Code_Saturne is running *********************** Version: 3.3 Path: /usr/local Result directory: /home/randd/Desktop/Secundario/STUSBDMS/CSBDM6/RESU/20141201-1320 Parallel Code_Saturne on 8 processes. **************************** Preparing calculation data **************************** *************************** Preprocessing calculation *************************** ********************** Starting calculation ********************** command: /usr/local/libexec/code_saturne/cs_solver --param RUN.XML --log 0 --mpi *************************************************************** (R) Code_Saturne Version 3.3.2 Copyright (C) 1998-2014 EDF S.A., France build Mon 29 Sep 2014 11:20:53 AM CEST MPI version 2.1 (Open MPI 1.4.3) The Code_Saturne CFD tool is free software; you can redistribute it and/or modify it under the terms of the GNU General Public License as published by the Free Software Foundation; either version 2 of the License, or (at your option) any later version. The Code_Saturne CFD tool is distributed in the hope that it will be useful, but WITHOUT ANY WARRANTY; without even the implied warranty of MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU General Public License for more details. *************************************************************** Local case configuration: Date: Mon 01 Dec 2014 01:20:27 PM CET System: Linux 3.2.0-70-generic Machine: Workstation Processor: model name : Intel(R) Xeon(R) CPU E5620 @ 2.40GHz Memory: 24095 MB User: randd (randd) Directory: /home/randd/Desktop/Secundario/STUSBDMS/CSBDM6/RESU/20141201-1320 MPI ranks: 8 (appnum attribute: 0) I/O read method: collective MPI-IO (explicit offsets) I/O write method: collective MPI-IO (explicit offsets) I/O rank step: 1 Reading metadata from file: "mesh_input" =============================================================== CALCULATION PREPARATION ======================= =========================================================== No error detected during the data verification cs_user_parameters.f90 and others). =========================================================== CALCULATION PARAMETERS SUMMARY ============================== ----------------------------------------------------------- ** DIMENSIONS ---------- --- Physics NVAR = 6 (Nb variables ) NSCAL = 0 (Nb scalars ) NSCAUS = 0 (Nb user scalars ) NSCAPP = 0 (Nb specific physics scalars ) NPROCE = 6 (Nb cell properties ) ----------------------------------------------------------- ** PHYSICAL PROPERTIES ------------------- GX = 0.00000E+00 (Gravity x component ) GY = 0.00000E+00 (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 = 0.40500E+00 (Reference density ) VISCL0 = 0.36510E-04 (Ref. molecular dyn. visc. ) CP0 = 0.13130E+04 (Ref. specific heat ) ICP = 0 (> 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 = 0 (Density constant(0) or not(1) IVIVAR = 0 (Molec. visc cst.(0) or not(1) Initial reference point for pressure XYZP0 = 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------- ** HOMOGENEOUS MIXTURE MODEL FOR CAVITATION ---------------------------------------- ICAVIT = -1 (-1: single phase flow ) ( 0: no vap./cond. model ) ( 1: Merkle's model ) ----------------------------------------------------------- ** THERMAL MODEL ------------- --- Continuous phase: - Commons ITHERM = 0 (0: no thermal model ) (10: temperature C ) (11: temperature K ) (20: enthalpy ) (30: total energy ) ISCALT = -1 (Thermal scalar number ) ** TURBULENCE ---------- --- Continuous phase: - Commons ITURB = 21 (Turbulence model ) IDEUCH = 1 (0: one-scale model ) (1: two-scale model ) (2: invariant wall function ) IWALLT = 0 (Exch. coeff. correlation ) (0: not activated ) (1: activated ) YPLULI = 0.23810E+01 (Limit Y+ ) ILOGPO = 1 (0: power law (forbidden for k-epsilon) ) (1: one-scale log law ) IGRHOK = 0 (1: computed Grad(rho k) ) - Linear production k-epsilon (ITURB = 21) ALMAX = -0.99900E+03 (Characteristic length ) UREF = 0.10000E+01 (Characteristic velocity ) ICLKEP = 0 (k-epsilon clipping model ) IKECOU = 0 (k-epsilon coupling mode ) IGRAKE = 1 (Account for gravity ) RELAXV = 0.10000E+01 for k (Relaxation) RELAXV = 0.10000E+01 for epsilon (Relaxation) - 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)) - Linear production k-epsilon (ITURB = 21) 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 = 0.25000E-02 (Minimum time step ) DTMAX = 0.50000E+02 (Maximum time step ) DTREF = 0.50000E-01 (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 ------------------------------------ Velocity 1 0.1000E+01 Pressure 0 0.1000E+01 k 1 0.1000E+01 epsilon 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 --------------------------------------------------------------------- Velocity 1 1 1 1 0 0.10E+01 0.10E+01 Pressure 0 1 1 1 0 0.00E+00 0.10E+01 k 1 1 1 1 0 0.00E+00 0.10E+01 epsilon 1 1 1 1 0 0.00E+00 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 ------ IDILAT = 1 (1 : without unsteady term in the continuity equation 2 : with unsteady term in the continuity equation) IPOROS = 0 (0 : without porous media 1 : with porous media) 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 ) 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 = 3 (Reconstruction mode ) ANOMAX = 0.78540E+00 (Non-ortho angle: limit for ) (least squares ext. neighbors) ------------------------------------------------------------------- Variable NSWRGR NSWRSM EPSRGR EPSRSM EXTRAG ------------------------------------------------------------------- Velocity 100 1 0.1000E-04 0.1000E-03 0.0000E+00 Pressure 100 2 0.1000E-04 0.1000E-03 0.0000E+00 k 100 1 0.1000E-04 0.1000E-03 0.0000E+00 epsilon 100 1 0.1000E-04 0.1000E-03 0.0000E+00 ----------------------------------------------------------- ------------------------------------------- Variable IRCFLU IMLIGR CLIMGR ------------------------------------------- Velocity 1 1 0.1500E+01 Pressure 1 1 0.1500E+01 k 1 1 0.1500E+01 epsilon 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 ) ----------------------------------------------------------- ** BASE ITERATIVE SOLVERS ---------------------- -------------------------------------------------- Variable IRESOL NITMAX EPSILO IDIRCL -------------------------------------------------- Velocity -1 10000 0.1000E-04 1 Pressure 0 10000 0.1000E-04 1 k -1 10000 0.1000E-04 1 epsilon -1 10000 0.1000E-04 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 -------------------------------------- Velocity 0 100 10 Pressure 1 100 10 k 0 100 10 epsilon 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 ----------------------------------------------------------- ** 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 = 400 (Final time step required ) --- CPU time margin TMARUS = -0.10000E+01 (CPU time margin before stop ) ----------------------------------------------------------- ** INPUT-OUTPUT ------------ --- Restart file NTSUIT = 0 (Checkpoint frequency ) --- Post-processed variables Number Name Velocity Pressure k epsilon turbulent_viscosity CourantNb FourierNb total_pressure Local Time Step -- -- --- 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 Velocity[X] -1 3 Velocity[Y] -1 4 Velocity[Z] -1 5 Pressure -1 6 k -1 7 epsilon -1 8 Density -1 9 LamVisc -1 10 turbulent_viscos -1 11 CourantNb -1 12 FourierNb -1 13 total_pressure -1 14 Local Time Step -1 -- -- -- --- Log files NTLIST = 10 (Output frequency ) Number Name IWARNI verbosity level (-999: not applicable) 2 Velocity 0 5 Pressure 0 6 k 0 7 epsilon 0 10 turbulent_viscos -999 11 CourantNb -999 12 FourierNb -999 13 total_pressure -999 14 Local Time Step -999 -- -- -- --- Additional post-processing variables (ipstdv) ipstfo = 1 (Force exerted at boundary) ipstyp = 1 (Yplus at boundary) ipstft = 1 (Thermal flow at boundary) ipsttb = 0 (Temperature at boundary) ipstnu = 0 (Nusselt at boundary) ----------------------------------------------------------- ** ALE METHOD (MOVING MESH) ----------- IALE = 0 (1: activated ) NALINF = 0 (Fluid initialization iterations) ----------------------------------------------------------- Postprocessing output writers: ------------------------------ -1: name: results directory: postprocessing format: EnSight Gold options: binary time dependency: fixed mesh output: every 10 time steps and at calculation end Reading file: mesh_input Finished reading: mesh_input No "partition_input/domain_number_8" file available; ---------------------------------------------------------- Partitioning by space-filling curve: Morton (in bounding box). Number of cells per domain (histogramm): [ 38352 ; 38353 ] = 8 Writing file: partition_output/domain_number_8 Finished writing: partition_output/domain_number_8 Partitioning finished (2.43 s) ---------------------------------------------------------- Halo construction with extended neighborhood ============================================ Face interfaces creation Vertex interfaces creation Halo creation Halo definition Local halo definition Distant halo creation Updating the faces -> cells connectivity Extended neighborhood structures definition Histogram of the number of cells per rank: minimum value = 38352 maximum value = 38353 1 : [ 38352 ; 38353 ] = 8 ---------------------------------------------------------- Histogram of the number of standard + halo cells per rank: minimum value = 38906 maximum value = 45404 1 : [ 38906 ; 40205 [ = 2 2 : [ 40205 ; 41505 [ = 1 3 : [ 41505 ; 42804 [ = 2 4 : [ 42804 ; 44104 [ = 2 5 : [ 44104 ; 45404 ] = 1 ---------------------------------------------------------- Histogram of the number of ghost cells per rank: minimum value = 554 maximum value = 7052 1 : [ 554 ; 1853 [ = 2 2 : [ 1853 ; 3153 [ = 1 3 : [ 3153 ; 4452 [ = 2 4 : [ 4452 ; 5752 [ = 2 5 : [ 5752 ; 7052 ] = 1 Histogram of the number of ghost cells in