0.1000E-06 0.0000E+00 ----------------------------------------------------------- ------------------------------------------- Variable IRCFLU IMLIGR CLIMGR ------------------------------------------- Pressure 1 -1 0.1500E+01 VelocityX 1 -1 0.1500E+01 VelocityY 1 -1 0.1500E+01 VelocityZ 1 -1 0.1500E+01 , gravity source terms, and head losses ) ICALHY = 0 (1: compute hydrastatic pressure for Dirichlet conditions for pressure on outlet ) IPRCO = 1 (1: pressure-continuity ) IPUCOU = 0 (1: reinforced U-P coupling ) NTERUP = 1 (n: n sweeps on navsto for velocity/pressure coupling ) -- Continuous phase: IREVMC = 0 (Velocity reconstruction mode) RELAXV = 0.10000E+01 for pressure (relaxation) ARAK = 0.10000E+01 (Arakawa factor ) ISTMPF = 1 (time scheme for flow (0: explicit (THETFL = 0 ) (1: std scheme (Saturne 1.0 ) (2: 2nd-order (THETFL = 0.5 ) THETFL = -0.99900E+03 (theta for mass flow ) IROEXT = 0 (density extrapolation (0: explicit (1: n+thetro with thetro=1/2 (2: n+thetro with thetro=1 THETRO = 0.00000E+00 (theta for density ((1+theta).new-theta.old IVIEXT = 0 (total viscosity extrapolation (0: explicit (1: n+thetvi with thetro=1/2 (2: n+thetvi with thetro=1 THETVI = 0.00000E+00 (theta for total viscosity ((1+theta).new-theta.old ICPEXT = 0 (specific heat extrapolation (0: explicit (1: n+thetcp with thetro=1/2 (2: n+thetcp with thetro=1 THETCP = 0.00000E+00 (specific heat theta-scheme ((1+theta).new-theta.old THETSN = 0.00000E+00 (Nav-Stokes S.T. theta scheme) ((1+theta).new-theta.old THETST = 0.00000E+00 (Turbulence S.T. theta-scheme) ((1+theta).new-theta.old EPSUP = 0.10000E-04 (Velocity/pressure coupling stop test ) ----------------------------------------------------------- ** GRADIENTS CALCULATION --------------------- IMRGRA = 0 (Reconstruction mode ) ANOMAX = 0.78540E+00 (Non-ortho angle: limit for ) (least squares ext. neighbors) ------------------------------------------------------------------- Variable NSWRGR NSWRSM EPSRGR EPSRSM EXTRAG ------------------------------------------------------------------- Pressure 100 2 0.1000E-04 0.1000E-06 0.0000E+00 VelocityX 100 10 0.1000E-04 0.1000E-06 0.0000E+00 VelocityY 100 10 0.1000E-04 0.1000E-06 0.0000E+00 VelocityZ 100 10 0.1000E-04 0.1000E-06 0.0000E+00 TurbEner 100 1 0.1000E-04 0.1000E-06 0.0000E+00 Dissip 100 1 0.1000E-04 0.1000E-06 0.0000E+00 TempK 100 1 0.1000E-04 0.1000E-06 0.0000E+00 ----------------------------------------------------------- ------------------------------------------- Variable IRCFLU IMLIGR CLIMGR ------------------------------------------- Pressure 1 -1 0.1500E+01 VelocityX 1 -1 0.1500E+01 VelocityY 1 -1 0.1500E+01 VelocityZ 1 -1 0.1500E+01 TurbEner 1 -1 0.1500E+01 Dissip 1 -1 0.1500E+01 TempK 1 -1 0.1500E+01 ----------------------------------- NSWRGR = (nb sweep gradient reconstr. ) NSWRSM = (nb sweep rhs reconstrcution ) EPSRGR = ---------------------- --------------------------------------------------------------------- Variable ICONV IDIFF IDIFFT ISCHCV ISSTPC BLENCV THETAV --------------------------------------------------------------------- Pressure 0 1 1 1 0 0.00E+00 0.10E+01 VelocityX 1 1 1 0 0 0.10E+01 0.10E+01 VelocityY 1 1 1 0 0 0.10E+01 0.10E+01 VelocityZ 1 1 1 0 0 0.10E+01 0.10E+01 TurbEner 1 1 1 1 0 0.00E+00 0.10E+01 Dissip 1 1 1 1 0 0.00E+00 0.10E+01 TempK 1 1 1 0 0 0.10E+01 0.10E+01 ------------------------------------------------------------- ICONV = 0 ou 1 (1 for convection active ) FACE INTERPOLATION ------------------ IMVISF = 0 (0 arithmetic ) ----------------------------------------------------------- ** CALCULATION OF TEMPORAL MEANS (MOMENTS) --------------------------------------- NBMOMT = 0 (Number of moments ) ----------------------------------------------------------- ** BASE ITERATIVE SOLVERS ---------------------- -------------------------------------------------- Variable IRESOL NITMAX EPSILO IDIRCL -------------------------------------------------- Pressure 0 10000 0.1000E-07 1 VelocityX -1 10000 0.1000E-07 1 VelocityY -1 10000 0.1000E-07 1 VelocityZ -1 10000 0.1000E-07 1 TurbEner -1 10000 0.1000E-07 1 Dissip -1 10000 0.1000E-07 1 TempK -1 10000 0.1000E-07 1 ----------------------------------- IRESOL = -1 (automatic solver choice ) IPOL*1000 + 0 (p conjuguate gradient ) 1 (Jacobi ) IPOL*1000 + 2 (bicgstab ) avec IPOL (preconditioning degree ) NITMAX = (max number of iterations ) EPSILO = (resolution precision ) IDIRCL = 0 ou 1 (shift diagonal if ISTAT=0 and no Dirichlet ) ----------------------------------------------------------- ** MULTIGRID --------- NCEGRM = 30 (Max nb cells coarsest grid ) NGRMAX = 25 (Max number of levels ) -------------------------------------- Variable IMGR NCYMAX NITMGF -------------------------------------- Pressure 1 100 10 VelocityX 0 100 10 VelocityY 0 100 10 VelocityZ 0 100 10 TurbEner 0 100 10 Dissip 0 100 10 TempK 0 100 10 ------------------------------ IMGR = 0 ou 1 (1: multigrid activated ) NCYMAX = (Max number of cycles ) NITMGF = (Max nb iter on coarsest grid) FACE INTERPOLATION ------------------ IMVISF = 0 (0 arithmetic ) ----------------------------------------------------------- ** CALCULATION OF TEMPORAL MEANS (MOMENTS) --------------------------------------- NBMOMT = 0 (Number of moments ) ----------------------------------------------------------- ** BASE ITERATIVE SOLVERS ---------------------- -------------------------------------------------- Variable IRESOL NITMAX EPSILO IDIRCL -------------------------------------------------- Pressure 0 10000 0.1000E-07 1 VelocityX -1 10000 0.1000E-07 1 VelocityY -1 10000 0.1000E-07 1 VelocityZ -1 10000 0.1000E-07 1 TurbEner -1 10000 0.1000E-07 1 Dissip -1 10000 0.1000E-07 1 TempK -1 10000 0.1000E-07 1 ----------------------------------- IRESOL = -1 (automatic solver choice ) IPOL*1000 + 0 (p conjuguate gradient ) 1 (Jacobi ) IPOL*1000 + 2 (bicgstab ) avec IPOL (preconditioning degree ) NITMAX = (max number of iterations ) EPSILO = (resolution precision ) IDIRCL = 0 ou 1 (shift diagonal if ISTAT=0 and no Dirichlet ) ----------------------------------------------------------- ** MULTIGRID --------- NCEGRM = 30 (Max nb cells coarsest grid ) NGRMAX = 25 (Max number of levels ) -------------------------------------- Variable IMGR NCYMAX NITMGF -------------------------------------- Pressure 1 100 10 VelocityX 0 100 10 VelocityY 0 100 10 VelocityZ 0 100 10 TurbEner 0 100 10 Dissip 0 100 10 TempK 0 100 10 ------------------------------ IMGR = 0 ou 1 (1: multigrid activated ) NCYMAX = (Max number of cycles ) NITMGF = (Max nb iter on coarsest grid) VelocityX 1 0.1000E+01 VelocityY 1 0.1000E+01 VelocityZ 1 0.1000E+01 TurbEner 1 0.1000E+01 Dissip 1 0.1000E+01 TempK 1 0.1000E+01 ---------------------------- ISTAT = 0 ou 1 (1 for unsteady ) CDTVAR > 0 (time step multiplier ) --- Order of base time stepping scheme ISCHTP = 1 (1: order 1; 2: order 2 ) ----------------------------------------------------------- ** CONVECTION - DIFFUSION ---------------------- --------------------------------------------------------------------- Variable ICONV IDIFF IDIFFT ISCHCV ISSTPC BLENCV THETAV --------------------------------------------------------------------- Pressure 0 1 1 1 0 0.00E+00 0.10E+01 VelocityX 1 1 1 0 0 0.10E+01 0.10E+01 VelocityY 1 1 1 0 0 0.10E+01 0.10E+01 VelocityZ 1 1 1 0 0 0.10E+01 0.10E+01 TurbEner 1 1 1 1 0 0.00E+00 0.10E+01 Dissip 1 1 1 1 0 0.00E+00 0.10E+01 TempK 1 1 1 0 0 0.10E+01 0.10E+01 IDIFF = 0 ou 1 (1 for total diffusion active) IDIFFT = 0 ou 1 (1 for turbulent diff. active) ISCHCV = 0 ou 1 (SOLU or CD ) ISSTPC = 0 ou 1 (1: no slope test ) BLENCV = [0.;1.] (1-upwind proportion ) THETAV = [0.;1.] (0.5 Crank-Nicolson/AB ) (theta for convection- ) (diffusion terms uses ) ((1-theta).old+theta.new ) ----------------------------------------------------------- ** STOKES ------ IVELCO = 1 (0: segregated solving of the velocity components during the prediction step 1: coupled solving of the velocity components ) IPHYDR = 0 (1: account for explicit balance between pressure Multigrid rank merge parameters: mean coarse cells merge threshold: 300 total coarse cells merge threshold: 500 minimum ranks merge threshold: 1 merge stride: 1 Multigrid coarsening type: algebraic, face traveral by criteria ----------------------------------------------------------- ** SCALARS ------- ITBRRB = 0 (T or H reconstruction at bdy) --------------------------------------------------------------------- Variable Number ISCSTH IVISLS ITURT VISLS0 SIGMAS --------------------------------------------------------------------- TempK 1 1 12 0 0.6155E+00 0.1000E+01 --------------------------------------------------------------------- ------------------------------------------- Variable Number ISCAVR RVARFL ------------------------------------------- Multigrid rank merge parameters: mean coarse cells merge threshold: 300 total coarse cells merge threshold: 500 minimum ranks merge threshold: 1 merge stride: 1 Multigrid coarsening type: algebraic, face traveral by criteria ----------------------------------------------------------- ** SCALARS ------- ITBRRB = 0 (T or H reconstruction at bdy) --------------------------------------------------------------------- Variable Number ISCSTH IVISLS ITURT VISLS0 SIGMAS --------------------------------------------------------------------- TempK 1 1 12 0 0.6155E+00 0.1000E+01 --------------------------------------------------------------------- ------------------------------------------- Variable Number ISCAVR RVARFL ------------------------------------------- TempK 1 0 0.8000E+00 ------------------------------------------- (grad. reconstruction prec. ) EPSRSM = (rhs reconstruction prec. ) EXTRAG = [0.;1.] (gradients extrapolation ) IRCFLU = 0 ou 1 (flow reconstruction ) IMLIGR = < 0, 0 ou 1 (gradient limitation method ) CLIMGR = > 1 ou 1 (gradient limitation coeff. ) ----------------------------------------------------------- ** FACE INTERPOLATION ------------------ IMVISF = 0 (0 arithmetic ) ----------------------------------------------------------- ** CALCULATION OF TEMPORAL MEANS (MOMENTS) --------------------------------------- NBMOMT = 0 (Number of moments ) ----------------------------------------------------------- ** BASE ITERATIVE SOLVERS ---------------------- -------------------------------------------------- Variable IRESOL NITMAX EPSILO IDIRCL -------------------------------------------------- Pressure 0 10000 0.1000E-07 1 VelocityX -1 10000 0.1000E-07 1 VelocityY -1 10000 0.1000E-07 1 VelocityZ -1 10000 0.1000E-07 1 TurbEner -1 10000 0.1000E-07 1 Dissip -1 10000 0.1000E-07 1 TempK -1 10000 0.1000E-07 1 ----------------------------------- TurbEner 1 -1 0.1500E+01 Dissip 1 -1 0.1500E+01 TempK 1 -1 0.1500E+01 ----------------------------------- NSWRGR = (nb sweep gradient reconstr. ) NSWRSM = (nb sweep rhs reconstrcution ) EPSRGR = (grad. reconstruction prec. ) EPSRSM = (rhs reconstruction prec. ) EXTRAG = [0.;1.] (gradients extrapolation ) IRCFLU = 0 ou 1 (flow reconstruction ) IMLIGR = < 0, 0 ou 1 (gradient limitation method ) CLIMGR = > 1 ou 1 (gradient limitation coeff. ) ----------------------------------------------------------- ** FACE INTERPOLATION ------------------ IMVISF = 0 (0 arithmetic ) ----------------------------------------------------------- ** CALCULATION OF TEMPORAL MEANS (MOMENTS) --------------------------------------- NBMOMT = 0 (Number of moments ) ----------------------------------------------------------- ** BASE ITERATIVE SOLVERS ---------------------- -------------------------------------------------- Variable IRESOL NITMAX EPSILO IDIRCL -------------------------------------------------- Pressure 0 10000 0.1000E-07 1 VelocityX -1 10000 0.1000E-07 1 VelocityY -1 10000 0.1000E-07 1 VelocityZ -1 10000 0.1000E-07 1 TurbEner -1 10000 0.1000E-07 1 Dissip -1 10000 0.1000E-07 1 TempK -1 10000 0.1000E-07 1 ------------------------------------------------------------- ICONV = 0 ou 1 (1 for convection active ) IDIFF = 0 ou 1 (1 for total diffusion active) IDIFFT = 0 ou 1 (1 for turbulent diff. active) ISCHCV = 0 ou 1 (SOLU or CD ) ISSTPC = 0 ou 1 (1: no slope test ) BLENCV = [0.;1.] (1-upwind proportion ) THETAV = [0.;1.] (0.5 Crank-Nicolson/AB ) (theta for convection- ) (diffusion terms uses ) ((1-theta).old+theta.new ) ----------------------------------------------------------- ** STOKES ------ IVELCO = 1 (0: segregated solving of the velocity components during the prediction step 1: coupled solving of the velocity components ) IPHYDR = 0 (1: account for explicit balance between pressure gradient, gravity source terms, and head losses ) ICALHY = 0 (1: compute hydrastatic pressure for Dirichlet conditions for pressure on outlet ) IPRCO = 1 (1: pressure-continuity ) IPUCOU = 0 (1: reinforced U-P coupling ) NTERUP = 1 (n: n sweeps on navsto for velocity/pressure coupling ) -- Continuous phase: IREVMC = 0 (Velocity reconstruction mode) RELAXV = 0.10000E+01 for pressure (relaxation) ARAK = 0.10000E+01 (Arakawa factor ) ----------------------------------- IRESOL = -1 (automatic solver choice ) IPOL*1000 + 0 (p conjuguate gradient ) 1 (Jacobi ) IPOL*1000 + 2 (bicgstab ) avec IPOL (preconditioning degree ) NITMAX = (max number of iterations ) EPSILO = (resolution precision ) IDIRCL = 0 ou 1 (shift diagonal if ISTAT=0 and no Dirichlet ) ----------------------------------------------------------- ** MULTIGRID --------- NCEGRM = 30 (Max nb cells coarsest grid ) NGRMAX = 25 (Max number of levels ) -------------------------------------- Variable IMGR NCYMAX NITMGF -------------------------------------- Pressure 1 100 10 VelocityX 0 100 10 VelocityY 0 100 10 VelocityZ 0 100 10 TurbEner 0 100 10 Dissip 0 100 10 TempK 0 100 10 ------------------------------ IMGR = 0 ou 1 (1: multigrid activated ) NCYMAX = (Max number of cycles ) NITMGF = (Max nb iter on coarsest grid) Multigrid rank merge parameters: mean coarse cells merge threshold: 300 total coarse cells merge threshold: 500 minimum ranks merge threshold: 1 merge stride: 1 Multigrid coarsening type: algebraic, face traveral by criteria gradient, gravity source terms, and head losses ) ICALHY = 0 (1: compute hydrastatic pressure for Dirichlet conditions for pressure on outlet ) IPRCO = 1 (1: pressure-continuity ) IPUCOU = 0 (1: reinforced U-P coupling ) NTERUP = 1 (n: n sweeps on navsto for velocity/pressure coupling ) -- Continuous phase: IREVMC = 0 (Velocity reconstruction mode) RELAXV = 0.10000E+01 for pressure (relaxation) ARAK = 0.10000E+01 (Arakawa factor ) ISTMPF = 1 (time scheme for flow (0: explicit (THETFL = 0 ) (1: std scheme (Saturne 1.0 ) (2: 2nd-order (THETFL = 0.5 ) THETFL = -0.99900E+03 (theta for mass flow ) IROEXT = 0 (density extrapolation (0: explicit (1: n+thetro with thetro=1/2 (2: n+thetro with thetro=1 THETRO = 0.00000E+00 (theta for density ((1+theta).new-theta.old IVIEXT = 0 (total viscosity extrapolation (0: explicit (1: n+thetvi with thetro=1/2 (2: n+thetvi with thetro=1 THETVI = 0.00000E+00 (theta for total viscosity ((1+theta).new-theta.old TempK 1 0 0.8000E+00 ------------------------------------------- ------------------------------------------------------- Variable Number ICLVFL SCAMIN SCAMAX ------------------------------------------------------- TempK 1 -1 0.0000E+00 0.1000E+13 ------------------------------------------------------- ------------------------------------------------------------- For each scalar, the number indicates it's rank in the list of all scalars. User scalars are placed first, from 1 to NSCAUS. Specific physics scalars are placed at the end, from NSCAUS+1 to NSCAPP+NSCAUS=NSCAL. ISCSTH = -1,0, 1 ou 2 (T (C), Passive, T (K) or H ) IVISLS = 0 ou >0 (Viscosity: constant or not ) VISLS0 = >0 (Reference viscosity ) SIGMAS = >0 (Schmidt ) ISCAVR = 0 ou >0 (Associat. scalar if variance) RVARFL = >0 (Rf, cf variance dissipation ) ICLVFL = 0, 1 ou 2 (Variance clipping mode ) SCAMIN = (Min authorized value ) SCAMAX = (Max authorized value ) For variances, SCAMIN is ignored and SCAMAX is used only if ICLVFL = 2 ------------------------------------------------------ Scalar THETSS IVSEXT THETVS ------------------------------------------------------ 1 0.0000E+00 0 0.0000E+00 ------------------------------------------------------ THETSS = (theta for source terms ) ((1+theta).new-theta.old ) IVSEXT = (extrap. total viscosity ) (0: explicit ) (1: n+thetvs with thetvs=1/2 ) (2: n+thetvs with thetvs=1 ) THETVS = (theta for scalar diffusivity ((1+theta).new-theta.old ) ----------------------------------------------------------- ** CALCULATION MANAGEMENT ---------------------- --- Restarted calculation ISUITE = 0 (1: restarted calculation ) ------------------------------------------------------- Variable Number ICLVFL SCAMIN SCAMAX ------------------------------------------------------- TempK 1 -1 0.0000E+00 0.1000E+13 ------------------------------------------------------- ------------------------------------------------------------- For each scalar, the number indicates it's rank in the list of all scalars. User scalars are placed first, from 1 to NSCAUS. Specific physics scalars are placed at the end, from NSCAUS+1 to NSCAPP+NSCAUS=NSCAL. ISCSTH = -1,0, 1 ou 2 (T (C), Passive, T (K) or H ) IVISLS = 0 ou >0 (Viscosity: constant or not ) VISLS0 = >0 (Reference viscosity ) SIGMAS = >0 (Schmidt ) ISCAVR = 0 ou >0 (Associat. scalar if variance) RVARFL = >0 (Rf, cf variance dissipation ) ICLVFL = 0, 1 ou 2 (Variance clipping mode ) SCAMIN = (Min authorized value ) SCAMAX = (Max authorized value ) For variances, SCAMIN is ignored and SCAMAX is used only if ICLVFL = 2 ------------------------------------------------------ Scalar THETSS IVSEXT THETVS ------------------------------------------------------ 1 0.0000E+00 0 0.0000E+00 ------------------------------------------------------ THETSS = (theta for source terms ) ((1+theta).new-theta.old ) IVSEXT = (extrap. total viscosity ) (0: explicit ) (1: n+thetvs with thetvs=1/2 ) (2: n+thetvs with thetvs=1 ) THETVS = (theta for scalar diffusivity ((1+theta).new-theta.old ) ----------------------------------------------------------- ** CALCULATION MANAGEMENT ---------------------- --- Restarted calculation ISUITE = 0 (1: restarted calculation ) IRESOL = -1 (automatic solver choice ) IPOL*1000 + 0 (p conjuguate gradient ) 1 (Jacobi ) IPOL*1000 + 2 (bicgstab ) avec IPOL (preconditioning degree ) NITMAX = (max number of iterations ) EPSILO = (resolution precision ) IDIRCL = 0 ou 1 (shift diagonal if ISTAT=0 and no Dirichlet ) ----------------------------------------------------------- ** MULTIGRID --------- NCEGRM = 30 (Max nb cells coarsest grid ) NGRMAX = 25 (Max number of levels ) -------------------------------------- Variable IMGR NCYMAX NITMGF -------------------------------------- Pressure 1 100 10 VelocityX 0 100 10 VelocityY 0 100 10 VelocityZ 0 100 10 TurbEner 0 100 10 Dissip 0 100 10 TempK 0 100 10 ------------------------------ IMGR = 0 ou 1 (1: multigrid activated ) NCYMAX = (Max number of cycles ) NITMGF = (Max nb iter on coarsest grid) Multigrid rank merge parameters: mean coarse cells merge threshold: 300 total coarse cells merge threshold: 500 minimum ranks merge threshold: 1 merge stride: 1 Multigrid coarsening type: algebraic, face traveral by criteria ----------------------------------------------------------- ** SCALARS ------- ITBRRB = 0 (T or H reconstruction at bdy) --------------------------------------------------------------------- Variable Number ISCSTH IVISLS ITURT VISLS0 SIGMAS --------------------------------------------------------------------- TempK 1 1 12 0 0.6155E+00 0.1000E+01 --------------------------------------------------------------------- ------------------------------------------- Variable Number ISCAVR RVARFL ------------------------------------------- ISTMPF = 1 (time scheme for flow (0: explicit (THETFL = 0 ) (1: std scheme (Saturne 1.0 ) (2: 2nd-order (THETFL = 0.5 ) THETFL = -0.99900E+03 (theta for mass flow ) IROEXT = 0 (density extrapolation (0: explicit (1: n+thetro with thetro=1/2 (2: n+thetro with thetro=1 THETRO = 0.00000E+00 (theta for density ((1+theta).new-theta.old IVIEXT = 0 (total viscosity extrapolation (0: explicit (1: n+thetvi with thetro=1/2 (2: n+thetvi with thetro=1 THETVI = 0.00000E+00 (theta for total viscosity ((1+theta).new-theta.old ICPEXT = 0 (specific heat extrapolation (0: explicit (1: n+thetcp with thetro=1/2 (2: n+thetcp with thetro=1 THETCP = 0.00000E+00 (specific heat theta-scheme ((1+theta).new-theta.old THETSN = 0.00000E+00 (Nav-Stokes S.T. theta scheme) ((1+theta).new-theta.old THETST = 0.00000E+00 (Turbulence S.T. theta-scheme) ((1+theta).new-theta.old EPSUP = 0.10000E-04 (Velocity/pressure coupling stop test ) ----------------------------------------------------------- ** GRADIENTS CALCULATION --------------------- IMRGRA = 0 (Reconstruction mode ) ANOMAX = 0.78540E+00 (Non-ortho angle: limit for ) (least squares ext. neighbors) ------------------------------------------------------------------- Variable NSWRGR NSWRSM EPSRGR EPSRSM EXTRAG ----------------------------------------------------------- ** SCALARS ------- ITBRRB = 0 (T or H reconstruction at bdy) --------------------------------------------------------------------- Variable Number ISCSTH IVISLS ITURT VISLS0 SIGMAS --------------------------------------------------------------------- TempK 1 1 12 0 0.6155E+00 0.1000E+01 --------------------------------------------------------------------- ------------------------------------------- Variable Number ISCAVR RVARFL ------------------------------------------- TempK 1 0 0.8000E+00 ------------------------------------------- ------------------------------------------------------- Variable Number ICLVFL SCAMIN SCAMAX ------------------------------------------------------- TempK 1 -1 0.0000E+00 0.1000E+13 ------------------------------------------------------- ------------------------------------------------------------- For each scalar, the number indicates it's rank in the list of all scalars. User scalars are placed first, from 1 to NSCAUS. Specific physics scalars are placed at the end, from NSCAUS+1 to NSCAPP+NSCAUS=NSCAL. ISCSTH = -1,0, 1 ou 2 (T (C), Passive, T (K) or H ) IVISLS = 0 ou >0 (Viscosity: constant or not ) VISLS0 = >0 (Reference viscosity ) SIGMAS = >0 (Schmidt ) ISCAVR = 0 ou >0 (Associat. scalar if variance) RVARFL = >0 (Rf, cf variance dissipation ) ICLVFL = 0, 1 ou 2 (Variance clipping mode ) SCAMIN = (Min authorized value ) SCAMAX = (Max authorized value ) For variances, SCAMIN is ignored and SCAMAX is used only if ICLVFL = 2 ------------------------------------------------------ Scalar THETSS IVSEXT THETVS ------------------------------------------------------ ICPEXT = 0 (specific heat extrapolation (0: explicit (1: n+thetcp with thetro=1/2 (2: n+thetcp with thetro=1 THETCP = 0.00000E+00 (specific heat theta-scheme ((1+theta).new-theta.old THETSN = 0.00000E+00 (Nav-Stokes S.T. theta scheme) ((1+theta).new-theta.old THETST = 0.00000E+00 (Turbulence S.T. theta-scheme) ((1+theta).new-theta.old EPSUP = 0.10000E-04 (Velocity/pressure coupling stop test ) ----------------------------------------------------------- ** GRADIENTS CALCULATION --------------------- IMRGRA = 0 (Reconstruction mode ) ANOMAX = 0.78540E+00 (Non-ortho angle: limit for ) (least squares ext. neighbors) ------------------------------------------------------------------- Variable NSWRGR NSWRSM EPSRGR EPSRSM EXTRAG ------------------------------------------------------------------- Pressure 100 2 0.1000E-04 0.1000E-06 0.0000E+00 VelocityX 100 10 0.1000E-04 0.1000E-06 0.0000E+00 VelocityY 100 10 0.1000E-04 0.1000E-06 0.0000E+00 VelocityZ 100 10 0.1000E-04 0.1000E-06 0.0000E+00 ILEAUX = 1 (1: read restart/auxiliary ) IECAUX = 1 (1: write checkpoint/auxiliary) --- Calculation time The numbering of time steps and the measure of simulated physical time are absolute values, and not values relative to the current calculation. INPDT0 = 0 (1: 0 time step calcuation ) NTMABS = 10 (Final time step required ) --- CPU time margin TMARUS = -0.10000E+01 (CPU time margin before stop ) ----------------------------------------------------------- ** INPUT-OUTPUT ------------ --- Restart file NTSUIT = -1 (Checkpoint frequency ) --- Post-processed variables Number Name 9 Density 10 LamVisc 15 SpecHeat 16 ThermalCond -- -- --- Probe history files NTHIST = -1 (Output frequency ) FRHIST = -.10000E+01 (Output frequency (s) ) NCAPT = 0 (Number of probes ) NTHSAV = -1 (Checkpoint frequency ) Number Name Nb. probes (-1: all) 2 Pressure -1 3 VelocityX -1 4 VelocityY -1 5 VelocityZ -1 6 TurbEner -1 7 Dissip -1 ILEAUX = 1 (1: read restart/auxiliary ) IECAUX = 1 (1: write checkpoint/auxiliary) --- Calculation time The numbering of time steps and the measure of simulated physical time are absolute values, and not values relative to the current calculation. INPDT0 = 0 (1: 0 time step calcuation ) NTMABS = 10 (Final time step required ) --- CPU time margin TMARUS = -0.10000E+01 (CPU time margin before stop ) ----------------------------------------------------------- ** INPUT-OUTPUT ------------ --- Restart file NTSUIT = -1 (Checkpoint frequency ) --- Post-processed variables Number Name 9 Density 10 LamVisc 15 SpecHeat 16 ThermalCond -- -- --- Probe history files NTHIST = -1 (Output frequency ) FRHIST = -.10000E+01 (Output frequency (s) ) NCAPT = 0 (Number of probes ) NTHSAV = -1 (Checkpoint frequency ) TempK 1 0 0.8000E+00 ------------------------------------------- ------------------------------------------------------- Variable Number ICLVFL SCAMIN SCAMAX ------------------------------------------------------- TempK 1 -1 0.0000E+00 0.1000E+13 ------------------------------------------------------- ------------------------------------------------------------- For each scalar, the number indicates it's rank in the list of all scalars. User scalars are placed first, from 1 to NSCAUS. Specific physics scalars are placed at the end, from NSCAUS+1 to NSCAPP+NSCAUS=NSCAL. ISCSTH = -1,0, 1 ou 2 (T (C), Passive, T (K) or H ) IVISLS = 0 ou >0 (Viscosity: constant or not ) VISLS0 = >0 (Reference viscosity ) SIGMAS = >0 (Schmidt ) ISCAVR = 0 ou >0 (Associat. scalar if variance) RVARFL = >0 (Rf, cf variance dissipation ) ICLVFL = 0, 1 ou 2 (Variance clipping mode ) SCAMIN = (Min authorized value ) SCAMAX = (Max authorized value ) For variances, SCAMIN is ignored and SCAMAX is used only if ICLVFL = 2 ------------------------------------------------------ Scalar THETSS IVSEXT THETVS ------------------------------------------------------ 1 0.0000E+00 0 0.0000E+00 ------------------------------------------------------ THETSS = (theta for source terms ) ((1+theta).new-theta.old ) IVSEXT = (extrap. total viscosity ) (0: explicit ) (1: n+thetvs with thetvs=1/2 ) (2: n+thetvs with thetvs=1 ) THETVS = (theta for scalar diffusivity ((1+theta).new-theta.old ) ----------------------------------------------------------- ** CALCULATION MANAGEMENT ---------------------- --- Restarted calculation ISUITE = 0 (1: restarted calculation ) Number Name Nb. probes (-1: all) 2 Pressure -1 3 VelocityX -1 4 VelocityY -1 5 VelocityZ -1 6 TurbEner -1 7 Dissip -1 8 TempK -1 9 Density -1 10 LamVisc -1 11 TurbVisc -1 12 CourantNb -1 13 FourierNb -1 14 total_pressure -1 15 SpecHeat -1 16 ThermalCond -1 17 LocalTime -1 -- -- -- --- Log files NTLIST = -1 (Output frequency ) Number Name IWARNI verbosity level (-999: not applicable) 9 Density -999 10 LamVisc -999 15 SpecHeat -999 16 ThermalCond -999 ------------------------------------------------------------------- Pressure 100 2 0.1000E-04 0.1000E-06 0.0000E+00 VelocityX 100 10 0.1000E-04 0.1000E-06 0.0000E+00 VelocityY 100 10 0.1000E-04 0.1000E-06 0.0000E+00 VelocityZ 100 10 0.1000E-04 0.1000E-06 0.0000E+00 TurbEner 100 1 0.1000E-04 0.1000E-06 0.0000E+00 Dissip 100 1 0.1000E-04 0.1000E-06 0.0000E+00 TempK 100 1 0.1000E-04 0.1000E-06 0.0000E+00 ----------------------------------------------------------- ------------------------------------------- Variable IRCFLU IMLIGR CLIMGR ------------------------------------------- Pressure 1 -1 0.1500E+01 VelocityX 1 -1 0.1500E+01 1 0.0000E+00 0 0.0000E+00 ------------------------------------------------------ THETSS = (theta for source terms ) ((1+theta).new-theta.old ) IVSEXT = (extrap. total viscosity ) (0: explicit ) (1: n+thetvs with thetvs=1/2 ) (2: n+thetvs with thetvs=1 ) THETVS = (theta for scalar diffusivity ((1+theta).new-theta.old ) ----------------------------------------------------------- ** CALCULATION MANAGEMENT ---------------------- --- Restarted calculation ISUITE = 0 (1: restarted calculation ) ILEAUX = 1 (1: read restart/auxiliary ) IECAUX = 1 (1: write checkpoint/auxiliary) --- Calculation time The numbering of time steps and the measure of simulated physical time are absolute values, and not values relative to the current calculation. INPDT0 = 0 (1: 0 time step calcuation ) NTMABS = 10 (Final time step required ) --- CPU time margin TMARUS = -0.10000E+01 (CPU time margin before stop ) ----------------------------------------------------------- ** INPUT-OUTPUT ------------ --- Restart file NTSUIT = -1 (Checkpoint frequency ) --- Post-processed variables Number Name 9 Density 10 LamVisc TurbEner 100 1 0.1000E-04 0.1000E-06 0.0000E+00 Dissip 100 1 0.1000E-04 0.1000E-06 0.0000E+00 TempK 100 1 0.1000E-04 0.1000E-06 0.0000E+00 ----------------------------------------------------------- ------------------------------------------- Variable IRCFLU IMLIGR CLIMGR ------------------------------------------- Pressure 1 -1 0.1500E+01 VelocityX 1 -1 0.1500E+01 VelocityY 1 -1 0.1500E+01 VelocityZ 1 -1 0.1500E+01 TurbEner 1 -1 0.1500E+01 Dissip 1 -1 0.1500E+01 TempK 1 -1 0.1500E+01 8 TempK -1 9 Density -1 10 LamVisc -1 11 TurbVisc -1 12 CourantNb -1 13 FourierNb -1 14 total_pressure -1 15 SpecHeat -1 16 ThermalCond -1 17 LocalTime -1 -- -- -- --- Log files NTLIST = -1 (Output frequency ) Number Name IWARNI verbosity level (-999: not applicable) 9 Density -999 10 LamVisc -999 15 SpecHeat -999 16 ThermalCond -999 -- -- -- --- Additional post-processing variables (ipstdv) ipstfo = 0 (Force exerted at boundary) ipstyp = 0 (Yplus at boundary) ipstft = 1 (Thermal flow at boundary) ipsttb = 1 (Temperature at boundary) ipstnu = 1 (Nusselt at boundary) ----------------------------------------------------------- ** ALE METHOD (MOVING MESH) ----------- IALE = 0 (1: activated ) NALINF = 0 (Fluid initialization ILEAUX = 1 (1: read restart/auxiliary ) IECAUX = 1 (1: write checkpoint/auxiliary) --- Calculation time The numbering of time steps and the measure of simulated physical time are absolute values, and not values relative to the current calculation. INPDT0 = 0 (1: 0 time step calcuation ) NTMABS = 10 (Final time step required ) --- CPU time margin TMARUS = -0.10000E+01 (CPU time margin before stop ) ----------------------------------------------------------- ** INPUT-OUTPUT ------------ --- Restart file NTSUIT = -1 (Checkpoint frequency ) --- Post-processed variables Number Name 9 Density 10 LamVisc 15 SpecHeat 16 ThermalCond -- -- --- Probe history files NTHIST = -1 (Output frequency ) FRHIST = -.10000E+01 (Output frequency (s) ) NCAPT = 0 (Number of probes ) NTHSAV = -1 (Checkpoint frequency ) Number Name Nb. probes (-1: all) 2 Pressure -1 3 VelocityX -1 4 VelocityY -1 5 VelocityZ -1 6 TurbEner -1 7 Dissip -1 8 TempK -1 9 Density -1 10 LamVisc -1 11 TurbVisc -1 12 CourantNb -1 13 FourierNb -1 14 total_pressure -1 15 SpecHeat -1 16 ThermalCond -1 iterations) ----------------------------------------------------------- -- -- -- --- Additional post-processing variables (ipstdv) ipstfo = 0 (Force exerted at boundary) ipstyp = 0 (Yplus at boundary) ipstft = 1 (Thermal flow at boundary) ipsttb = 1 (Temperature at boundary) ipstnu = 1 (Nusselt at boundary) ----------------------------------------------------------- ** ALE METHOD (MOVING MESH) ----------- IALE = 0 (1: activated ) NALINF = 0 (Fluid initialization iterations) ----------------------------------------------------------- VelocityY 1 -1 0.1500E+01 VelocityZ 1 -1 0.1500E+01 TurbEner 1 -1 0.1500E+01 Dissip 1 -1 0.1500E+01 TempK 1 -1 0.1500E+01 ----------------------------------- NSWRGR = (nb sweep gradient reconstr. ) NSWRSM = (nb sweep rhs reconstrcution ) EPSRGR = (grad. reconstruction prec. ) EPSRSM = (rhs reconstruction prec. ) EXTRAG = [0.;1.] (gradients extrapolation ) IRCFLU = 0 ou 1 (flow reconstruction ) IMLIGR = < 0, 0 ou 1 (gradient limitation method ) CLIMGR = > 1 ou 1 (gradient limitation coeff. ) ----------------------------------------------------------- ** FACE INTERPOLATION ------------------ IMVISF = 0 (0 arithmetic ) ----------------------------------------------------------- ** CALCULATION OF TEMPORAL MEANS (MOMENTS) --------------------------------------- NBMOMT = 0 (Number of moments ) ----------------------------------------------------------- 15 SpecHeat 16 ThermalCond -- -- --- Probe history files NTHIST = -1 (Output frequency ) FRHIST = -.10000E+01 (Output frequency (s) ) NCAPT = 0 (Number of probes ) NTHSAV = -1 (Checkpoint frequency ) Number Name Nb. probes (-1: all) 2 Pressure -1 3 VelocityX -1 4 VelocityY -1 5 VelocityZ -1 6 TurbEner -1 7 Dissip -1 8 TempK -1 9 Density -1 10 LamVisc -1 11 TurbVisc -1 12 CourantNb -1 13 FourierNb -1 14 total_pressure -1 15 SpecHeat -1 16 ThermalCond -1 17 LocalTime -1 -- -- -- --- Log files NTLIST = -1 (Output frequency ) Number Name IWARNI verbosity level (-999: not applicable) 9 Density -999 10 LamVisc -999 15 SpecHeat -999 16 ThermalCond -999 -- -- -- --- Additional post-processing variables (ipstdv) ipstfo = 0 (Force exerted at boundary) ipstyp = 0 (Yplus at boundary) ipstft = 1 (Thermal flow at boundary) ipsttb = 1 (Temperature at boundary) ipstnu = 1 (Nusselt at boundary) ----------------------------------- NSWRGR = (nb sweep gradient reconstr. ) NSWRSM = (nb sweep rhs reconstrcution ) EPSRGR = (grad. reconstruction prec. ) EPSRSM = (rhs reconstruction prec. ) EXTRAG = [0.;1.] (gradients extrapolation ) IRCFLU = 0 ou 1 (flow reconstruction ) IMLIGR = < 0, 0 ou 1 (gradient limitation method ) CLIMGR = > 1 ou 1 (gradient limitation coeff. ) ----------------------------------------------------------- ** FACE INTERPOLATION ------------------ IMVISF = 0 (0 arithmetic ) ----------------------------------------------------------- ** CALCULATION OF TEMPORAL MEANS (MOMENTS) --------------------------------------- NBMOMT = 0 (Number of moments ) ----------------------------------------------------------- ** BASE ITERATIVE SOLVERS ---------------------- -------------------------------------------------- Variable IRESOL NITMAX EPSILO IDIRCL -------------------------------------------------- 17 LocalTime -1 -- -- -- --- Log files NTLIST = -1 (Output frequency ) Number Name IWARNI verbosity level (-999: not applicable) 9 Density -999 10 LamVisc -999 15 SpecHeat -999 16 ThermalCond -999 -- -- -- --- Additional post-processing variables (ipstdv) ipstfo = 0 (Force exerted at