the standard neighborhood per rank: minimum value = 248 maximum value = 2576 1 : [ 248 ; 713 [ = 2 2 : [ 713 ; 1179 [ = 1 3 : [ 1179 ; 1644 [ = 3 4 : [ 1644 ; 2110 [ = 1 5 : [ 2110 ; 2576 ] = 1 ---------------------------------------------------------- Histogram of the number of interior faces per rank: minimum value = 70183 maximum value = 73324 1 : [ 70183 ; 70811 [ = 1 2 : [ 70811 ; 71439 [ = 3 3 : [ 71439 ; 72067 [ = 2 4 : [ 72067 ; 72695 [ = 0 5 : [ 72695 ; 73324 ] = 2 ---------------------------------------------------------- Histogram of the number of boundary faces per rank: minimum value = 11379 maximum value = 13375 1 : [ 11379 ; 11778 [ = 1 2 : [ 11778 ; 12177 [ = 2 3 : [ 12177 ; 12576 [ = 3 4 : [ 12576 ; 12975 [ = 0 5 : [ 12975 ; 13375 ] = 2 ---------------------------------------------------------- Histogram of the number of interior faces per cell: minimum value = 3 maximum value = 5 1 : [ 3 ; 4 [ = 97128 2 : [ 4 ; 5 ] = 209693 ---------------------------------------------------------- Histogram of the number of neighboring domains per rank: minimum value = 1 maximum value = 4 1 : [ 1 ; 2 [ = 2 2 : [ 2 ; 3 [ = 3 3 : [ 3 ; 4 ] = 3 ---------------------------------------------------------- Global definition of the number of elements (cells, vertices, faces...) Synchronizing cell families Renumbering mesh: Checking mesh renumbering for threads: ------------------------------------- Histogram of volume mesh matrix bandwidth per rank: minimum value = 38252 maximum value = 43243 1 : [ 38252 ; 39250 [ = 2 2 : [ 39250 ; 40248 [ = 2 3 : [ 40248 ; 41246 [ = 2 4 : [ 41246 ; 42244 [ = 1 5 : [ 42244 ; 43243 ] = 1 Histogram of volume mesh matrix profile/lines per rank: minimum value = 16867 maximum value = 20405 1 : [ 16867 ; 17574 [ = 2 2 : [ 17574 ; 18282 [ = 0 3 : [ 18282 ; 18989 [ = 0 4 : [ 18989 ; 19697 [ = 1 5 : [ 19697 ; 20405 ] = 5 Mesh coordinates: minimum and maximum X : -2.5000000e-01 8.3112348e+00 Y : 6.6467695e+00 1.6180000e+01 Z : 9.3600000e+00 1.2676000e+01 Mesh Number of cells: 306821 Number of interior faces: 568098 Number of boundary faces: 99538 Number of vertices: 81864 Groups: "7" cells: 306821 interior faces: 1690 boundary faces: 99538 "CC_SAL_SD6" interior faces: 1690 "CC_SAL_SD6_extruded" cells: 8450 "CC_SAL_SD6_top" boundary faces: 1690 "IF_5-6_2" boundary faces: 358 --- Information on the volumes Minimum control volume = 1.0986596e-08 Maximum control volume = 2.6395856e-04 Total volume for the domain = 4.7312750e+00 Criterion 1: Orthogonality: Number of bad cells detected: 0 --> 0 % Criterion 2: Offset: Number of bad cells detected: 0 --> 0 % Criterion 3: Least-Squares Gradient Quality: Number of bad cells detected: 44 --> 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 (0.236 s) Extended neighborhood reduced by non-orthogonality -------------------------------------------------- Size of complete cell-cell connectivity: 18221804 Size of filtered cell-cell conectivity: 52558 18169246 connections removed, for a ratio of 0.29 % used ALMAX = 0.16779E+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 ----------------------------------------- Velocity 0.0000E+00 0.0000E+00 Velocity 0.0000E+00 0.0000E+00 Velocity 0.0000E+00 0.0000E+00 Pressure 0.0000E+00 0.0000E+00 k 0.6000E-03 0.6000E-03 epsilon 0.7883E-06 0.7883E-06 --------------------------------- dt 0.5000E-01 0.5000E-01 --------------------------------- ------------------------------------------------------------- ------------------------------------------------------------- =============================================================== MAIN CALCULATION ================ =============================================================== =============================================================== INSTANT 0.500000000E-01 TIME STEP NUMBER 1 ============================================================= ----------------------------------------- Property Min. value Max. value ----------------------------------------- density 0.4050E+00 0.4050E+00 molecular_viscos 0.3651E-04 0.3651E-04 turbulent_viscos 0.1665E-01 0.1665E-01 ----------------------------------------- ** INFORMATION ON BOUNDARY FACES TYPE ---------------------------------- ------------------------------------------------------------------------- Boundary type Code Nb faces ------------------------------------------------------------------------- Inlet 2 358 Smooth wall 5 97490 Rough wall 6 0 Symmetry 4 0 Free outlet 3 1690 Free inlet 13 0 Undefined 1 0 ------------------------------------------------------------------------- Boundary faces with free inlet/outlet detected Update of reference point for total pressure XYZP0 = 0.70962E+01 0.67173E+01 0.10308E+02 ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 358 0.000000000E+00 Smooth wall 5 97490 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 1690 0.000000000E+00 Free inlet 13 