boundary) ipstyp = 0 (Yplus at boundary) ipstft = 1 (Thermal flow at boundary) ipsttb = 1 (Temperature at boundary) ipstnu = 1 (Nusselt at boundary) ----------------------------------------------------------- ** ALE METHOD (MOVING MESH) ----------- IALE = 0 (1: activated ) NALINF = 0 (Fluid initialization iterations) ----------------------------------------------------------- Pressure 0 10000 0.1000E-07 1 VelocityX -1 10000 0.1000E-07 1 VelocityY -1 10000 0.1000E-07 1 VelocityZ -1 10000 0.1000E-07 1 TurbEner -1 10000 0.1000E-07 1 Dissip -1 10000 0.1000E-07 1 TempK -1 10000 0.1000E-07 1 ----------------------------------- ** BASE ITERATIVE SOLVERS ---------------------- -------------------------------------------------- Variable IRESOL NITMAX EPSILO IDIRCL -------------------------------------------------- Pressure 0 10000 0.1000E-07 1 VelocityX -1 10000 0.1000E-07 1 VelocityY -1 10000 0.1000E-07 1 VelocityZ -1 10000 0.1000E-07 1 TurbEner -1 10000 0.1000E-07 1 Dissip -1 10000 0.1000E-07 1 TempK -1 10000 0.1000E-07 1 ----------------------------------- IRESOL = -1 (automatic solver choice ) ----------------------------------------------------------- ** ALE METHOD (MOVING MESH) ----------- IALE = 0 (1: activated ) NALINF = 0 (Fluid initialization iterations) ----------------------------------------------------------- Reading file: mesh_input Reading file: mesh_input IRESOL = -1 (automatic solver choice ) IPOL*1000 + 0 (p conjuguate gradient ) 1 (Jacobi ) IPOL*1000 + 2 (bicgstab ) avec IPOL (preconditioning degree ) NITMAX = (max number of iterations ) EPSILO = (resolution precision ) IDIRCL = 0 ou 1 (shift diagonal if ISTAT=0 and no Dirichlet ) ----------------------------------------------------------- ** MULTIGRID --------- NCEGRM = 30 (Max nb cells coarsest grid ) NGRMAX = 25 (Max number of levels ) -------------------------------------- Variable IMGR NCYMAX NITMGF -------------------------------------- IPOL*1000 + 0 (p conjuguate gradient ) 1 (Jacobi ) IPOL*1000 + 2 (bicgstab ) avec IPOL (preconditioning degree ) NITMAX = (max number of iterations ) EPSILO = (resolution precision ) IDIRCL = 0 ou 1 (shift diagonal if ISTAT=0 and no Dirichlet ) ----------------------------------------------------------- ** MULTIGRID --------- NCEGRM = 30 (Max nb cells coarsest grid ) NGRMAX = 25 (Max number of levels ) -------------------------------------- Variable IMGR NCYMAX NITMGF -------------------------------------- Pressure 1 100 10 VelocityX 0 100 10 VelocityY 0 100 10 VelocityZ 0 100 10 TurbEner 0 100 10 Dissip 0 100 10 TempK 0 100 10 ------------------------------ IMGR = 0 ou 1 (1: multigrid activated ) NCYMAX = (Max number of cycles ) NITMGF = (Max nb iter on coarsest grid) Reading file: mesh_input Reading file: mesh_input Pressure 1 100 10 VelocityX 0 100 10 VelocityY 0 100 10 VelocityZ 0 100 10 TurbEner 0 100 10 Dissip 0 100 10 TempK 0 100 10 ------------------------------ IMGR = 0 ou 1 (1: multigrid activated ) NCYMAX = (Max number of cycles ) NITMGF = (Max nb iter on coarsest grid) Multigrid rank merge parameters: mean coarse cells merge threshold: 300 total coarse cells merge threshold: 500 minimum ranks merge threshold: 1 merge stride: 1 Multigrid coarsening type: algebraic, face traveral by criteria ----------------------------------------------------------- Multigrid rank merge parameters: mean coarse cells merge threshold: 300 total coarse cells merge threshold: 500 minimum ranks merge threshold: 1 merge stride: 1 Multigrid coarsening type: algebraic, face traveral by criteria ----------------------------------------------------------- ** SCALARS ------- ITBRRB = 0 (T or H reconstruction at bdy) --------------------------------------------------------------------- Variable Number ISCSTH IVISLS ITURT VISLS0 SIGMAS --------------------------------------------------------------------- ** SCALARS ------- ITBRRB = 0 (T or H reconstruction at bdy) --------------------------------------------------------------------- Variable Number ISCSTH IVISLS ITURT VISLS0 SIGMAS --------------------------------------------------------------------- TempK 1 1 12 0 0.6155E+00 0.1000E+01 --------------------------------------------------------------------- ------------------------------------------- Variable Number ISCAVR RVARFL ------------------------------------------- TempK 1 0 0.8000E+00 ------------------------------------------- TempK 1 1 12 0 0.6155E+00 0.1000E+01 --------------------------------------------------------------------- ------------------------------------------- Variable Number ISCAVR RVARFL ------------------------------------------- TempK 1 0 0.8000E+00 ------------------------------------------- ------------------------------------------------------- Variable Number ICLVFL SCAMIN SCAMAX ------------------------------------------------------- TempK 1 -1 0.0000E+00 0.1000E+13 ------------------------------------------------------- Variable Number ICLVFL SCAMIN SCAMAX ------------------------------------------------------- TempK 1 -1 0.0000E+00 0.1000E+13 ------------------------------------------------------- ------------------------------------------------------- ------------------------------------------------------------- For each scalar, the number indicates it's rank in the list of all scalars. User scalars are placed first, from 1 to NSCAUS. Specific physics scalars are placed at the end, from NSCAUS+1 to NSCAPP+NSCAUS=NSCAL. ISCSTH = -1,0, 1 ou 2 (T (C), Passive, T (K) or H ) IVISLS = 0 ou >0 (Viscosity: constant or not ) VISLS0 = >0 (Reference viscosity ) SIGMAS = >0 (Schmidt ) ISCAVR = 0 ou >0 (Associat. scalar if variance) RVARFL = >0 (Rf, cf variance dissipation ) ICLVFL = 0, 1 ou 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 ------------------------------------------------------------- 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. ISCSTH = -1,0, 1 ou 2 (T (C), Passive, T (K) or H ) IVISLS = 0 ou >0 (Viscosity: constant or not ) VISLS0 = >0 (Reference viscosity ) SIGMAS = >0 (Schmidt ) ISCAVR = 0 ou >0 (Associat. scalar if variance) RVARFL = >0 (Rf, cf variance dissipation ) ICLVFL = 0, 1 ou 2 (Variance clipping mode ) SCAMIN = (Min authorized value ) SCAMAX = (Max authorized value ) For variances, SCAMIN is ignored and SCAMAX is used only if ICLVFL = 2 ------------------------------------------------------ Scalar THETSS IVSEXT THETVS ------------------------------------------------------ 1 0.0000E+00 0 0.0000E+00 ------------------------------------------------------ ------------------------------------------------------ Scalar THETSS IVSEXT THETVS ------------------------------------------------------ 1 0.0000E+00 0 0.0000E+00 ------------------------------------------------------ THETSS = (theta for source terms ) ((1+theta).new-theta.old ) IVSEXT = (extrap. total viscosity ) (0: explicit ) (1: n+thetvs with thetvs=1/2 ) (2: n+thetvs with thetvs=1 ) THETVS = (theta for scalar diffusivity ((1+theta).new-theta.old ) ----------------------------------------------------------- ** CALCULATION MANAGEMENT ---------------------- THETSS = (theta for source terms ) ((1+theta).new-theta.old ) IVSEXT = (extrap. total viscosity ) (0: explicit ) (1: n+thetvs with thetvs=1/2 ) (2: n+thetvs with thetvs=1 ) THETVS = (theta for scalar diffusivity ((1+theta).new-theta.old ) ----------------------------------------------------------- ** CALCULATION MANAGEMENT ---------------------- --- Restarted calculation ISUITE = 0 (1: restarted calculation ) ILEAUX = 1 (1: read restart/auxiliary ) IECAUX = 1 (1: write checkpoint/auxiliary) --- Restarted calculation ISUITE = 0 (1: restarted calculation ) ILEAUX = 1 (1: read restart/auxiliary ) IECAUX = 1 (1: write checkpoint/auxiliary) --- Calculation time The numbering of time steps and the measure of simulated physical time are absolute values, and not values relative to the current calculation. INPDT0 = 0 (1: 0 time step calcuation ) NTMABS = 10 (Final time step required ) --- CPU time margin --- Calculation time The numbering of time steps and the measure of simulated physical time are absolute values, and not values relative to the current calculation. INPDT0 = 0 (1: 0 time step calcuation ) NTMABS = 10 (Final time step required ) --- CPU time margin TMARUS = -0.10000E+01 (CPU time margin before stop ) ----------------------------------------------------------- ** INPUT-OUTPUT ------------ --- Restart file NTSUIT = -1 (Checkpoint frequency ) --- Post-processed variables TMARUS = -0.10000E+01 (CPU time margin before stop ) ----------------------------------------------------------- ** INPUT-OUTPUT ------------ --- Restart file NTSUIT = -1 (Checkpoint frequency ) --- Post-processed variables Number Name 9 Density 10 LamVisc 15 SpecHeat 16 ThermalCond -- -- --- Probe history files Number Name 9 Density 10 LamVisc 15 SpecHeat 16 ThermalCond -- -- --- Probe history files NTHIST = -1 (Output frequency ) FRHIST = -.10000E+01 (Output frequency (s) ) NCAPT = 0 (Number of probes ) NTHSAV = -1 (Checkpoint frequency ) Number Name Nb. probes (-1: all) 2 Pressure -1 3 VelocityX -1 4 VelocityY -1 5 VelocityZ -1 6 TurbEner -1 NTHIST = -1 (Output frequency ) FRHIST = -.10000E+01 (Output frequency (s) ) NCAPT = 0 (Number of probes ) NTHSAV = -1 (Checkpoint frequency ) Number Name Nb. probes (-1: all) 2 Pressure -1 3 VelocityX -1 4 VelocityY -1 5 VelocityZ -1 6 TurbEner -1 7 Dissip -1 8 TempK -1 9 Density -1 10 LamVisc -1 11 TurbVisc -1 12 CourantNb -1 13 FourierNb -1 14 total_pressure -1 15 SpecHeat -1 16 ThermalCond -1 17 LocalTime -1 7 Dissip -1 8 TempK -1 9 Density -1 10 LamVisc -1 11 TurbVisc -1 12 CourantNb -1 13 FourierNb -1 14 total_pressure -1 15 SpecHeat -1 16 ThermalCond -1 17 LocalTime -1 -- -- -- --- Log files NTLIST = -1 (Output frequency ) Number Name IWARNI verbosity level (-999: not applicable) 9 Density -999 10 LamVisc -999 15 SpecHeat -999 -- -- -- --- Log files NTLIST = -1 (Output frequency ) Number Name IWARNI verbosity level (-999: not applicable) 9 Density -999 10 LamVisc -999 15 SpecHeat -999 16 ThermalCond -999 -- -- -- --- Additional post-processing variables (ipstdv) ipstfo = 0 (Force exerted at boundary) ipstyp = 0 (Yplus at boundary) ipstft = 1 (Thermal flow at boundary) ipsttb = 1 (Temperature at boundary) ipstnu = 1 (Nusselt at boundary) ----------------------------------------------------------- 16 ThermalCond -999 -- -- -- --- Additional post-processing variables (ipstdv) ipstfo = 0 (Force exerted at boundary) ipstyp = 0 (Yplus at boundary) ipstft = 1 (Thermal flow at boundary) ipsttb = 1 (Temperature at boundary) ipstnu = 1 (Nusselt at boundary) ----------------------------------------------------------- ** ALE METHOD (MOVING MESH) ----------- IALE = 0 (1: activated ) NALINF = 0 (Fluid initialization iterations) ----------------------------------------------------------- ** ALE METHOD (MOVING MESH) ----------- IALE = 0 (1: activated ) NALINF = 0 (Fluid initialization iterations) ----------------------------------------------------------- Reading file: mesh_input Reading file: mesh_input Finished reading: mesh_input Finished reading: mesh_input No "partition_input/domain_number_6" file available; ---------------------------------------------------------- No "partition_input/domain_number_6" file available; ---------------------------------------------------------- Finished reading: mesh_input No "partition_input/domain_number_6" file available; ---------------------------------------------------------- Finished reading: mesh_input No "partition_input/domain_number_6" file available; ---------------------------------------------------------- Finished reading: mesh_input No "partition_input/domain_number_6" file available; ---------------------------------------------------------- Finished reading: mesh_input No "partition_input/domain_number_6" file available; ---------------------------------------------------------- Partitioning 3475272 cells to 6 domains on 6 ranks (SCOTCH_dgraphPart). Partitioning 3475272 cells to 6 domains on 6 ranks (SCOTCH_dgraphPart). Partitioning 3475272 cells to 6 domains on 6 ranks (SCOTCH_dgraphPart). Partitioning 3475272 cells to 6 domains on 6 ranks (SCOTCH_dgraphPart). Partitioning 3475272 cells to 6 domains on 6 ranks (SCOTCH_dgraphPart). Partitioning 3475272 cells to 6 domains on 6 ranks (SCOTCH_dgraphPart). wall-clock time: 1.697176 s wall-clock time: 1.690330 s wall-clock time: 1.709227 s Number of cells per domain (histogramm): wall-clock time: 1.700486 s Number of cells per domain (histogramm): wall-clock time: 1.700433 s Number of cells per domain (histogramm): wall-clock time: 1.700032 s Number of cells per domain (histogramm): Number of cells per domain (histogramm): Number of cells per domain (histogramm): [ 576043 ; 576676 [ = 1 [ 576676 ; 577310 [ = 0 [ 577310 ; 577944 [ = 0 [ 577944 ; 578578 [ = 0 [ 578578 ; 579212 [ = 0 [ 579212 ; 579845 [ = 4 [ 579845 ; 580479 [ = 0 [ 580479 ; 581113 [ = 0 [ 581113 ; 581747 [ = 0 [ 581747 ; 582381 ] = 1 Writing file: partition_output/domain_number_6 [ 576043 ; 576676 [ = 1 [ 576676 ; 577310 [ = 0 [ 577310 ; 577944 [ = 0 [ 577944 ; 578578 [ = 0 [ 578578 ; 579212 [ = 0 [ 579212 ; 579845 [ = 4 [ 579845 ; 580479 [ = 0 [ 580479 ; 581113 [ = 0 [ 581113 ; 581747 [ = 0 [ 581747 ; 582381 ] = 1 Writing file: partition_output/domain_number_6 [ 576043 ; 576676 [ = 1 [ 576676 ; 577310 [ = 0 [ 577310 ; 577944 [ = 0 [ 577944 ; 578578 [ = 0 [ 578578 ; 579212 [ = 0 [ 579212 ; 579845 [ = 4 [ 579845 ; 580479 [ = 0 [ 580479 ; 581113 [ = 0 [ 581113 ; 581747 [ = 0 [ 581747 ; 582381 ] = 1 Writing file: partition_output/domain_number_6 [ 576043 ; 576676 [ = 1 [ 576676 ; 577310 [ = 0 [ 577310 ; 577944 [ = 0 [ 577944 ; 578578 [ = 0 [ 578578 ; 579212 [ = 0 [ 579212 ; 579845 [ = 4 [ 579845 ; 580479 [ = 0 [ 580479 ; 581113 [ = 0 [ 581113 ; 581747 [ = 0 [ 581747 ; 582381 ] = 1 Writing file: partition_output/domain_number_6 [ 576043 ; 576676 [ = 1 [ 576676 ; 577310 [ = 0 [ 577310 ; 577944 [ = 0 [ 577944 ; 578578 [ = 0 [ 578578 ; 579212 [ = 0 [ 579212 ; 579845 [ = 4 [ 579845 ; 580479 [ = 0 [ 580479 ; 581113 [ = 0 [ 581113 ; 581747 [ = 0 [ 581747 ; 582381 ] = 1 Writing file: partition_output/domain_number_6 [ 576043 ; 576676 [ = 1 [ 576676 ; 577310 [ = 0 [ 577310 ; 577944 [ = 0 [ 577944 ; 578578 [ = 0 [ 578578 ; 579212 [ = 0 [ 579212 ; 579845 [ = 4 [ 579845 ; 580479 [ = 0 [ 580479 ; 581113 [ = 0 [ 581113 ; 581747 [ = 0 [ 581747 ; 582381 ] = 1 Writing file: partition_output/domain_number_6 Finished writing: partition_output/domain_number_6 Partitioning finished (2.52 s) Finished writing: partition_output/domain_number_6 Partitioning finished (2.52 s) Finished writing: partition_output/domain_number_6 Partitioning finished (2.52 s) Finished writing: partition_output/domain_number_6 Finished writing: partition_output/domain_number_6 Partitioning finished (2.52 s) Finished writing: partition_output/domain_number_6 Partitioning finished (2.53 s) Partitioning finished (2.53 s) ---------------------------------------------------------- Halo construction with standard neighborhood ============================================ Face interfaces creation ---------------------------------------------------------- Halo construction with standard neighborhood ============================================ Face interfaces creation ---------------------------------------------------------- Halo construction with standard neighborhood ============================================ Face interfaces creation ---------------------------------------------------------- Halo construction with standard neighborhood ============================================ Face interfaces creation ---------------------------------------------------------- Halo construction with standard neighborhood ============================================ Face interfaces creation Postprocessing output writers: ------------------------------ -1: name: results directory: postprocessing format: EnSight Gold options: binary time dependency: fixed mesh output: ---------------------------------------------------------- Halo construction with standard neighborhood ============================================ Face interfaces creation Vertex interfaces creation Vertex interfaces creation Vertex interfaces creation Vertex interfaces creation Vertex interfaces creation Vertex interfaces creation Halo creation Halo definition Halo creation Halo definition Halo creation Halo definition Halo creation Halo definition Halo creation Halo definition Halo creation Halo definition Local halo definition Local halo definition Local halo definition Local halo definition Local halo definition Local halo definition Distant halo creation Distant halo creation Distant halo creation Distant halo creation Distant halo creation Distant halo creation Updating the faces -> cells connectivity Updating the faces -> cells connectivity Updating the faces -> cells connectivity Updating the faces -> cells connectivity Updating the faces -> cells connectivity Updating the faces -> cells connectivity Histogram of the number of cells per rank: minimum value = 576043 maximum value = 582381 1 : [ 576043 ; 577310 [ = 1 2 : [ 577310 ; 578578 [ = 0 3 : [ 578578 ; 579845 [ = 4 4 : [ 579845 ; 581113 [ = 0 5 : [ 581113 ; 582381 ] = 1 ---------------------------------------------------------- Histogram of the number of standard + halo cells per rank: minimum value = 577402 maximum value = 584436 1 : [ 577402 ; 578808 [ = 1 2 : [ 578808 ; 580215 [ = 0 3 : [ 580215 ; 581622 [ = 4 4 : [ 581622 ; 583029 [ = 0 5 : [ 583029 ; 584436 ] = 1 ---------------------------------------------------------- Histogram of the number of ghost cells per rank: minimum value = 1322 maximum value = 2055 1 : [ 1322 ; 1468 [ = 3 2 : [ 1468 ; 1615 [ = 1 3 : [ 1615 ; 1761 [ = 0 4 : [ 1761 ; 1908 [ = 1 5 : [ 1908 ; 2055 ] = 1 ---------------------------------------------------------- Histogram of the number of interior faces per rank: minimum value = 1120904 maximum value = 1154621 1 : [ 1120904 ; 1127647 [ = 3 2 : [ 1127647 ; 1134390 [ = 1 3 : [ 1134390 ; 1141134 [ = 0 4 : [ 1141134 ; 1147877 [ = 1 5 : [ 1147877 ; 1154621 ] = 1 ---------------------------------------------------------- Histogram of the number of boundary faces per rank: minimum value = 1164945 maximum value = 1178956 1 : [ 1164945 ; 1167747 [ = 1 2 : [ 1167747 ; 1170549 [ = 0 3 : [ 1170549 ; 1173351 [ = 4 4 : [ 1173351 ; 1176153 [ = 0 5 : [ 1176153 ; 1178956 ] = 1 ---------------------------------------------------------- Histogram of the number of cells per rank: minimum value = 576043 maximum value = 582381 1 : [ 576043 ; 577310 [ = 1 2 : [ 577310 ; 578578 [ = 0 3 : [ 578578 ; 579845 [ = 4 4 : [ 579845 ; 581113 [ = 0 5 : [ 581113 ; 582381 ] = 1 ---------------------------------------------------------- Histogram of the number of standard + halo cells per rank: minimum value = 577402 maximum value = 584436 1 : [ 577402 ; 578808 [ = 1 2 : [ 578808 ; 580215 [ = 0 3 : [ 580215 ; 581622 [ = 4 4 : [ 581622 ; 583029 [ = 0 5 : [ 583029 ; 584436 ] = 1 ---------------------------------------------------------- Histogram of the number of ghost cells per rank: minimum value = 1322 maximum value = 2055 1 : [ 1322 ; 1468 [ = 3 2 : [ 1468 ; 1615 [ = 1 3 : [ 1615 ; 1761 [ = 0 4 : [ 1761 ; 1908 [ = 1 5 : [ 1908 ; 2055 ] = 1 ---------------------------------------------------------- Histogram of the number of interior faces per rank: minimum value = 1120904 maximum value = 1154621 1 : [ 1120904 ; 1127647 [ = 3 2 : [ 1127647 ; 1134390 [ = 1 3 : [ 1134390 ; 1141134 [ = 0 4 : [ 1141134 ; 1147877 [ = 1 5 : [ 1147877 ; 1154621 ] = 1 ---------------------------------------------------------- Histogram of the number of boundary faces per rank: minimum value = 1164945 maximum value = 1178956 1 : [ 1164945 ; 1167747 [ = 1 2 : [ 1167747 ; 1170549 [ = 0 3 : [ 1170549 ; 1173351 [ = 4 4 : [ 1173351 ; 1176153 [ = 0 5 : [ 1176153 ; 1178956 ] = 1 ---------------------------------------------------------- Histogram of the number of cells per rank: minimum value = 576043 maximum value = 582381 1 : [ 576043 ; 577310 [ = 1 2 : [ 577310 ; 578578 [ = 0 3 : [ 578578 ; 579845 [ = 4 4 : [ 579845 ; 581113 [ = 0 5 : [ 581113 ; 582381 ] = 1 ---------------------------------------------------------- Histogram of the number of standard + halo cells per rank: minimum value = 577402 maximum value = 584436 1 : [ 577402 ; 578808 [ = 1 2 : [ 578808 ; 580215 [ = 0 3 : [ 580215 ; 581622 [ = 4 4 : [ 581622 ; 583029 [ = 0 5 : [ 583029 ; 584436 ] = 1 ---------------------------------------------------------- Histogram of the number of ghost cells per rank: minimum value = 1322 maximum value = 2055 1 : [ 1322 ; 1468 [ = 3 2 : [ 1468 ; 1615 [ = 1 3 : [ 1615 ; 1761 [ = 0 4 : [ 1761 ; 1908 [ = 1 5 : [ 1908 ; 2055 ] = 1 ---------------------------------------------------------- Histogram of the number of interior faces per rank: minimum value = 1120904 maximum value = 1154621 1 : [ 1120904 ; 1127647 [ = 3 2 : [ 1127647 ; 1134390 [ = 1 3 : [ 1134390 ; 1141134 [ = 0 4 : [ 1141134 ; 1147877 [ = 1 5 : [ 1147877 ; 1154621 ] = 1 ---------------------------------------------------------- Histogram of the number of boundary faces per rank: minimum value = 1164945 maximum value = 1178956 1 : [ 1164945 ; 1167747 [ = 1 2 : [ 1167747 ; 1170549 [ = 0 3 : [ 1170549 ; 1173351 [ = 4 4 : [ 1173351 ; 1176153 [ = 0 5 : [ 1176153 ; 1178956 ] = 1 ---------------------------------------------------------- Histogram of the number of cells per rank: minimum value = 576043 maximum value = 582381 1 : [ 576043 ; 577310 [ = 1 2 : [ 577310 ; 578578 [ = 0 3 : [ 578578 ; 579845 [ = 4 4 : [ 579845 ; 581113 [ = 0 5 : [ 581113 ; 582381 ] = 1 ---------------------------------------------------------- Histogram of the number of standard + halo cells per rank: minimum value = 577402 maximum value = 584436 1 : [ 577402 ; 578808 [ = 1 2 : [ 578808 ; 580215 [ = 0 3 : [ 580215 ; 581622 [ = 4 4 : [ 581622 ; 583029 [ = 0 5 : [ 583029 ; 584436 ] = 1 ---------------------------------------------------------- Histogram of the number of ghost cells per rank: minimum value = 1322 maximum value = 2055 1 : [ 1322 ; 1468 [ = 3 2 : [ 1468 ; 1615 [ = 1 3 : [ 1615 ; 1761 [ = 0 4 : [ 1761 ; 1908 [ = 1 5 : [ 1908 ; 2055 ] = 1 ---------------------------------------------------------- Histogram of the number of interior faces per rank: minimum value = 1120904 maximum value = 1154621 1 : [ 1120904 ; 1127647 [ = 3 2 : [ 1127647 ; 1134390 [ = 1 3 : [ 1134390 ; 1141134 [ = 0 4 : [ 1141134 ; 1147877 [ = 1 5 : [ 1147877 ; 1154621 ] = 1 ---------------------------------------------------------- Histogram of the number of boundary faces per rank: minimum value = 1164945 maximum value = 1178956 1 : [ 1164945 ; 1167747 [ = 1 2 : [ 1167747 ; 1170549 [ = 0 3 : [ 1170549 ; 1173351 [ = 4 4 : [ 1173351 ; 1176153 [ = 0 5 : [ 1176153 ; 1178956 ] = 1 ---------------------------------------------------------- Histogram of the number of cells per rank: minimum value = 576043 maximum value = 582381 1 : [ 576043 ; 577310 [ = 1 2 : [ 577310 ; 578578 [ = 0 3 : [ 578578 ; 579845 [ = 4 4 : [ 579845 ; 581113 [ = 0 5 : [ 581113 ; 582381 ] = 1 ---------------------------------------------------------- Histogram of the number of standard + halo cells per rank: minimum value = 577402 maximum value = 584436 1 : [ 577402 ; 578808 [ = 1 2 : [ 578808 ; 580215 [ = 0 3 : [ 580215 ; 581622 [ = 4 4 : [ 581622 ; 583029 [ = 0 5 : [ 583029 ; 584436 ] = 1 ---------------------------------------------------------- Histogram of the number of ghost cells per rank: minimum value = 1322 maximum value = 2055 1 : [ 1322 ; 1468 [ = 3 2 : [ 1468 ; 1615 [ = 1 3 : [ 1615 ; 1761 [ = 0 4 : [ 1761 ; 1908 [ = 1 5 : [ 1908 ; 2055 ] = 1 ---------------------------------------------------------- Histogram of the number of interior faces per rank: minimum value = 1120904 maximum value = 1154621 1 : [ 1120904 ; 1127647 [ = 3 2 : [ 1127647 ; 1134390 [ = 1 3 : [ 1134390 ; 1141134 [ = 0 4 : [ 1141134 ; 1147877 [ = 1 5 : [ 1147877 ; 1154621 ] = 1 ---------------------------------------------------------- Histogram of the number of boundary faces per rank: minimum value = 1164945 maximum value = 1178956 1 : [ 1164945 ; 1167747 [ = 1 2 : [ 1167747 ; 1170549 [ = 0 3 : [ 1170549 ; 1173351 [ = 4 4 : [ 1173351 ; 1176153 [ = 0 5 : [ 1176153 ; 1178956 ] = 1 ---------------------------------------------------------- Histogram of the number of cells per rank: minimum value = 576043 maximum value = 582381 1 : [ 576043 ; 577310 [ = 1 2 : [ 577310 ; 578578 [ = 0 3 : [ 578578 ; 579845 [ = 4 4 : [ 579845 ; 581113 [ = 0 5 : [ 581113 ; 582381 ] = 1 ---------------------------------------------------------- Histogram of the number of standard + halo cells per rank: minimum value = 577402 maximum value = 584436 1 : [ 577402 ; 578808 [ = 1 2 : [ 578808 ; 580215 [ = 0 3 : [ 580215 ; 581622 [ = 4 4 : [ 581622 ; 583029 [ = 0 5 : [ 583029 ; 584436 ] = 1 ---------------------------------------------------------- Histogram of the number of ghost cells per rank: minimum value = 1322 maximum value = 2055 1 : [ 1322 ; 1468 [ = 3 2 : [ 1468 ; 1615 [ = 1 3 : [ 1615 ; 1761 [ = 0 4 : [ 1761 ; 1908 [ = 1 5 : [ 1908 ; 2055 ] = 1 ---------------------------------------------------------- Histogram of the number of interior faces per rank: minimum value = 1120904 maximum value = 1154621 1 : [ 1120904 ; 1127647 [ = 3 2 : [ 1127647 ; 1134390 [ = 1 3 : [ 1134390 ; 1141134 [ = 0 4 : [ 1141134 ; 1147877 [ = 1 5 : [ 1147877 ; 1154621 ] = 1 ---------------------------------------------------------- Histogram of the number of boundary faces per rank: minimum value = 1164945 maximum value = 1178956 1 : [ 1164945 ; 1167747 [ = 1 2 : [ 1167747 ; 1170549 [ = 0 3 : [ 1170549 ; 1173351 [ = 4 4 : [ 1173351 ; 1176153 [ = 0 5 : [ 1176153 ; 1178956 ] = 1 ---------------------------------------------------------- Histogram of the number of interior faces per cell: minimum value = 2 maximum value = 4 Histogram of the number of interior faces per cell: minimum value = 2 maximum value = 4 Histogram of the number of interior faces per cell: minimum value = 2 maximum value = 4 Histogram of the number of interior faces per cell: minimum value = 2 maximum value = 4 Histogram of the number of interior faces per cell: minimum value = 2 maximum value = 4 Histogram of the number of interior faces per cell: minimum value = 2 maximum value = 4 1 : [ 2 ; 3 [ = 2 2 : [ 3 ; 4 ] = 3475270 ---------------------------------------------------------- Histogram of the number of neighboring domains per rank: minimum value = 2 maximum value = 5 1 : [ 2 ; 3 [ = 2 2 : [ 3 ; 4 [ = 3 3 : [ 4 ; 5 ] = 1 ---------------------------------------------------------- 1 : [ 2 ; 3 [ = 2 2 : [ 3 ; 4 ] = 3475270 ---------------------------------------------------------- Histogram of the number of neighboring domains per rank: minimum value = 2 maximum value = 5 1 : [ 2 ; 3 [ = 2 2 : [ 3 ; 4 [ = 3 3 : [ 4 ; 5 ] = 1 ---------------------------------------------------------- 1 : [ 2 ; 3 [ = 2 2 : [ 3 ; 4 ] = 3475270 ---------------------------------------------------------- Histogram of the number of neighboring domains per rank: minimum value = 2 maximum value = 5 1 : [ 2 ; 3 [ = 2 2 : [ 3 ; 4 [ = 3 3 : [ 4 ; 5 ] = 1 ---------------------------------------------------------- 1 : [ 2 ; 3 [ = 2 2 : [ 3 ; 4 ] = 3475270 ---------------------------------------------------------- Histogram of the number of neighboring domains per rank: minimum value = 2 maximum value = 5 1 : [ 2 ; 3 [ = 2 2 : [ 3 ; 4 [ = 3 3 : [ 4 ; 5 ] = 1 ---------------------------------------------------------- 1 : [ 2 ; 3 [ = 2 2 : [ 3 ; 4 ] = 3475270 ---------------------------------------------------------- Histogram of the number of neighboring domains per rank: minimum value = 2 maximum value = 5 1 : [ 2 ; 3 [ = 2 2 : [ 3 ; 4 [ = 3 3 : [ 4 ; 5 ] = 1 ---------------------------------------------------------- 1 : [ 2 ; 3 [ = 2 2 : [ 3 ; 4 ] = 3475270 ---------------------------------------------------------- Histogram of the number of neighboring domains per rank: minimum value = 2 maximum value = 5 1 : [ 2 ; 3 [ = 2 2 : [ 3 ; 4 [ = 3 3 : [ 4 ; 5 ] = 1 ---------------------------------------------------------- Global definition of the number of elements (cells, vertices, faces...) Global definition of the number of elements (cells, vertices, faces...) Global definition of the number of elements (cells, vertices, faces...) Global definition of the number of elements (cells, vertices, faces...) Global definition of the number of elements (cells, vertices, faces...) Global definition of the number of elements (cells, vertices, faces...) Synchronizing cell families Synchronizing cell families Synchronizing cell families Synchronizing cell families Synchronizing cell families Synchronizing cell families Renumbering mesh: Checking mesh renumbering for threads: ------------------------------------- Renumbering mesh: Checking mesh renumbering for threads: ------------------------------------- Renumbering mesh: Checking mesh renumbering for threads: ------------------------------------- Renumbering mesh: Checking mesh renumbering for threads: ------------------------------------- Renumbering mesh: Checking mesh renumbering for threads: ------------------------------------- Renumbering mesh: Checking mesh renumbering for threads: ------------------------------------- Histogram of volume mesh matrix bandwidth per rank: minimum value = 558516 maximum value = 583668 1 : [ 558516 ; 563546 [ = 1 2 : [ 563546 ; 568576 [ = 0 3 : [ 568576 ; 573607 [ = 0 4 : [ 573607 ; 578637 [ = 3 5 : [ 578637 ; 583668 ] = 2 Histogram of volume mesh matrix profile/lines per rank: minimum value = 650 maximum value = 4833 1 : [ 650 ; 1486 [ = 3 2 : [ 1486 ; 2323 [ = 1 3 : [ 2323 ; 3159 [ = 0 4 : [ 3159 ; 3996 [ = 1 5 : [ 3996 ; 4833 ] = 1 Histogram of volume mesh matrix bandwidth per rank: minimum value = 558516 maximum value = 583668 1 : [ 558516 ; 563546 [ = 1 2 : [ 563546 ; 568576 [ = 0 3 : [ 568576 ; 573607 [ = 0 4 : [ 573607 ; 578637 [ = 3 5 : [ 578637 ; 583668 ] = 2 Histogram of volume mesh matrix profile/lines per rank: minimum value = 650 maximum value = 4833 1 : [ 650 ; 1486 [ = 3 2 : [ 1486 ; 2323 [ = 1 3 : [ 2323 ; 3159 [ = 0 4 : [ 3159 ; 3996 [ = 1 5 : [ 3996 ; 4833 ] = 1 Histogram of volume mesh matrix bandwidth per rank: minimum value = 558516 maximum value = 583668 1 : [ 558516 ; 563546 [ = 1 2 : [ 563546 ; 568576 [ = 0 3 : [ 568576 ; 573607 [ = 0 4 : [ 573607 ; 578637 [ = 3 5 : [ 578637 ; 583668 ] = 2 Histogram of volume mesh matrix profile/lines per rank: minimum value = 650 maximum value = 4833 1 : [ 650 ; 1486 [ = 3 2 : [ 1486 ; 2323 [ = 1 3 : [ 2323 ; 3159 [ = 0 4 : [ 3159 ; 3996 [ = 1 5 : [ 3996 ; 4833 ] = 1 Histogram of volume mesh matrix bandwidth per rank: minimum value = 558516 maximum value = 583668 1 : [ 558516 ; 563546 [ = 1 2 : [ 563546 ; 568576 [ = 0 3 : [ 568576 ; 573607 [ = 0 4 : [ 573607 ; 578637 [ = 3 5 : [ 578637 ; 583668 ] = 2 Histogram of volume mesh matrix profile/lines per rank: minimum value = 650 maximum value = 4833 1 : [ 650 ; 1486 [ = 3 2 : [ 1486 ; 2323 [ = 1 3 : [ 2323 ; 3159 [ = 0 4 : [ 3159 ; 3996 [ = 1 5 : [ 3996 ; 4833 ] = 1 Histogram of volume mesh matrix bandwidth per rank: minimum value = 558516 maximum value = 583668 1 : [ 558516 ; 563546 [ = 1 2 : [ 563546 ; 568576 [ = 0 3 : [ 568576 ; 573607 [ = 0 4 : [ 573607 ; 578637 [ = 3 5 : [ 578637 ; 583668 ] = 2 Histogram of volume mesh matrix profile/lines per rank: minimum value = 650 maximum value = 4833 1 : [ 650 ; 1486 [ = 3 2 : [ 1486 ; 2323 [ = 1 3 : [ 2323 ; 3159 [ = 0 4 : [ 3159 ; 3996 [ = 1 5 : [ 3996 ; 4833 ] = 1 Histogram of volume mesh matrix bandwidth per rank: minimum value = 558516 maximum value = 583668 1 : [ 558516 ; 563546 [ = 1 2 : [ 563546 ; 568576 [ = 0 3 : [ 568576 ; 573607 [ = 0 4 : [ 573607 ; 578637 [ = 3 5 : [ 578637 ; 583668 ] = 2 Histogram of volume mesh matrix profile/lines per rank: minimum value = 650 maximum value = 4833 1 : [ 650 ; 1486 [ = 3 2 : [ 1486 ; 2323 [ = 1 3 : [ 2323 ; 3159 [ = 0 4 : [ 3159 ; 3996 [ = 1 5 : [ 3996 ; 4833 ] = 1 Mesh coordinates: minimum and maximum X : -3.7999993e+00 3.7999993e+00 Y : -4.0739558e+00 3.8000000e+00 Z : 0.0000000e+00 1.0000000e+00 Mesh Number of cells: 3475272 Number of interior faces: 6795032 Number of boundary faces: 7030448 Number of vertices: 6798566 Mesh coordinates: minimum and maximum X : -3.7999993e+00 3.7999993e+00 Y : -4.0739558e+00 3.8000000e+00 Z : 0.0000000e+00 1.0000000e+00 Mesh Number of cells: 3475272 Number of interior faces: 6795032 Number of boundary faces: 7030448 Number of vertices: 6798566 Mesh coordinates: minimum and maximum X : -3.7999993e+00 3.7999993e+00 Y : -4.0739558e+00 3.8000000e+00 Z : 0.0000000e+00 1.0000000e+00 Mesh Number of cells: 3475272 Number of interior faces: 6795032 Number of boundary faces: 7030448 Number of vertices: 6798566 Mesh coordinates: minimum and maximum X : -3.7999993e+00 3.7999993e+00 Y : -4.0739558e+00 3.8000000e+00 Z : 0.0000000e+00 1.0000000e+00 Mesh Number of cells: 3475272 Number of interior faces: 6795032 Number of boundary faces: 7030448 Number of vertices: 6798566 Mesh coordinates: minimum and maximum X : -3.7999993e+00 3.7999993e+00 Y : -4.0739558e+00 3.8000000e+00 Z : 0.0000000e+00 1.0000000e+00 Mesh Number of cells: 3475272 Number of interior faces: 6795032 Number of boundary faces: 7030448 Number of vertices: 6798566 Mesh coordinates: minimum and maximum X : -3.7999993e+00 3.7999993e+00 Y : -4.0739558e+00 3.8000000e+00 Z : 0.0000000e+00 1.0000000e+00 Mesh Number of cells: 3475272 Number of interior faces: 6795032 Number of boundary faces: 7030448 Number of vertices: 6798566 Groups: "cyls" interior faces: 80 boundary faces: 76000 "fluid" cells: 3475272 "inj_l" boundary faces: 40 "inj_r" boundary faces: 40 "inlet_l" boundary faces: 30 "inlet_r" boundary faces: 30 "outlet" boundary faces: 44 "shell" boundary faces: 3720 "syms" boundary faces: 6950544 Groups: "cyls" interior faces: 80 boundary faces: 76000 "fluid" cells: 3475272 "inj_l" boundary faces: 40 "inj_r" boundary faces: 40 "inlet_l" boundary faces: 30 "inlet_r" boundary faces: 30 "outlet" boundary faces: 44 "shell" boundary faces: 3720 "syms" boundary faces: 6950544 Groups: "cyls" interior faces: 80 boundary faces: 76000 "fluid" cells: 3475272 "inj_l" boundary faces: 40 "inj_r" boundary faces: 40 "inlet_l" boundary faces: 30 "inlet_r" boundary faces: 30 "outlet" boundary faces: 44 "shell" boundary faces: 3720 "syms" boundary faces: 6950544 Groups: "cyls" interior faces: 80 boundary faces: 76000 "fluid" cells: 3475272 "inj_l" boundary faces: 40 "inj_r" boundary faces: 40 "inlet_l" boundary faces: 30 "inlet_r" boundary faces: 30 "outlet" boundary faces: 44 "shell" boundary faces: 3720 "syms" boundary faces: 6950544 Groups: "cyls" interior faces: 80 boundary faces: 76000 "fluid" cells: 3475272 "inj_l" boundary faces: 40 "inj_r" boundary faces: 40 "inlet_l" boundary faces: 30 "inlet_r" boundary faces: 30 "outlet" boundary faces: 44 "shell" boundary faces: 3720 "syms" boundary faces: 6950544 Groups: "cyls" interior faces: 80 boundary faces: 76000 "fluid" cells: 3475272 "inj_l" boundary faces: 40 "inj_r" boundary faces: 40 "inlet_l" boundary faces: 30 "inlet_r" boundary faces: 30 "outlet" boundary faces: 44 "shell" boundary faces: 3720 "syms" boundary faces: 6950544 --- Information on the volumes Minimum control volume = 2.7297972e-07 Maximum control volume = 1.6141728e-04 Total volume for the domain = 4.0350779e+01 --- Information on the volumes Minimum control volume = 2.7297972e-07 Maximum control volume = 1.6141728e-04 Total volume for the domain = 4.0350779e+01 --- Information on the volumes Minimum control volume = 2.7297972e-07 Maximum control volume = 1.6141728e-04 Total volume for the domain = 4.0350779e+01 --- Information on the volumes Minimum control volume = 2.7297972e-07 Maximum control volume = 1.6141728e-04 Total volume for the domain = 4.0350779e+01 --- Information on the volumes Minimum control volume = 2.7297972e-07 Maximum control volume = 1.6141728e-04 Total volume for the domain = 4.0350779e+01 --- Information on the volumes Minimum control volume = 2.7297972e-07 Maximum control volume = 1.6141728e-04 Total volume for the domain = 4.0350779e+01 Criterion 1: Orthogonality: Number of bad cells detected: 0 --> 0 % Criterion 1: Orthogonality: Number of bad cells detected: 0 --> 0 % Criterion 1: Orthogonality: Number of bad cells detected: 0 --> 0 % Criterion 1: Orthogonality: Number of bad cells detected: 0 --> 0 % Criterion 1: Orthogonality: Number of bad cells detected: 0 --> 0 % Criterion 1: Orthogonality: Number of bad cells detected: 0 --> 0 % Criterion 2: Offset: Number of bad cells detected: 0 --> 0 % Criterion 2: Offset: Number of bad cells detected: 0 --> 0 % Criterion 2: Offset: Number of bad cells detected: 0 --> 0 % Criterion 2: Offset: Number of bad cells detected: 0 --> 0 % Criterion 2: Offset: 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: 264 --> 0 % Criterion 3: Least-Squares Gradient Quality: Number of bad cells detected: 264 --> 0 % Criterion 3: Least-Squares Gradient Quality: Number of bad cells detected: 264 --> 0 % Criterion 3: Least-Squares Gradient Quality: Number of bad cells detected: 264 --> 0 % Criterion 3: Least-Squares Gradient Quality: Number of bad cells detected: 264 --> 0 % Criterion 3: Least-Squares Gradient Quality: Number of bad cells detected: 264 --> 0 % Criterion 4: Cells Volume Ratio: Number of bad cells detected: 0 --> 0 % Criterion 4: Cells Volume Ratio: Number of bad cells detected: 0 --> 0 % Criterion 4: Cells Volume Ratio: Number of bad cells detected: 0 --> 0 % Criterion 4: Cells Volume Ratio: Number of bad cells detected: 0 --> 0 % Criterion 4: Cells Volume Ratio: 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 % Warning: -------- Mesh quality issue has been detected The mesh should be re-considered using the listed criteria. The calculation will run but the solution quality may be degraded... Computing geometric quantities (1.63 s) Criterion 5: Guilt by Association: Number of bad cells detected: 0 --> 0 % Warning: -------- Mesh quality issue has been detected The mesh should be re-considered using the listed criteria. The calculation will run but the solution quality may be degraded... Computing geometric quantities (1.63 s) Criterion 5: Guilt by Association: Number of bad cells detected: 0 --> 0 % Warning: -------- Mesh quality issue has been detected The mesh should be re-considered using the listed criteria. The calculation will run but the solution quality may be degraded... Computing geometric quantities (1.63 s) Criterion 5: Guilt by Association: Number of bad cells detected: 0 --> 0 % Warning: -------- Mesh quality issue has been detected The mesh should be re-considered using the listed criteria. The calculation will run but the solution quality may be degraded... Computing geometric quantities (1.63 s) Criterion 5: Guilt by Association: Number of bad cells detected: 0 --> 0 % Warning: -------- Mesh quality issue has been detected The mesh should be re-considered using the listed criteria. The calculation will run but the solution quality may be degraded... Computing geometric quantities (1.63 s) Criterion 5: Guilt by Association: Number of bad cells detected: 0 --> 0 % Warning: -------- Mesh quality issue has been detected The mesh should be re-considered using the listed criteria. The calculation will run but the solution quality may be degraded... Computing geometric quantities (1.63 s) ALMAX = 0.34257E+01 (Characteristic length ) ALMAX is the cubic root of the domain volume. ALMAX is the length used to initialize the turbulence. ALMAX = 0.34257E+01 (Characteristic length ) ALMAX is the cubic root of the domain volume. ALMAX is the length used to initialize the turbulence. ALMAX = 0.34257E+01 (Characteristic length ) ALMAX is the cubic root of the domain volume. ALMAX is the length used to initialize the turbulence. ALMAX = 0.34257E+01 (Characteristic length ) ALMAX is the cubic root of the domain volume. ALMAX is the length used to initialize the turbulence. ALMAX = 0.34257E+01 (Characteristic length ) ALMAX is the cubic root of the domain volume. ALMAX is the length used to initialize the turbulence. ALMAX = 0.34257E+01 (Characteristic length ) ALMAX is the cubic root of the domain volume. ALMAX is the length used to initialize the turbulence. ----------------------------------------------------------- ** VARIABLES INITIALIZATION ------------------------ ----------------------------------------- Variable Min. value Max. value ----------------------------------------- ----------------------------------------------------------- ** VARIABLES INITIALIZATION ------------------------ ----------------------------------------- Variable Min. value Max. value ----------------------------------------- ----------------------------------------------------------- ** VARIABLES INITIALIZATION ------------------------ ----------------------------------------- Variable Min. value Max. value ----------------------------------------- ----------------------------------------------------------- ** VARIABLES INITIALIZATION ------------------------ ----------------------------------------- Variable Min. value Max. value ----------------------------------------- ----------------------------------------------------------- ** VARIABLES INITIALIZATION ------------------------ ----------------------------------------- Variable Min. value Max. value ----------------------------------------- ----------------------------------------------------------- ** VARIABLES INITIALIZATION ------------------------ ----------------------------------------- Variable Min. value Max. value ----------------------------------------- Pressure 0.0000E+00 0.0000E+00 Pressure 0.0000E+00 0.0000E+00 Pressure 0.0000E+00 0.0000E+00 Pressure 0.0000E+00 0.0000E+00 Pressure 0.0000E+00 0.0000E+00 Pressure 0.0000E+00 0.0000E+00 VelocityX 0.3000E+00 0.3000E+00 VelocityY 0.5300E+01 0.5300E+01 VelocityZ 0.0000E+00 0.0000E+00 TurbEner 0.1685E-01 0.1685E-01 Dissip 0.5748E-04 0.5748E-04 TempK 0.3180E+03 0.3180E+03 --------------------------------- LocalTime 0.1000E-02 0.1000E-02 --------------------------------- ------------------------------------------------------------- ------------------------------------------------------------- =============================================================== MAIN CALCULATION ================ =============================================================== =============================================================== INSTANT 0.100000000E-02 TIME STEP NUMBER 1 ============================================================= VelocityX 0.3000E+00 0.3000E+00 VelocityY 0.5300E+01 0.5300E+01 VelocityZ 0.0000E+00 0.0000E+00 TurbEner 0.1685E-01 0.1685E-01 Dissip 0.5748E-04 0.5748E-04 TempK 0.3180E+03 0.3180E+03 --------------------------------- LocalTime 0.1000E-02 0.1000E-02 --------------------------------- ------------------------------------------------------------- ------------------------------------------------------------- =============================================================== MAIN CALCULATION ================ =============================================================== =============================================================== INSTANT 0.100000000E-02 TIME STEP NUMBER 1 ============================================================= VelocityX 0.3000E+00 0.3000E+00 VelocityY 0.5300E+01 0.5300E+01 VelocityZ 0.0000E+00 0.0000E+00 TurbEner 0.1685E-01 0.1685E-01 Dissip 0.5748E-04 0.5748E-04 TempK 0.3180E+03 0.3180E+03 --------------------------------- LocalTime 0.1000E-02 0.1000E-02 --------------------------------- ------------------------------------------------------------- ------------------------------------------------------------- =============================================================== MAIN CALCULATION ================ =============================================================== =============================================================== INSTANT 0.100000000E-02 TIME STEP NUMBER 1 ============================================================= VelocityX 0.3000E+00 0.3000E+00 VelocityY 0.5300E+01 0.5300E+01 VelocityZ 0.0000E+00 0.0000E+00 TurbEner 0.1685E-01 0.1685E-01 Dissip 0.5748E-04 0.5748E-04 TempK 0.3180E+03 0.3180E+03 --------------------------------- LocalTime 0.1000E-02 0.1000E-02 --------------------------------- ------------------------------------------------------------- ------------------------------------------------------------- =============================================================== MAIN CALCULATION ================ =============================================================== =============================================================== INSTANT 0.100000000E-02 TIME STEP NUMBER 1 ============================================================= VelocityX 0.3000E+00 0.3000E+00 VelocityY 0.5300E+01 0.5300E+01 VelocityZ 0.0000E+00 0.0000E+00 TurbEner 0.1685E-01 0.1685E-01 Dissip 0.5748E-04 0.5748E-04 TempK 0.3180E+03 0.3180E+03 --------------------------------- LocalTime 0.1000E-02 0.1000E-02 --------------------------------- ------------------------------------------------------------- ------------------------------------------------------------- =============================================================== MAIN CALCULATION ================ =============================================================== =============================================================== INSTANT 0.100000000E-02 TIME STEP NUMBER 1 ============================================================= VelocityX 0.3000E+00 0.3000E+00 VelocityY 0.5300E+01 0.5300E+01 VelocityZ 0.0000E+00 0.0000E+00 TurbEner 0.1685E-01 0.1685E-01 Dissip 0.5748E-04 0.5748E-04 TempK 0.3180E+03 0.3180E+03 --------------------------------- LocalTime 0.1000E-02 0.1000E-02 --------------------------------- ------------------------------------------------------------- ------------------------------------------------------------- =============================================================== MAIN CALCULATION ================ =============================================================== =============================================================== INSTANT 0.100000000E-02 TIME STEP NUMBER 1 ============================================================= ----------------------------------------- Property Min. value Max. value ----------------------------------------- Density 0.9987E+03 0.9987E+03 LamVisc 0.5716E-03 0.5716E-03 TurbVisc 0.4442E+03 0.4442E+03 SpecHeat 0.4298E+04 0.4298E+04 ----------------------------------------- ----------------------------------------- Property Min. value Max. value ----------------------------------------- Density 0.9987E+03 0.9987E+03 LamVisc 0.5716E-03 0.5716E-03 TurbVisc 0.4442E+03 0.4442E+03 SpecHeat 0.4298E+04 0.4298E+04 ----------------------------------------- ----------------------------------------- Property Min. value Max. value ----------------------------------------- Density 0.9987E+03 0.9987E+03 LamVisc 0.5716E-03 0.5716E-03 TurbVisc 0.4442E+03 0.4442E+03 SpecHeat 0.4298E+04 0.4298E+04 ----------------------------------------- ----------------------------------------- Property Min. value Max. value ----------------------------------------- Density 0.9987E+03 0.9987E+03 LamVisc 0.5716E-03 0.5716E-03 TurbVisc 0.4442E+03 0.4442E+03 SpecHeat 0.4298E+04 0.4298E+04 ----------------------------------------- ----------------------------------------- Property Min. value Max. value ----------------------------------------- Density 0.9987E+03 0.9987E+03 LamVisc 0.5716E-03 0.5716E-03 TurbVisc 0.4442E+03 0.4442E+03 SpecHeat 0.4298E+04 0.4298E+04 ----------------------------------------- ----------------------------------------- Property Min. value Max. value ----------------------------------------- Density 0.9987E+03 0.9987E+03 LamVisc 0.5716E-03 0.5716E-03 TurbVisc 0.4442E+03 0.4442E+03 SpecHeat 0.4298E+04 0.4298E+04 ----------------------------------------- --- Diffusivity: ----------------------------------------------- Scalar Number Min. value Max. value ----------------------------------------------- TempK 1 0.6308E+03 0.6308E+03 ----------------------------------------------- --- Diffusivity: ----------------------------------------------- Scalar Number Min. value Max. value ----------------------------------------------- TempK 1 0.6308E+03 0.6308E+03 ----------------------------------------------- --- Diffusivity: ----------------------------------------------- Scalar Number Min. value Max. value ----------------------------------------------- --- Diffusivity: ----------------------------------------------- Scalar Number Min. value Max. value ----------------------------------------------- TempK 1 0.6308E+03 0.6308E+03 ----------------------------------------------- --- Diffusivity: ----------------------------------------------- Scalar Number Min. value Max. value ----------------------------------------------- TempK 1 0.6308E+03 0.6308E+03 ----------------------------------------------- --- Diffusivity: ----------------------------------------------- Scalar Number Min. value Max. value ----------------------------------------------- TempK 1 0.6308E+03 0.6308E+03 ----------------------------------------------- TempK 1 0.6308E+03 0.6308E+03 ----------------------------------------------- ** INFORMATION ON BOUNDARY FACES TYPE ---------------------------------- ------------------------------------------------------------------------- Boundary type Code Nb faces ------------------------------------------------------------------------- ** INFORMATION ON BOUNDARY FACES TYPE ---------------------------------- ------------------------------------------------------------------------- Boundary type Code Nb faces ------------------------------------------------------------------------- ** INFORMATION ON BOUNDARY FACES TYPE ---------------------------------- ------------------------------------------------------------------------- Boundary type Code Nb faces ------------------------------------------------------------------------- ** INFORMATION ON BOUNDARY FACES TYPE ---------------------------------- ------------------------------------------------------------------------- Boundary type Code Nb faces ------------------------------------------------------------------------- ** INFORMATION ON BOUNDARY FACES TYPE ---------------------------------- ------------------------------------------------------------------------- Boundary type Code Nb faces ------------------------------------------------------------------------- Inlet 2 60 ** INFORMATION ON BOUNDARY FACES TYPE ---------------------------------- ------------------------------------------------------------------------- Boundary type Code Nb faces ------------------------------------------------------------------------- Inlet 2 60 Smooth wall 5 79800 Rough wall 6 0 Inlet 2 60 Smooth wall 5 79800 Rough wall 6 0 Symmetry 4 6950544 Free outlet 3 44 Undefined 1 0 Symmetry 4 6950544 Free outlet 3 44 Undefined 1 0 Smooth wall 5 79800 Rough wall 6 0 Symmetry 4 6950544 Free outlet 3 44 Undefined 1 0 Inlet 2 60 Smooth wall 5 79800 Rough wall 6 0 Symmetry 4 6950544 Free outlet 3 44 Undefined 1 0 Inlet 2 60 Smooth wall 5 79800 Rough wall 6 0 Symmetry 4 6950544 Free outlet 3 44 Undefined 1 0 Inlet 2 60 Smooth wall 5 79800 Rough wall 6 0 Symmetry 4 6950544 Free outlet 3 44 Undefined 1 0 ------------------------------------------------------------------------- ------------------------------------------------------------------------- ------------------------------------------------------------------------- ------------------------------------------------------------------------- ------------------------------------------------------------------------- ------------------------------------------------------------------------- Boundary faces with free inlet/outlet detected Update of reference point for total pressure XYZP0 = 0.11714E+01 -0.40333E+01 0.50000E+00 Boundary faces with free inlet/outlet detected Update of reference point for total pressure XYZP0 = 0.11714E+01 -0.40333E+01 0.50000E+00 Boundary faces with free inlet/outlet detected Update of reference point for total pressure XYZP0 = 0.11714E+01 -0.40333E+01 0.50000E+00 Boundary faces with free inlet/outlet detected Update of reference point for total pressure XYZP0 = 0.11714E+01 -0.40333E+01 0.50000E+00 Boundary faces