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.00000E+00 0.00000E+00 Friction velocity uk : 0.14334E-02 0.92136E-02 Dimensionless distance yplus : 0.73896E-02 0.26395E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 97486 Total number of wall faces : 97490 ------------------------------------------------------------ @ @@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@ @ @ @@ WARNING: MESH TOO REFINED AT THE WALL @ ======== @ The mesh seems to be too refined at the wall to use @ a high-Reynolds turbulence model. @ @ The last time step at which too small values for the @ dimensionless distance to the wall (yplus) have been @ observed is the time step 1 @ @ The minimum value for yplus must be greater than the @ limit value YPLULI = 0.23810E+01 @ @ Have a look at the distribution of yplus at the wall @ (with EnSight or ParaView for example) to conclude on @ the way the results quality might be affected. @ @ This warning is only printed at the first two @ occurences of the problem and at the last time step @ of the calculation. The vanishing of the message does @ not necessarily mean the vanishing of the problem. @ @@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@ @ TIME FOR THE TIME STEP 1: 0.77522E+01 =============================================================== INSTANT 0.100000000E+00 TIME STEP NUMBER 2 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 358 -0.264069000E+01 Smooth wall 5 97490 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 1690 0.264079177E+01 Free inlet 13 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : -0.20948E+03 0.12090E+03 Friction velocity uet : 0.11238E-01 0.10281E+02 Friction velocity uk : 0.25750E-01 0.49146E+01 Dimensionless distance yplus : 0.10100E+01 0.25768E+03 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 28811 Nb of faces within the viscous sub-layer : 54 Total number of wall faces : 97490 ------------------------------------------------------------ @ @@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@ @ @ @@ WARNING: MESH TOO REFINED AT THE WALL @ ======== @ The mesh seems to be too refined at the wall to use @ a high-Reynolds turbulence model. @ @ The last time step at which too small values for the @ dimensionless distance to the wall (yplus) have been @ observed is the time step 2 @ @ The minimum value for yplus must be greater than the @ limit value YPLULI = 0.23810E+01 @ @ Have a look at the distribution of yplus at the wall @ (with EnSight or ParaView for example) to conclude on @ the way the results quality might be affected. @ @ This warning is only printed at the first two @ occurences of the problem and at the last time step @ of the calculation. The vanishing of the message does @ not necessarily mean the vanishing of the problem. @ @@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@ @ TIME FOR THE TIME STEP 2: 0.47723E+01 =============================================================== INSTANT 0.150000000E+00 TIME STEP NUMBER 3 ============================================================= TIME FOR THE TIME STEP 3: 0.36340E+01 =============================================================== INSTANT 0.200000000E+00 TIME STEP NUMBER 4 ============================================================= TIME FOR THE TIME STEP 4: 0.36274E+01 =============================================================== INSTANT 0.250000000E+00 TIME STEP NUMBER 5 ============================================================= TIME FOR THE TIME STEP 5: 0.37117E+01 =============================================================== INSTANT 0.300000000E+00 TIME STEP NUMBER 6 ============================================================= TIME FOR THE TIME STEP 6: 0.44892E+01 =============================================================== INSTANT 0.350000000E+00 TIME STEP NUMBER 7 ============================================================= TIME FOR THE TIME STEP 7: 0.39395E+01 =============================================================== INSTANT 0.400000000E+00 TIME STEP NUMBER 8 ============================================================= TIME FOR THE TIME STEP 8: 0.35817E+01 =============================================================== INSTANT 0.450000000E+00 TIME STEP NUMBER 9 ============================================================= TIME FOR THE TIME STEP 9: 0.38757E+01 =============================================================== INSTANT 0.500000000E+00 TIME STEP NUMBER 10 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 358 -0.264069000E+01 Smooth wall 5 97490 -0.140023011E-17 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 1690 0.264000237E+01 Free inlet 13 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : -0.72312E+03 0.20620E+03 Friction velocity uet : 0.16957E-02 0.17162E+02 Friction velocity uk : 0.25905E-01 0.32988E+02 Dimensionless distance yplus : 0.20758E+01 0.12391E+04 