with free inlet/outlet detected Update of reference point for total pressure XYZP0 = 0.11714E+01 -0.40333E+01 0.50000E+00 Boundary faces with free inlet/outlet detected Update of reference point for total pressure XYZP0 = 0.11714E+01 -0.40333E+01 0.50000E+00 ** BOUNDARY MASS FLOW INFORMATION ------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 60 0.000000000E+00 Smooth wall 5 79800 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 6950544 0.000000000E+00 Free outlet 3 44 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 60 0.000000000E+00 Smooth wall 5 79800 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 6950544 0.000000000E+00 Free outlet 3 44 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 60 0.000000000E+00 Smooth wall 5 79800 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 6950544 0.000000000E+00 Free outlet 3 44 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 60 0.000000000E+00 Smooth wall 5 79800 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 6950544 0.000000000E+00 Free outlet 3 44 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 60 0.000000000E+00 Smooth wall 5 79800 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 6950544 0.000000000E+00 Free outlet 3 44 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 60 0.000000000E+00 Smooth wall 5 79800 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 6950544 0.000000000E+00 Free outlet 3 44 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- --------------------------------------------------------------- --------------------------------------------------------------- --------------------------------------------------------------- --------------------------------------------------------------- --------------------------------------------------------------- TIME FOR THE TIME STEP 1: 0.14945E+04 =============================================================== INSTANT 0.200000000E-02 TIME STEP NUMBER 2 ============================================================= TIME FOR THE TIME STEP 1: 0.14945E+04 =============================================================== INSTANT 0.200000000E-02 TIME STEP NUMBER 2 ============================================================= TIME FOR THE TIME STEP 1: 0.14945E+04 =============================================================== INSTANT 0.200000000E-02 TIME STEP NUMBER 2 ============================================================= TIME FOR THE TIME STEP 1: 0.14945E+04 =============================================================== INSTANT 0.200000000E-02 TIME STEP NUMBER 2 ============================================================= TIME FOR THE TIME STEP 1: 0.14945E+04 =============================================================== INSTANT 0.200000000E-02 TIME STEP NUMBER 2 ============================================================= TIME FOR THE TIME STEP 1: 0.14945E+04 =============================================================== INSTANT 0.200000000E-02 TIME STEP NUMBER 2 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 60 -0.804570765E+03 Smooth wall 5 79800 -0.107327982E-12 Rough wall 6 0 0.000000000E+00 Symmetry 4 6950544 0.000000000E+00 Free outlet 3 44 0.804568416E+03 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 60 -0.804570765E+03 Smooth wall 5 79800 -0.107327982E-12 Rough wall 6 0 0.000000000E+00 Symmetry 4 6950544 0.000000000E+00 Free outlet 3 44 0.804568416E+03 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 60 -0.804570765E+03 Smooth wall 5 79800 -0.107327982E-12 Rough wall 6 0 0.000000000E+00 Symmetry 4 6950544 0.000000000E+00 Free outlet 3 44 0.804568416E+03 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 60 -0.804570765E+03 Smooth wall 5 79800 -0.107327982E-12 Rough wall 6 0 0.000000000E+00 Symmetry 4 6950544 0.000000000E+00 Free outlet 3 44 0.804568416E+03 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 60 -0.804570765E+03 Smooth wall 5 79800 -0.107327982E-12 Rough wall 6 0 0.000000000E+00 Symmetry 4 6950544 0.000000000E+00 Free outlet 3 44 0.804568416E+03 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 60 -0.804570765E+03 Smooth wall 5 79800 -0.107327982E-12 Rough wall 6 0 0.000000000E+00 Symmetry 4 6950544 0.000000000E+00 Free outlet 3 44 0.804568416E+03 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- --------------------------------------------------------------- --------------------------------------------------------------- --------------------------------------------------------------- --------------------------------------------------------------- --------------------------------------------------------------- Incoming flow detained for 20 outlet faces on 44 Incoming flow detained for 20 outlet faces on 44 Incoming flow detained for 20 outlet faces on 44 Incoming flow detained for 20 outlet faces on 44 Incoming flow detained for 20 outlet faces on 44 Incoming flow detained for 20 outlet faces on 44 TIME FOR THE TIME STEP 2: 0.18835E+03 =============================================================== INSTANT 0.300000000E-02 TIME STEP NUMBER 3 ============================================================= TIME FOR THE TIME STEP 2: 0.18835E+03 =============================================================== INSTANT 0.300000000E-02 TIME STEP NUMBER 3 ============================================================= TIME FOR THE TIME STEP 2: 0.18835E+03 =============================================================== INSTANT 0.300000000E-02 TIME STEP NUMBER 3 ============================================================= TIME FOR THE TIME STEP 2: 0.18835E+03 =============================================================== INSTANT 0.300000000E-02 TIME STEP NUMBER 3 ============================================================= TIME FOR THE TIME STEP 2: 0.18835E+03 =============================================================== INSTANT 0.300000000E-02 TIME STEP NUMBER 3 ============================================================= TIME FOR THE TIME STEP 2: 0.18835E+03 =============================================================== INSTANT 0.300000000E-02 TIME STEP NUMBER 3 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 60 -0.804570765E+03 Smooth wall 5 79800 -0.248430391E-12 --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 60 -0.804570765E+03 Smooth wall 5 79800 -0.248430391E-12 Rough wall 6 0 0.000000000E+00 --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 60 -0.804570765E+03 Smooth wall 5 79800 -0.248430391E-12 Rough wall 6 0 0.000000000E+00 Symmetry 4 6950544 0.000000000E+00 --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 60 -0.804570765E+03 Smooth wall 5 79800 -0.248430391E-12 Rough wall 6 0 0.000000000E+00 Symmetry 4 6950544 0.000000000E+00 --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 60 -0.804570765E+03 Smooth wall 5 79800 -0.248430391E-12 Rough wall 6 0 0.000000000E+00 Symmetry 4 6950544 0.000000000E+00 --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 60 -0.804570765E+03 Smooth wall 5 79800 -0.248430391E-12 Rough wall 6 0 0.000000000E+00 Symmetry 4 6950544 0.000000000E+00 Free outlet 3 44 0.804569365E+03 Free outlet 3 44 0.804569365E+03 Undefined 1 0 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 6950544 0.000000000E+00 Free outlet 3 44 0.804569365E+03 Undefined 1 0 0.000000000E+00 Symmetry 4 6950544 0.000000000E+00 Free outlet 3 44 0.804569365E+03 Undefined 1 0 0.000000000E+00 Free outlet 3 44 0.804569365E+03 Undefined 1 0 0.000000000E+00 Free outlet 3 44 0.804569365E+03 Undefined 1 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- --------------------------------------------------------------- --------------------------------------------------------------- --------------------------------------------------------------- --------------------------------------------------------------- --------------------------------------------------------------- Incoming flow detained for 20 outlet faces on 44 Incoming flow detained for 20 outlet faces on 44 Incoming flow detained for 20 outlet faces on 44 Incoming flow detained for 20 outlet faces on 44 Incoming flow detained for 20 outlet faces on 44 Incoming flow detained for 20 outlet faces on 44 TIME FOR THE TIME STEP 3: 0.17558E+03 =============================================================== INSTANT 0.400000000E-02 TIME STEP NUMBER 4 ============================================================= TIME FOR THE TIME STEP 3: 0.17558E+03 =============================================================== INSTANT 0.400000000E-02 TIME STEP NUMBER 4 ============================================================= TIME FOR THE TIME STEP 3: 0.17558E+03 =============================================================== INSTANT 0.400000000E-02 TIME STEP NUMBER 4 ============================================================= TIME FOR THE TIME STEP 3: 0.17558E+03 =============================================================== INSTANT 0.400000000E-02 TIME STEP NUMBER 4 ============================================================= TIME FOR THE TIME STEP 3: 0.17558E+03 =============================================================== INSTANT 0.400000000E-02 TIME STEP NUMBER 4 ============================================================= TIME FOR THE TIME STEP 3: 0.17558E+03 =============================================================== INSTANT 0.400000000E-02 TIME STEP NUMBER 4 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 60 -0.804570765E+03 Smooth wall 5 79800 -0.433244993E-13 Rough wall 6 0 0.000000000E+00 Symmetry 4 6950544 0.000000000E+00 Free outlet 3 44 0.804571614E+03 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 60 -0.804570765E+03 Smooth wall 5 79800 -0.433244993E-13 Rough wall 6 0 0.000000000E+00 Symmetry 4 6950544 0.000000000E+00 Free outlet 3 44 0.804571614E+03 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 60 -0.804570765E+03 Smooth wall 5 79800 -0.433244993E-13 Rough wall 6 0 0.000000000E+00 Symmetry 4 6950544 0.000000000E+00 Free outlet 3 44 0.804571614E+03 Undefined 1 0 0.000000000E+00 Inlet 2 60 -0.804570765E+03 Smooth wall 5 79800 -0.433244993E-13 Rough wall 6 0 0.000000000E+00 Symmetry 4 6950544 0.000000000E+00 Free outlet 3 44 0.804571614E+03 Undefined 1 0 0.000000000E+00 Inlet 2 60 -0.804570765E+03 Smooth wall 5 79800 -0.433244993E-13 Rough wall 6 0 0.000000000E+00 Symmetry 4 6950544 0.000000000E+00 Free outlet 3 44 0.804571614E+03 Undefined 1 0 0.000000000E+00 Inlet 2 60 -0.804570765E+03 Smooth wall 5 79800 -0.433244993E-13 Rough wall 6 0 0.000000000E+00 Symmetry 4 6950544 0.000000000E+00 Free outlet 3 44 0.804571614E+03 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- --------------------------------------------------------------- --------------------------------------------------------------- --------------------------------------------------------------- --------------------------------------------------------------- --------------------------------------------------------------- Incoming flow detained for 23 outlet faces on 44 Incoming flow detained for 23 outlet faces on 44 Incoming flow detained for 23 outlet faces on 44 Incoming flow detained for 23 outlet faces on 44 Incoming flow detained for 23 outlet faces on 44 Incoming flow detained for 23 outlet faces on 44 TIME FOR THE TIME STEP 4: 0.16227E+03 =============================================================== INSTANT 0.500000000E-02 TIME STEP NUMBER 5 ============================================================= TIME FOR THE TIME STEP 4: 0.16227E+03 =============================================================== INSTANT 0.500000000E-02 TIME STEP NUMBER 5 ============================================================= TIME FOR THE TIME STEP 4: 0.16227E+03 =============================================================== INSTANT 0.500000000E-02 TIME STEP NUMBER 5 ============================================================= TIME FOR THE TIME STEP 4: 0.16227E+03 =============================================================== INSTANT 0.500000000E-02 TIME STEP NUMBER 5 ============================================================= TIME FOR THE TIME STEP 4: 0.16227E+03 =============================================================== INSTANT 0.500000000E-02 TIME STEP NUMBER 5 ============================================================= TIME FOR THE TIME STEP 4: 0.16227E+03 =============================================================== INSTANT 0.500000000E-02 TIME STEP NUMBER 5 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 60 -0.804570765E+03 Smooth wall 5 79800 -0.631600316E-14 Rough wall 6 0 0.000000000E+00 Symmetry 4 6950544 0.000000000E+00 Free outlet 3 44 0.804571334E+03 Undefined 1 0 0.000000000E+00 Inlet 2 60 -0.804570765E+03 Smooth wall 5 79800 -0.631600316E-14 Rough wall 6 0 0.000000000E+00 Symmetry 4 6950544 0.000000000E+00 Free outlet 3 44 0.804571334E+03 Undefined 1 0 0.000000000E+00 Inlet 2 60 -0.804570765E+03 Smooth wall 5 79800 -0.631600316E-14 Rough wall 6 0 0.000000000E+00 Symmetry 4 6950544 0.000000000E+00 Free outlet 3 44 0.804571334E+03 Undefined 1 0 0.000000000E+00 Inlet 2 60 -0.804570765E+03 Smooth wall 5 79800 -0.631600316E-14 Rough wall 6 0 0.000000000E+00 Symmetry 4 6950544 0.000000000E+00 Free outlet 3 44 0.804571334E+03 Undefined 1 0 0.000000000E+00 Inlet 2 60 -0.804570765E+03 Smooth wall 5 79800 -0.631600316E-14 Rough wall 6 0 0.000000000E+00 Symmetry 4 6950544 0.000000000E+00 Free outlet 3 44 0.804571334E+03 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 60 -0.804570765E+03 Smooth wall 5 79800 -0.631600316E-14 Rough wall 6 0 0.000000000E+00 Symmetry 4 6950544 0.000000000E+00 Free outlet 3 44 0.804571334E+03 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- --------------------------------------------------------------- --------------------------------------------------------------- --------------------------------------------------------------- --------------------------------------------------------------- --------------------------------------------------------------- Incoming flow detained for 22 outlet faces on 44 Incoming flow detained for 22 outlet faces on 44 Incoming flow detained for 22 outlet faces on 44 Incoming flow detained for 22 outlet faces on 44 Incoming flow detained for 22 outlet faces on 44 Incoming flow detained for 22 outlet faces on 44 TIME FOR THE TIME STEP 5: 0.15651E+03 =============================================================== INSTANT 0.600000000E-02 TIME STEP NUMBER 6 ============================================================= TIME FOR THE TIME STEP 5: 0.15651E+03 =============================================================== INSTANT 0.600000000E-02 TIME STEP NUMBER 6 ============================================================= TIME FOR THE TIME STEP 5: 0.15651E+03 =============================================================== INSTANT 0.600000000E-02 TIME STEP NUMBER 6 ============================================================= TIME FOR THE TIME STEP 5: 0.15651E+03 =============================================================== INSTANT 0.600000000E-02 TIME STEP NUMBER 6 ============================================================= TIME FOR THE TIME STEP 5: 0.15651E+03 =============================================================== INSTANT 0.600000000E-02 TIME STEP NUMBER 6 ============================================================= TIME FOR THE TIME STEP 5: 0.15651E+03 =============================================================== INSTANT 0.600000000E-02 TIME STEP NUMBER 6 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 60 -0.804570765E+03 Smooth wall 5 79800 0.130905778E-13 Rough wall 6 0 0.000000000E+00 Symmetry 4 6950544 0.000000000E+00 Free outlet 3 44 0.804571219E+03 Undefined 1 0 0.000000000E+00 Inlet 2 60 -0.804570765E+03 Smooth wall 5 79800 0.130905778E-13 Rough wall 6 0 0.000000000E+00 Symmetry 4 6950544 0.000000000E+00 Free outlet 3 44 0.804571219E+03 Undefined 1 0 0.000000000E+00 Inlet 2 60 -0.804570765E+03 Smooth wall 5 79800 0.130905778E-13 Rough wall 6 0 0.000000000E+00 Symmetry 4 6950544 0.000000000E+00 Free outlet 3 44 0.804571219E+03 Undefined 1 0 0.000000000E+00 Inlet 2 60 -0.804570765E+03 Smooth wall 5 79800 0.130905778E-13 Rough wall 6 0 0.000000000E+00 Symmetry 4 6950544 0.000000000E+00 Free outlet 3 44 0.804571219E+03 Undefined 1 0 0.000000000E+00 Inlet 2 60 -0.804570765E+03 Smooth wall 5 79800 0.130905778E-13 Rough wall 6 0 0.000000000E+00 Symmetry 4 6950544 0.000000000E+00 Free outlet 3 44 0.804571219E+03 Undefined 1 0 0.000000000E+00 Inlet 2 60 -0.804570765E+03 Smooth wall 5 79800 0.130905778E-13 Rough wall 6 0 0.000000000E+00 Symmetry 4 6950544 0.000000000E+00 Free outlet 3 44 0.804571219E+03 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- --------------------------------------------------------------- --------------------------------------------------------------- --------------------------------------------------------------- --------------------------------------------------------------- --------------------------------------------------------------- Incoming flow detained for 15 outlet faces on 44 Incoming flow detained for 15 outlet faces on 44 Incoming flow detained for 15 outlet faces on 44 Incoming flow detained for 15 outlet faces on 44 Incoming flow detained for 15 outlet faces on 44 Incoming flow detained for 15 outlet faces on 44 TIME FOR THE TIME STEP 6: 0.15734E+03 =============================================================== INSTANT 0.700000000E-02 TIME STEP NUMBER 7 ============================================================= TIME FOR THE TIME STEP 6: 0.15734E+03 =============================================================== INSTANT 0.700000000E-02 TIME STEP NUMBER 7 ============================================================= TIME FOR THE TIME STEP 6: 0.15734E+03 =============================================================== INSTANT 0.700000000E-02 TIME STEP NUMBER 7 ============================================================= TIME FOR THE TIME STEP 6: 0.15734E+03 =============================================================== INSTANT 0.700000000E-02 TIME STEP NUMBER 7 ============================================================= TIME FOR THE TIME STEP 6: 0.15734E+03 =============================================================== INSTANT 0.700000000E-02 TIME STEP NUMBER 7 ============================================================= TIME FOR THE TIME STEP 6: 0.15734E+03 =============================================================== INSTANT 0.700000000E-02 TIME STEP NUMBER 7 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 60 -0.804570765E+03 Smooth wall 5 79800 0.155361838E-12 Rough wall 6 0 0.000000000E+00 Symmetry 4 6950544 0.000000000E+00 --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 60 -0.804570765E+03 Smooth wall 5 79800 0.155361838E-12 Rough wall 6 0 0.000000000E+00 Symmetry 4 6950544 0.000000000E+00 --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 60 -0.804570765E+03 Smooth wall 5 79800 0.155361838E-12 Rough wall 6 0 0.000000000E+00 Symmetry 4 6950544 0.000000000E+00 --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 60 -0.804570765E+03 Smooth wall 5 79800 0.155361838E-12 Rough wall 6 0 0.000000000E+00 Symmetry 4 6950544 0.000000000E+00 --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 60 -0.804570765E+03 Smooth wall 5 79800 0.155361838E-12 Rough wall 6 0 0.000000000E+00 Symmetry 4 6950544 0.000000000E+00 --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 60 -0.804570765E+03 Smooth wall 5 79800 0.155361838E-12 Rough wall 6 0 0.000000000E+00 Symmetry 4 6950544 0.000000000E+00 Free outlet 3 44 0.804571190E+03 Free outlet 3 44 0.804571190E+03 Undefined 1 0 0.000000000E+00 Free outlet 3 44 0.804571190E+03 Undefined 1 0 0.000000000E+00 Free outlet 3 44 0.804571190E+03 Undefined 1 0 0.000000000E+00 Free outlet 3 44 0.804571190E+03 Undefined 1 0 0.000000000E+00 Free outlet 3 44 0.804571190E+03 Undefined 1 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- --------------------------------------------------------------- --------------------------------------------------------------- --------------------------------------------------------------- --------------------------------------------------------------- --------------------------------------------------------------- Incoming flow detained for 14 outlet faces on 44 Incoming flow detained for 14 outlet faces on 44 Incoming flow detained for 14 outlet faces on 44 Incoming flow detained for 14 outlet faces on 44 Incoming flow detained for 14 outlet faces on 44 Incoming flow detained for 14 outlet faces on 44 TIME FOR THE TIME STEP 7: 0.15543E+03 =============================================================== INSTANT 0.800000000E-02 TIME STEP NUMBER 8 ============================================================= TIME FOR THE TIME STEP 7: 0.15543E+03 =============================================================== INSTANT 0.800000000E-02 TIME STEP NUMBER 8 ============================================================= TIME FOR THE TIME STEP 7: 0.15543E+03 =============================================================== INSTANT 0.800000000E-02 TIME STEP NUMBER 8 ============================================================= TIME FOR THE TIME STEP 7: 0.15543E+03 =============================================================== INSTANT 0.800000000E-02 TIME STEP NUMBER 8 ============================================================= TIME FOR THE TIME STEP 7: 0.15543E+03 =============================================================== INSTANT 0.800000000E-02 TIME STEP NUMBER 8 ============================================================= TIME FOR THE TIME STEP 7: 0.15543E+03 =============================================================== INSTANT 0.800000000E-02 TIME STEP NUMBER 8 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 60 -0.804570765E+03 Smooth wall 5 79800 0.327725291E-12 Rough wall 6 0 0.000000000E+00 Symmetry 4 6950544 0.000000000E+00 Free outlet 3 44 0.804571113E+03 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 60 -0.804570765E+03 Smooth wall 5 79800 0.327725291E-12 Rough wall 6 0 0.000000000E+00 Symmetry 4 6950544 0.000000000E+00 Free outlet 3 44 0.804571113E+03 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 60 -0.804570765E+03 Smooth wall 5 79800 0.327725291E-12 Rough wall 6 0 0.000000000E+00 Symmetry 4 6950544 0.000000000E+00 Free outlet 3 44 0.804571113E+03 Undefined 1 0 0.000000000E+00 Inlet 2 60 -0.804570765E+03 Smooth wall 5 79800 0.327725291E-12 Rough wall 6 0 0.000000000E+00 Symmetry 4 6950544 0.000000000E+00 Free outlet 3 44 0.804571113E+03 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 60 -0.804570765E+03 Smooth wall 5 79800 0.327725291E-12 Rough wall 6 0 0.000000000E+00 Symmetry 4 6950544 0.000000000E+00 Free outlet 3 44 0.804571113E+03 Undefined 1 0 0.000000000E+00 Inlet 2 60 -0.804570765E+03 Smooth wall 5 79800 0.327725291E-12 Rough wall 6 0 0.000000000E+00 Symmetry 4 6950544 0.000000000E+00 Free outlet 3 44 0.804571113E+03 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- --------------------------------------------------------------- --------------------------------------------------------------- --------------------------------------------------------------- --------------------------------------------------------------- --------------------------------------------------------------- Incoming flow detained for 10 outlet faces on 44 Incoming flow detained for 10 outlet faces on 44 Incoming flow detained for 10 outlet faces on 44 Incoming flow detained for 10 outlet faces on 44 Incoming flow detained for 10 outlet faces on 44 Incoming flow detained for 10 outlet faces on 44 TIME FOR THE TIME STEP 8: 0.14868E+03 =============================================================== INSTANT 0.900000000E-02 TIME STEP NUMBER 9 ============================================================= TIME FOR THE TIME STEP 8: 0.14868E+03 =============================================================== INSTANT 0.900000000E-02 TIME STEP NUMBER 9 ============================================================= TIME FOR THE TIME STEP 8: 0.14868E+03 =============================================================== INSTANT 0.900000000E-02 TIME STEP NUMBER 9 ============================================================= TIME FOR THE TIME STEP 8: 0.14868E+03 =============================================================== INSTANT 0.900000000E-02 TIME STEP NUMBER 9 ============================================================= TIME FOR THE TIME STEP 8: 0.14868E+03 =============================================================== INSTANT 0.900000000E-02 TIME STEP NUMBER 9 ============================================================= TIME FOR THE TIME STEP 8: 0.14868E+03 =============================================================== INSTANT 0.900000000E-02 TIME STEP NUMBER 9 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 60 -0.804570765E+03 Smooth wall 5 79800 0.552782014E-12 Rough wall 6 0 0.000000000E+00 Symmetry 4 6950544 0.000000000E+00 Free outlet 3 44 0.804570469E+03 Undefined 1 0 0.000000000E+00 Inlet 2 60 -0.804570765E+03 Smooth wall 5 79800 0.552782014E-12 Rough wall 6 0 0.000000000E+00 Symmetry 4 6950544 0.000000000E+00 Free outlet 3 44 0.804570469E+03 Undefined 1 0 0.000000000E+00 Inlet 2 60 -0.804570765E+03 Smooth wall 5 79800 0.552782014E-12 Rough wall 6 0 0.000000000E+00 Symmetry 4 6950544 0.000000000E+00 Free outlet 3 44 0.804570469E+03 Undefined 1 0 0.000000000E+00 Inlet 2 60 -0.804570765E+03 Smooth wall 5 79800 0.552782014E-12 Rough wall 6 0 0.000000000E+00 Symmetry 4 6950544 0.000000000E+00 Free outlet 3 44 0.804570469E+03 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 60 -0.804570765E+03 Smooth wall 5 79800 0.552782014E-12 Rough wall 6 0 0.000000000E+00 Symmetry 4 6950544 0.000000000E+00 Free outlet 3 44 0.804570469E+03 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 60 -0.804570765E+03 Smooth wall 5 79800 0.552782014E-12 Rough wall 6 0 0.000000000E+00 Symmetry 4 6950544 0.000000000E+00 Free outlet 3 44 0.804570469E+03 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- --------------------------------------------------------------- --------------------------------------------------------------- --------------------------------------------------------------- --------------------------------------------------------------- --------------------------------------------------------------- Incoming flow detained for 10 outlet faces on 44 Incoming flow detained for 10 outlet faces on 44 Incoming flow detained for 10 outlet faces on 44 Incoming flow detained for 10 outlet faces on 44 Incoming flow detained for 10 outlet faces on 44 Incoming flow detained for 10 outlet faces on 44 TIME FOR THE TIME STEP 9: 0.14660E+03 =============================================================== INSTANT 0.100000000E-01 TIME STEP NUMBER 10 ============================================================= TIME FOR THE TIME STEP 9: 0.14660E+03 =============================================================== INSTANT 0.100000000E-01 TIME STEP NUMBER 10 ============================================================= TIME FOR THE TIME STEP 9: 0.14660E+03 =============================================================== INSTANT 0.100000000E-01 TIME STEP NUMBER 10 ============================================================= TIME FOR THE TIME STEP 9: 0.14660E+03 =============================================================== INSTANT 0.100000000E-01 TIME STEP NUMBER 10 ============================================================= TIME FOR THE TIME STEP 9: 0.14660E+03 =============================================================== INSTANT 0.100000000E-01 TIME STEP NUMBER 10 ============================================================= TIME FOR THE TIME STEP 9: 0.14660E+03 =============================================================== INSTANT 0.100000000E-01 TIME STEP NUMBER 10 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 60 -0.804570765E+03 Smooth wall 5 79800 0.191171726E-12 Rough wall 6 0 0.000000000E+00 Symmetry 4 6950544 0.000000000E+00 Free outlet 3 44 0.804570456E+03 Undefined 1 0 0.000000000E+00 Inlet 2 60 -0.804570765E+03 Smooth wall 5 79800 0.191171726E-12 Rough wall 6 0 0.000000000E+00 Symmetry 4 6950544 0.000000000E+00 Free outlet 3 44 0.804570456E+03 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 60 -0.804570765E+03 Smooth wall 5 79800 0.191171726E-12 Rough wall 6 0 0.000000000E+00 Symmetry 4 6950544 0.000000000E+00 Free outlet 3 44 0.804570456E+03 Undefined 1 0 0.000000000E+00 Inlet 2 60 -0.804570765E+03 Smooth wall 5 79800 0.191171726E-12 Rough wall 6 0 0.000000000E+00 Symmetry 4 6950544 0.000000000E+00 Free outlet 3 44 0.804570456E+03 Undefined 1 0 0.000000000E+00 Inlet 2 60 -0.804570765E+03 Smooth wall 5 79800 0.191171726E-12 Rough wall 6 0 0.000000000E+00 Symmetry 4 6950544 0.000000000E+00 Free outlet 3 44 0.804570456E+03 Undefined 1 0 0.000000000E+00 Inlet 2 60 -0.804570765E+03 Smooth wall 5 79800 0.191171726E-12 Rough wall 6 0 0.000000000E+00 Symmetry 4 6950544 0.000000000E+00 Free outlet 3 44 0.804570456E+03 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- --------------------------------------------------------------- --------------------------------------------------------------- --------------------------------------------------------------- --------------------------------------------------------------- --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.41863E-05 0.51475E+01 Friction velocity uet : 0.34745E-06 0.27635E+00 Friction velocity uk : 0.35030E-05 0.18521E+01 Dimensionless distance yplus : 0.54475E-03 0.21367E+05 Friction thermal sca. tstar : -0.22316E+06 0.00000E+00 Rough dim-less th. sca. tplus : 0.40788E-01 0.10843E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 0 Total number of wall faces : 79800 ------------------------------------------------------------ ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.41863E-05 0.51475E+01 Friction velocity uet : 0.34745E-06 0.27635E+00 Friction velocity uk : 0.35030E-05 0.18521E+01 Dimensionless distance yplus : 0.54475E-03 0.21367E+05 Friction thermal sca. tstar : -0.22316E+06 0.00000E+00 Rough dim-less th. sca. tplus : 0.40788E-01 0.10843E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 0 Total number of wall faces : 79800 ------------------------------------------------------------ ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.41863E-05 0.51475E+01 Friction velocity uet : 0.34745E-06 0.27635E+00 Friction velocity uk : 0.35030E-05 0.18521E+01 Dimensionless distance yplus : 0.54475E-03 0.21367E+05 Friction thermal sca. tstar : -0.22316E+06 0.00000E+00 Rough dim-less th. sca. tplus : 0.40788E-01 0.10843E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 0 Total number of wall faces : 79800 ------------------------------------------------------------ ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.41863E-05 0.51475E+01 Friction velocity uet : 0.34745E-06 0.27635E+00 Friction velocity uk : 0.35030E-05 0.18521E+01 Dimensionless distance yplus : 0.54475E-03 0.21367E+05 Friction thermal sca. tstar : -0.22316E+06 0.00000E+00 Rough dim-less th. sca. tplus : 0.40788E-01 0.10843E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 0 Total number of wall faces : 79800 ------------------------------------------------------------ ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.41863E-05 0.51475E+01 Friction velocity uet : 0.34745E-06 0.27635E+00 Friction velocity uk : 0.35030E-05 0.18521E+01 Dimensionless distance yplus : 0.54475E-03 0.21367E+05 Friction thermal sca. tstar : -0.22316E+06 0.00000E+00 Rough dim-less th. sca. tplus : 0.40788E-01 0.10843E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 0 Total number of wall faces : 79800 ------------------------------------------------------------ ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.41863E-05 0.51475E+01 Friction velocity uet : 0.34745E-06 0.27635E+00 Friction velocity uk : 0.35030E-05 0.18521E+01 Dimensionless distance yplus : 0.54475E-03 0.21367E+05 Friction thermal sca. tstar : -0.22316E+06 0.00000E+00 Rough dim-less th. sca. tplus : 0.40788E-01 0.10843E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 0 Total number of wall faces : 79800 ------------------------------------------------------------ Incoming flow detained for 10 outlet faces on 44 Incoming flow detained for 10 outlet faces on 44 Incoming flow detained for 10 outlet faces on 44 Incoming flow detained for 10 outlet faces on 44 Incoming flow detained for 10 outlet faces on 44 Incoming flow detained for 10 outlet faces on 44 Write final restart files checkpoint at iteration 10, Physical time 0.10000E-01 Write final restart files checkpoint at iteration 10, Physical time 0.10000E-01 ** Writing the main restart file ----------------------------- Write final restart files checkpoint at iteration 10, Physical time 0.10000E-01 ** Writing the main restart file ----------------------------- Write final restart files checkpoint at iteration 10, Physical time 0.10000E-01 ** Writing the main restart file ----------------------------- ** Writing the main restart file ----------------------------- Write final restart files checkpoint at iteration 10, Physical time 0.10000E-01 ** Writing the main restart file ----------------------------- Write final restart files checkpoint at iteration 10, Physical time 0.10000E-01 ** Writing the main restart file ----------------------------- Start writing End writing the dimensions End writing the options Start writing End writing the dimensions End writing the options Start writing End writing the dimensions End writing the options Start writing End writing the dimensions End writing the options Start writing End writing the dimensions End writing the options Start writing End writing the dimensions End writing the options End writing the main variables End writing the main variables End writing the main variables End writing the main variables End writing the main variables End writing the main variables End writing ** Writing the auxilliary restart file ----------------------------------- End writing ** Writing the auxilliary restart file ----------------------------------- End writing ** Writing the auxilliary restart file ----------------------------------- End writing ** Writing the auxilliary restart file ----------------------------------- End writing ** Writing the auxilliary restart file ----------------------------------- End writing ** Writing the auxilliary restart file ----------------------------------- Start writing Start writing End writing the dimensions and options Start writing End writing the dimensions and options Start writing End writing the dimensions and options Start writing End writing the dimensions and options Start writing End writing the dimensions and options End writing the dimensions and options End writing the physical properties End writing the physical properties End writing the physical properties End writing the physical properties End writing the physical properties End writing the physical properties End writing the time step End