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 68033 Nb of faces within the viscous sub-layer : 5 Total number of wall faces : 97490 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- --------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual derive --------------------------------------------------------------- c VelocityX 0.89931E+02 152 0.17331E+00 0.30354E+03 c VelocityY 0.89931E+02 152 0.17331E+00 0.00000E+00 c VelocityZ 0.89931E+02 152 0.17331E+00 0.00000E+00 c Pressure 0.19493E+00 412 0.24787E-01 0.21072E+00 c k 0.72115E+02 115 0.28839E-01 0.35520E+04 c epsilon 0.42678E+06 69 0.26172E-01 0.28111E+12 --------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a epsilon a Local Time Step 3.9191e-05 38051 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ------------------- -------------- -------------- -------------- -------------- v Velocity[X] -260.1 126.85 -9.4591 9.7446 v Velocity[Y] -291.7 162.85 -5.5125 -4.4825 v Velocity[Z] -179.25 168.98 0.032288 1.0288 v ǁVelocityǁ 0.022058 299.45 39.828 32.703 v Pressure -2415.5 6452.4 5077.1 5807.4 v k 0.00052962 7778 0.92546 0.66925 v epsilon 8.1274e-06 6.6933e+07 1188.3 100.78 v turbulent_viscosity 2.0077e-07 0.027455 0.00036429 0.00076189 v CourantNb 0.017098 673.61 15.159 5.5457 v FourierNb 0.00067546 26.033 0.070216 0.046114 v total_pressure 98909 1.0778e+05 1.064e+05 1.0713e+05 v Local Time Step 0.0025 0.027036 0.0025843 0.0025454 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.040382 677.59 15.229 5.5918 TIME FOR THE TIME STEP 10: 0.38382E+01 =============================================================== INSTANT 0.550000000E+00 TIME STEP NUMBER 11 ============================================================= TIME FOR THE TIME STEP 11: 0.37111E+01 =============================================================== INSTANT 0.600000000E+00 TIME STEP NUMBER 12 ============================================================= TIME FOR THE TIME STEP 12: 0.35289E+01 =============================================================== INSTANT 0.650000000E+00 TIME STEP NUMBER 13 ============================================================= TIME FOR THE TIME STEP 13: 0.32783E+01 =============================================================== INSTANT 0.700000000E+00 TIME STEP NUMBER 14 ============================================================= TIME FOR THE TIME STEP 14: 0.30738E+01 =============================================================== INSTANT 0.750000000E+00 TIME STEP NUMBER 15 ============================================================= TIME FOR THE TIME STEP 15: 0.32932E+01 =============================================================== INSTANT 0.800000000E+00 TIME STEP NUMBER 16 ============================================================= TIME FOR THE TIME STEP 16: 0.35223E+01 =============================================================== INSTANT 0.850000000E+00 TIME STEP NUMBER 17 ============================================================= TIME FOR THE TIME STEP 17: 0.33288E+01 =============================================================== INSTANT 0.900000000E+00 TIME STEP NUMBER 18 ============================================================= TIME FOR THE TIME STEP 18: 0.32919E+01 =============================================================== INSTANT 0.950000000E+00 TIME STEP NUMBER 19 ============================================================= TIME FOR THE TIME STEP 19: 0.34194E+01 =============================================================== INSTANT 0.100000000E+01 TIME STEP NUMBER 20 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 358 -0.264069000E+01 Smooth wall 5 97490 0.426229604E-17 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 1690 0.264236289E+01 Free inlet 13 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : -0.89053E+03 0.20466E+03 Friction velocity uet : 0.74000E-03 0.41609E+02 Friction velocity uk : 0.30293E-01 0.95118E+02 Dimensionless distance yplus : 0.27408E+01 0.51967E+04 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 29543 Nb of faces within the viscous sub-layer : 0 Total number of wall faces : 97490 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- --------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual derive --------------------------------------------------------------- c VelocityX 0.84925E+02 154 0.23301E+00 0.26573E+03 c VelocityY 0.84925E+02 154 0.23301E+00 0.00000E+00 c VelocityZ 0.84925E+02 154 0.23301E+00 0.00000E+00 c Pressure 0.21408E+00 210 0.98980E-02 0.11311E+00 c k 0.10927E+04 77 0.21132E-02 0.37162E+04 c epsilon 0.24140E+08 22 0.72810E-03 0.13271E+13 --------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a epsilon a Local Time Step 3.4071e-05 38063 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ------------------- -------------- -------------- -------------- -------------- v Velocity[X] -348.79 125.57 -8.5985 9.7304 v Velocity[Y] -217.87 206.69 -6.7547 -4.4651 v Velocity[Z] -185.86 186.33 -0.20609 1.0393 v ǁVelocityǁ 0.08041 367.86 43.342 32.707 v Pressure -4824.5 6052.2 4788.6 5530 v k 0.00097097 31955 3.6109 1.2644 v epsilon 0.00023586 6.803e+08 14667 1225.6 v turbulent_viscosity 6.3461e-07 0.053253 0.00065654 0.0011047 v CourantNb 0.02043 650.19 16.463 5.7882 v FourierNb 0.00070259 28.92 0.18898 0.071941 v total_pressure 96501 1.0738e+05 1.0611e+05 1.0686e+05 v Local Time Step 0.0025 0.04584 0.0025926 0.0025603 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.04662 677.12 16.652 5.8602 TIME FOR THE TIME STEP 20: 0.31547E+01 =============================================================== INSTANT 0.105000000E+01 TIME STEP NUMBER 21 ============================================================= TIME FOR THE TIME STEP 21: 0.29629E+01 =============================================================== INSTANT 0.110000000E+01 TIME STEP NUMBER 22 ============================================================= TIME FOR THE TIME STEP 22: 0.29372E+01 =============================================================== INSTANT 0.115000000E+01 TIME STEP NUMBER 23 ============================================================= TIME FOR THE TIME STEP 23: 0.29279E+01 =============================================================== INSTANT 0.120000000E+01 TIME STEP NUMBER 24 ============================================================= TIME FOR THE TIME STEP 24: 0.29961E+01 =============================================================== INSTANT 0.125000000E+01 TIME STEP NUMBER 25 ============================================================= TIME FOR THE TIME STEP 25: 0.30267E+01 =============================================================== INSTANT 0.130000000E+01 TIME STEP NUMBER 26 ============================================================= TIME FOR THE TIME STEP 26: 0.30358E+01 =============================================================== INSTANT 0.135000000E+01 TIME STEP NUMBER 27 ============================================================= TIME FOR THE TIME STEP 27: 0.30226E+01 =============================================================== INSTANT 0.140000000E+01 TIME STEP NUMBER 28 ============================================================= TIME FOR THE TIME STEP 28: 0.30148E+01 =============================================================== INSTANT 0.145000000E+01 TIME STEP NUMBER 29 ============================================================= TIME FOR THE TIME STEP 29: 0.29984E+01 =============================================================== INSTANT 0.150000000E+01 TIME STEP NUMBER 30 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 358 -0.264069000E+01 Smooth wall 5 97490 0.450475762E-16 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 1690 0.263863129E+01 Free inlet 13 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : -0.12685E+04 0.22751E+03 Friction velocity uet : 0.76865E-03 0.28863E+02 Friction velocity uk : 0.49906E-01 0.59231E+02 Dimensionless distance yplus : 0.27224E+01 0.35147E+04 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 8857 Nb of faces within the viscous sub-layer : 0 Total number of wall faces : 97490 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- --------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual derive --------------------------------------------------------------- c VelocityX 0.85210E+02 155 0.29725E+00 0.22390E+03 c VelocityY 0.85210E+02 155 0.29725E+00 0.00000E+00 c VelocityZ 0.85210E+02 155 0.29725E+00 0.00000E+00 c Pressure 0.23748E+00 158 0.57309E-02 0.79272E-01 c k 0.60831E+03 65 0.11622E-02 0.26501E+04 c epsilon 0.10867E+08 24 0.65708E-03 0.75270E+12 --------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a epsilon a Local Time Step 3.2021e-05 38209 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ------------------- -------------- -------------- -------------- -------------- v Velocity[X] -760.93 175.21 -7.9765 9.7321 v Velocity[Y] -262.02 274.53 -7.2312 -4.4558 v Velocity[Z] -278.29 256.56 -0.20521 1.0383 v ǁVelocityǁ 0.056351 763.77 44.121 32.573 v Pressure -6506.9 7111.6 5538.1 6314.9 v k 0.0015391 12484 4.5298 1.7124 v epsilon 0.0032402 2.2119e+08 11296 879.94 v turbulent_viscosity 2.2032e-07 0.024719 0.00089116 0.0013503 v CourantNb 0.050441 659.61 16.861 5.8412 v FourierNb 0.00091351 34.548 0.24861 0.093089 v total_pressure 94818 1.0844e+05 1.0686e+05 1.0764e+05 v Local Time Step 0.0025 0.03103 0.0025683 0.0025605 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.12162 672.02 17.11 5.9343 TIME FOR THE TIME STEP 30: 0.29663E+01 =============================================================== INSTANT 0.155000000E+01 TIME STEP NUMBER 31 ============================================================= TIME FOR THE TIME STEP 31: 0.29291E+01 =============================================================== INSTANT 