writing the time step End writing the time step End writing the time step End writing the time step End writing the time step End writing the mass fluxes End writing the mass fluxes End writing the mass fluxes End writing the mass fluxes End writing the mass fluxes End writing the mass fluxes End writing the boundary conditions End writing the boundary conditions End writing the boundary conditions End writing the boundary conditions End writing the boundary conditions End writing the boundary conditions End writing Time for restart files: 0.51746E+01 End writing Time for restart files: 0.51747E+01 End writing Time for restart files: 0.51744E+01 End writing Time for restart files: 0.51743E+01 End writing Time for restart files: 0.51747E+01 End writing Time for restart files: 0.51748E+01 ** INFORMATION ON CONVERGENCE -------------------------- --------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual derive --------------------------------------------------------------- --------------------------------------------------------------- ** INFORMATION ON VARIABLES ------------------------ --------------------------------------------------------------- Variable Min. value Max. value Min clip Max clip --------------------------------------------------------------- v Density 0.99765E+03 0.99873E+03 0 0 v LamVisc 0.55204E-03 0.57160E-03 0 0 v SpecHeat 0.42981E+04 0.43000E+04 0 0 v ThermalCond 0.63077E+03 0.63319E+03 0 0 --------------------------------------------------------------- ** INFORMATION ON CLIPPINGS ------------------------ --------------------------------------------------------------- Variable Min wo clips Max wo clips Min clip Max clip --------------------------------------------------------------- --------------------------------------------------------------- ** INFORMATION ON THE TIME STEP ----------------------------- --------------------------------------------------------------- Criterion Value at xc yc zc --------------------------------------------------------------- Courant min 0.11610E-03 -0.41746E+00 -0.37766E+01 0.50000E+00 Courant max 0.10000E+01 0.36038E+01 -0.24308E+00 0.50000E+00 Fourier min 0.30367E-04 0.69524E+00 -0.31180E+01 0.50000E+00 Fourier max 0.39211E+02 -0.21702E+01 0.24132E+01 0.50000E+00 Cou_Fou min 0.66299E-03 0.50351E+00 0.36856E+01 0.50000E+00 Cou_Fou max 0.39287E+02 -0.21702E+01 0.24132E+01 0.50000E+00 --------------------------------------------------------------- Dt min 0.10000E-03 0.29399E+01 0.13191E+01 0.50000E+00 Dt max 0.19020E-02 0.11434E+01 -0.40374E+01 0.50000E+00 --------------------------------------------------------------- TIME FOR THE TIME STEP 10: 0.15632E+03 =============================================================== =============================================================== FINAL STAGE OF THE CALCULATION ============================== =========================================================== ** INFORMATION ON CONVERGENCE -------------------------- --------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual derive --------------------------------------------------------------- --------------------------------------------------------------- ** INFORMATION ON VARIABLES ------------------------ --------------------------------------------------------------- Variable Min. value Max. value Min clip Max clip --------------------------------------------------------------- v Density 0.99765E+03 0.99873E+03 0 0 v LamVisc 0.55204E-03 0.57160E-03 0 0 v SpecHeat 0.42981E+04 0.43000E+04 0 0 v ThermalCond 0.63077E+03 0.63319E+03 0 0 --------------------------------------------------------------- ** INFORMATION ON CLIPPINGS ------------------------ --------------------------------------------------------------- Variable Min wo clips Max wo clips Min clip Max clip --------------------------------------------------------------- --------------------------------------------------------------- ** INFORMATION ON THE TIME STEP ----------------------------- --------------------------------------------------------------- Criterion Value at xc yc zc --------------------------------------------------------------- Courant min 0.11610E-03 -0.41746E+00 -0.37766E+01 0.50000E+00 Courant max 0.10000E+01 0.36038E+01 -0.24308E+00 0.50000E+00 Fourier min 0.30367E-04 0.69524E+00 -0.31180E+01 0.50000E+00 Fourier max 0.39211E+02 -0.21702E+01 0.24132E+01 0.50000E+00 Cou_Fou min 0.66299E-03 0.50351E+00 0.36856E+01 0.50000E+00 Cou_Fou max 0.39287E+02 -0.21702E+01 0.24132E+01 0.50000E+00 --------------------------------------------------------------- Dt min 0.10000E-03 0.29399E+01 0.13191E+01 0.50000E+00 Dt max 0.19020E-02 0.11434E+01 -0.40374E+01 0.50000E+00 --------------------------------------------------------------- TIME FOR THE TIME STEP 10: 0.15632E+03 =============================================================== =============================================================== FINAL STAGE OF THE CALCULATION ============================== =========================================================== ** INFORMATION ON CONVERGENCE -------------------------- --------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual derive --------------------------------------------------------------- --------------------------------------------------------------- ** INFORMATION ON VARIABLES ------------------------ --------------------------------------------------------------- Variable Min. value Max. value Min clip Max clip --------------------------------------------------------------- v Density 0.99765E+03 0.99873E+03 0 0 v LamVisc 0.55204E-03 0.57160E-03 0 0 v SpecHeat 0.42981E+04 0.43000E+04 0 0 v ThermalCond 0.63077E+03 0.63319E+03 0 0 --------------------------------------------------------------- ** INFORMATION ON CLIPPINGS ------------------------ --------------------------------------------------------------- Variable Min wo clips Max wo clips Min clip Max clip --------------------------------------------------------------- --------------------------------------------------------------- ** INFORMATION ON THE TIME STEP ----------------------------- --------------------------------------------------------------- Criterion Value at xc yc zc --------------------------------------------------------------- Courant min 0.11610E-03 -0.41746E+00 -0.37766E+01 0.50000E+00 Courant max 0.10000E+01 0.36038E+01 -0.24308E+00 0.50000E+00 Fourier min 0.30367E-04 0.69524E+00 -0.31180E+01 0.50000E+00 Fourier max 0.39211E+02 -0.21702E+01 0.24132E+01 0.50000E+00 Cou_Fou min 0.66299E-03 0.50351E+00 0.36856E+01 0.50000E+00 Cou_Fou max 0.39287E+02 -0.21702E+01 0.24132E+01 0.50000E+00 --------------------------------------------------------------- Dt min 0.10000E-03 0.29399E+01 0.13191E+01 0.50000E+00 Dt max 0.19020E-02 0.11434E+01 -0.40374E+01 0.50000E+00 --------------------------------------------------------------- TIME FOR THE TIME STEP 10: 0.15632E+03 =============================================================== =============================================================== FINAL STAGE OF THE CALCULATION ============================== =========================================================== ** INFORMATION ON CONVERGENCE -------------------------- --------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual derive --------------------------------------------------------------- --------------------------------------------------------------- ** INFORMATION ON VARIABLES ------------------------ --------------------------------------------------------------- Variable Min. value Max. value Min clip Max clip --------------------------------------------------------------- v Density 0.99765E+03 0.99873E+03 0 0 v LamVisc 0.55204E-03 0.57160E-03 0 0 v SpecHeat 0.42981E+04 0.43000E+04 0 0 v ThermalCond 0.63077E+03 0.63319E+03 0 0 --------------------------------------------------------------- ** INFORMATION ON CLIPPINGS ------------------------ --------------------------------------------------------------- Variable Min wo clips Max wo clips Min clip Max clip --------------------------------------------------------------- --------------------------------------------------------------- ** INFORMATION ON THE TIME STEP ----------------------------- --------------------------------------------------------------- Criterion Value at xc yc zc --------------------------------------------------------------- Courant min 0.11610E-03 -0.41746E+00 -0.37766E+01 0.50000E+00 Courant max 0.10000E+01 0.36038E+01 -0.24308E+00 0.50000E+00 Fourier min 0.30367E-04 0.69524E+00 -0.31180E+01 0.50000E+00 Fourier max 0.39211E+02 -0.21702E+01 0.24132E+01 0.50000E+00 Cou_Fou min 0.66299E-03 0.50351E+00 0.36856E+01 0.50000E+00 Cou_Fou max 0.39287E+02 -0.21702E+01 0.24132E+01 0.50000E+00 --------------------------------------------------------------- Dt min 0.10000E-03 0.29399E+01 0.13191E+01 0.50000E+00 Dt max 0.19020E-02 0.11434E+01 -0.40374E+01 0.50000E+00 --------------------------------------------------------------- TIME FOR THE TIME STEP 10: 0.15632E+03 =============================================================== =============================================================== FINAL STAGE OF THE CALCULATION ============================== =========================================================== ** INFORMATION ON CONVERGENCE -------------------------- --------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual derive --------------------------------------------------------------- --------------------------------------------------------------- ** INFORMATION ON VARIABLES ------------------------ --------------------------------------------------------------- Variable Min. value Max. value Min clip Max clip --------------------------------------------------------------- v Density 0.99765E+03 0.99873E+03 0 0 v LamVisc 0.55204E-03 0.57160E-03 0 0 v SpecHeat 0.42981E+04 0.43000E+04 0 0 v ThermalCond 0.63077E+03 0.63319E+03 0 0 --------------------------------------------------------------- ** INFORMATION ON CLIPPINGS ------------------------ --------------------------------------------------------------- Variable Min wo clips Max wo clips Min clip Max clip --------------------------------------------------------------- --------------------------------------------------------------- ** INFORMATION ON THE TIME STEP ----------------------------- --------------------------------------------------------------- Criterion Value at xc yc zc --------------------------------------------------------------- Courant min 0.11610E-03 -0.41746E+00 -0.37766E+01 0.50000E+00 Courant max 0.10000E+01 0.36038E+01 -0.24308E+00 0.50000E+00 Fourier min 0.30367E-04 0.69524E+00 -0.31180E+01 0.50000E+00 Fourier max 0.39211E+02 -0.21702E+01 0.24132E+01 0.50000E+00 Cou_Fou min 0.66299E-03 0.50351E+00 0.36856E+01 0.50000E+00 Cou_Fou max 0.39287E+02 -0.21702E+01 0.24132E+01 0.50000E+00 --------------------------------------------------------------- Dt min 0.10000E-03 0.29399E+01 0.13191E+01 0.50000E+00 Dt max 0.19020E-02 0.11434E+01 -0.40374E+01 0.50000E+00 --------------------------------------------------------------- TIME FOR THE TIME STEP 10: 0.15632E+03 =============================================================== =============================================================== FINAL STAGE OF THE CALCULATION ============================== =========================================================== ** INFORMATION ON CONVERGENCE -------------------------- --------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual derive --------------------------------------------------------------- --------------------------------------------------------------- ** INFORMATION ON VARIABLES ------------------------ --------------------------------------------------------------- Variable Min. value Max. value Min clip Max clip --------------------------------------------------------------- v Density 0.99765E+03 0.99873E+03 0 0 v LamVisc 0.55204E-03 0.57160E-03 0 0 v SpecHeat 0.42981E+04 0.43000E+04 0 0 v ThermalCond 0.63077E+03 0.63319E+03 0 0 --------------------------------------------------------------- ** INFORMATION ON CLIPPINGS ------------------------ --------------------------------------------------------------- Variable Min wo clips Max wo clips Min clip Max clip --------------------------------------------------------------- --------------------------------------------------------------- ** INFORMATION ON THE TIME STEP ----------------------------- --------------------------------------------------------------- Criterion Value at xc yc zc --------------------------------------------------------------- Courant min 0.11610E-03 -0.41746E+00 -0.37766E+01 0.50000E+00 Courant max 0.10000E+01 0.36038E+01 -0.24308E+00 0.50000E+00 Fourier min 0.30367E-04 0.69524E+00 -0.31180E+01 0.50000E+00 Fourier max 0.39211E+02 -0.21702E+01 0.24132E+01 0.50000E+00 Cou_Fou min 0.66299E-03 0.50351E+00 0.36856E+01 0.50000E+00 Cou_Fou max 0.39287E+02 -0.21702E+01 0.24132E+01 0.50000E+00 --------------------------------------------------------------- Dt min 0.10000E-03 0.29399E+01 0.13191E+01 0.50000E+00 Dt max 0.19020E-02 0.11434E+01 -0.40374E+01 0.50000E+00 --------------------------------------------------------------- TIME FOR THE TIME STEP 10: 0.15632E+03 =============================================================== =============================================================== FINAL STAGE OF THE CALCULATION ============================== =========================================================== ** TIME FOR FINAL WRITING: 0.45916E-02 ----------------------- ** TIME FOR FINAL WRITING: 0.51309E-02 ----------------------- ** TIME FOR FINAL WRITING: 0.59252E-02 ----------------------- ** TIME FOR FINAL WRITING: 0.60709E-02 ----------------------- ** TIME FOR FINAL WRITING: 0.66084E-02 ----------------------- ** TIME FOR FINAL WRITING: 0.65264E-02 ----------------------- =========================================================== END OF CALCULATION ================== =============================================================== Destroying structures and ending computation Time elapsed defining values using MEI: 20.66565 =========================================================== END OF CALCULATION ================== =============================================================== Destroying structures and ending computation Time elapsed defining values using MEI: 20.66565 =========================================================== END OF CALCULATION ================== =============================================================== Destroying structures and ending computation Time elapsed defining values using MEI: 20.66565 =========================================================== END OF CALCULATION ================== =============================================================== Destroying structures and ending computation Time elapsed defining values using MEI: 20.66565 =========================================================== END OF CALCULATION ================== =============================================================== Destroying structures and ending computation Time elapsed defining values using MEI: 20.66565 =========================================================== END OF CALCULATION ================== =============================================================== Destroying structures and ending computation Time elapsed defining values using MEI: 20.66565 Calculation time summary: User CPU time: 2901.195 s System CPU time: 34.100 s Elapsed time: 2957.306 s CPU / elapsed time 0.993 Memory use summary: Total memory used: 2.052 GiB Theoretical instrumented dynamic memory: 677.383 MiB Calculation time summary: User CPU time: 2901.669 s System CPU time: 34.769 s Elapsed time: 2957.306 s CPU / elapsed time 0.993 Memory use summary: Total memory used: 2.080 GiB Theoretical instrumented dynamic memory: 690.515 MiB Calculation time summary: User CPU time: 2904.390 s System CPU time: 33.408 s Elapsed time: 2957.306 s CPU / elapsed time 0.993 Memory use summary: Total memory used: 2.062 GiB Theoretical instrumented dynamic memory: 680.649 MiB Calculation time summary: User CPU time: 2907.665 s System CPU time: 33.500 s Elapsed time: 2957.306 s CPU / elapsed time 0.995 Memory use summary: Total memory used: 2.061 GiB Theoretical instrumented dynamic memory: 680.574 MiB Calculation time summary: User CPU time: 2902.452 s System CPU time: 33.438 s Elapsed time: 2957.306 s CPU / elapsed time 0.993 Memory use summary: Total memory used: 2.069 GiB Theoretical instrumented dynamic memory: 685.604 MiB Calculation time summary: User CPU time: 2902.454 s System CPU time: 34.944 s Total CPU time: 17623.983 s Elapsed time: 2957.306 s CPU / elapsed time 0.993 Memory use summary: Total memory used: 12.395 GiB local minimum: 2.052 GiB (rank 4) local maximum: 2.080 GiB (rank 5) Theoretical instrumented dynamic memory: 4.001 GiB local minimum: 677.383 MiB (rank 4) local maximum: 690.515 MiB (rank 5) **************************** Saving calculation results **************************** ---------------------------------------- Begin PBS Epilogue Wed Oct 16 20:05:45 EDT 2013 1381968345 Job ID: 1706649.egeon2 Username: mehdizde Group: etienne Job Name: nameandcase Session: 22976 Limits: neednodes=1:ppn=6,nodes=1:ppn=6,walltime=06:10:00 Resources: cput=04:54:08,mem=10893348kb,vmem=13158512kb,walltime=00:49:52 Queue: courte Account: Nodes: node-c3-47 Killing leftovers... End PBS Epilogue Wed Oct 16 20:05:45 EDT 2013 1381968345 ----------------------------------------