0.160000000E+01 TIME STEP NUMBER 32 ============================================================= TIME FOR THE TIME STEP 32: 0.29054E+01 =============================================================== INSTANT 0.165000000E+01 TIME STEP NUMBER 33 ============================================================= TIME FOR THE TIME STEP 33: 0.29096E+01 =============================================================== INSTANT 0.170000000E+01 TIME STEP NUMBER 34 ============================================================= TIME FOR THE TIME STEP 34: 0.29578E+01 =============================================================== INSTANT 0.175000000E+01 TIME STEP NUMBER 35 ============================================================= TIME FOR THE TIME STEP 35: 0.29861E+01 =============================================================== INSTANT 0.180000000E+01 TIME STEP NUMBER 36 ============================================================= TIME FOR THE TIME STEP 36: 0.29714E+01 =============================================================== INSTANT 0.185000000E+01 TIME STEP NUMBER 37 ============================================================= TIME FOR THE TIME STEP 37: 0.29389E+01 =============================================================== INSTANT 0.190000000E+01 TIME STEP NUMBER 38 ============================================================= TIME FOR THE TIME STEP 38: 0.29317E+01 =============================================================== INSTANT 0.195000000E+01 TIME STEP NUMBER 39 ============================================================= TIME FOR THE TIME STEP 39: 0.29295E+01 =============================================================== INSTANT 0.200000000E+01 TIME STEP NUMBER 40 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 358 -0.264069000E+01 Smooth wall 5 97490 0.419301403E-16 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 1690 0.264300635E+01 Free inlet 13 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : -0.44442E+03 0.32415E+03 Friction velocity uet : 0.19292E-02 0.25602E+02 Friction velocity uk : 0.52616E-01 0.10262E+03 Dimensionless distance yplus : 0.28802E+01 0.69512E+04 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 1923 Nb of faces within the viscous sub-layer : 0 Total number of wall faces : 97490 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- --------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual derive --------------------------------------------------------------- c VelocityX 0.92255E+02 163 0.39470E+00 0.15215E+03 c VelocityY 0.92255E+02 163 0.39470E+00 0.00000E+00 c VelocityZ 0.92255E+02 163 0.39470E+00 0.00000E+00 c Pressure 0.26891E+00 120 0.38462E-02 0.61042E-01 c k 0.17746E+04 78 0.20677E-02 0.39592E+04 c epsilon 0.36748E+08 27 0.17531E-02 0.61365E+12 --------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a epsilon a Local Time Step 3.0656e-05 38324 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ------------------- -------------- -------------- -------------- -------------- v Velocity[X] -461.6 210.06 -7.8752 9.7483 v Velocity[Y] -357.56 221.63 -7.3183 -4.4379 v Velocity[Z] -314.65 297.6 -0.23055 1.0278 v ǁVelocityǁ 0.17667 465.57 44.349 32.444 v Pressure -9702 8433.1 5122.1 5895.6 v k 0.0024701 34029 8.5627 2.3732 v epsilon 0.015278 7.1177e+08 24196 2049 v turbulent_viscosity 4.2006e-07 0.065599 0.0011843 0.0015377 v CourantNb 0.05096 913.69 17.076 5.8427 v FourierNb 0.0013261 40.369 0.41781 0.11333 v total_pressure 91623 1.0976e+05 1.0645e+05 1.0722e+05 v Local Time Step 0.0025 0.037154 0.0025552 0.0025632 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.086647 913.85 17.494 5.956 TIME FOR THE TIME STEP 40: 0.29679E+01 =============================================================== INSTANT 0.205000000E+01 TIME STEP NUMBER 41 ============================================================= TIME FOR THE TIME STEP 41: 0.29125E+01 =============================================================== INSTANT 0.210000000E+01 TIME STEP NUMBER 42 ============================================================= TIME FOR THE TIME STEP 42: 0.29151E+01 =============================================================== INSTANT 0.215000000E+01 TIME STEP NUMBER 43 ============================================================= TIME FOR THE TIME STEP 43: 0.29093E+01 =============================================================== INSTANT 0.220000000E+01 TIME STEP NUMBER 44 ============================================================= TIME FOR THE TIME STEP 44: 0.30755E+01 =============================================================== INSTANT 0.225000000E+01 TIME STEP NUMBER 45 ============================================================= TIME FOR THE TIME STEP 45: 0.29242E+01 =============================================================== INSTANT 0.230000000E+01 TIME STEP NUMBER 46 ============================================================= TIME FOR THE TIME STEP 46: 0.29930E+01 =============================================================== INSTANT 0.235000000E+01 TIME STEP NUMBER 47 ============================================================= TIME FOR THE TIME STEP 47: 0.30121E+01 =============================================================== INSTANT 0.240000000E+01 TIME STEP NUMBER 48 ============================================================= TIME FOR THE TIME STEP 48: 0.30264E+01 =============================================================== INSTANT 0.245000000E+01 TIME STEP NUMBER 49 ============================================================= TIME FOR THE TIME STEP 49: 0.30021E+01 =============================================================== INSTANT 0.250000000E+01 TIME STEP NUMBER 50 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 358 -0.264069000E+01 Smooth wall 5 97490 -0.151236471E-16 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 1690 0.263761011E+01 Free inlet 13 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : -0.24575E+03 0.36718E+03 Friction velocity uet : 0.51040E-02 0.26335E+02 Friction velocity uk : 0.66794E-01 0.96555E+02 Dimensionless distance yplus : 0.30891E+01 0.65087E+04 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 662 Nb of faces within the viscous sub-layer : 0 Total number of wall faces : 97490 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- --------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual derive --------------------------------------------------------------- c VelocityX 0.14277E+03 176 0.66698E+00 0.15965E+03 c VelocityY 0.14277E+03 176 0.66698E+00 0.00000E+00 c VelocityZ 0.14277E+03 176 0.66698E+00 0.00000E+00 c Pressure 0.35969E+00 139 0.34442E-02 0.56152E-01 c k 0.12052E+05 69 0.37765E-02 0.52189E+06 c epsilon 0.11686E+09 44 0.99186E-02 0.59867E+14 --------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a epsilon a Local Time Step 2.9772e-05 38352 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ------------------- -------------- -------------- -------------- -------------- v Velocity[X] -570.91 327.15 -7.9937 9.7596 v Velocity[Y] -356.33 422.03 -7.4189 -4.4473 v Velocity[Z] -395.33 250.49 -0.15037 1.021 v ǁVelocityǁ 0.075346 576.75 44.516 32.295 v Pressure -11648 11442 5502.5 6298.7 v k 0.0051035 46707 24.268 4.0541 v epsilon 0.044267 7.9208e+08 99291 8898.7 v turbulent_viscosity 1.5924e-06 0.12683 0.0014902 0.0016774 v CourantNb 0.067153 1099.9 17.404 5.8362 v FourierNb 0.0019344 129.55 0.61472 0.13196 v total_pressure 89677 1.1277e+05 1.0683e+05 1.0762e+05 v Local Time Step 0.0025 0.025913 0.0025543 0.0025681 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.12683 1102.1 18.019 5.9681 TIME FOR THE TIME STEP 50: 0.31061E+01 =============================================================== INSTANT 0.255000000E+01 TIME STEP NUMBER 51 ============================================================= TIME FOR THE TIME STEP 51: 0.30223E+01 =============================================================== INSTANT 0.260000000E+01 TIME STEP NUMBER 52 ============================================================= TIME FOR THE TIME STEP 52: 0.30587E+01 =============================================================== INSTANT 0.265000000E+01 TIME STEP NUMBER 53 ============================================================= TIME FOR THE TIME STEP 53: 0.29892E+01 =============================================================== INSTANT 0.270000000E+01 TIME STEP NUMBER 54 ============================================================= TIME FOR THE TIME STEP 54: 0.30291E+01 =============================================================== INSTANT 0.275000000E+01 TIME STEP NUMBER 55 ============================================================= TIME FOR THE TIME STEP 55: 0.30682E+01 =============================================================== INSTANT 0.280000000E+01 TIME STEP NUMBER 56 ============================================================= TIME FOR THE TIME STEP 56: 0.30028E+01 =============================================================== INSTANT 0.285000000E+01 TIME STEP NUMBER 57 ============================================================= TIME FOR THE TIME STEP 57: 0.30897E+01 =============================================================== INSTANT 0.290000000E+01 TIME STEP NUMBER 58 ============================================================= TIME FOR THE TIME STEP 58: 0.30206E+01 =============================================================== INSTANT 0.295000000E+01 TIME STEP NUMBER 59 ============================================================= TIME FOR THE TIME STEP 59: 0.32707E+01 =============================================================== INSTANT 0.300000000E+01 TIME STEP NUMBER 60 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 358 -0.264069000E+01 Smooth wall 5 97490 0.464260622E-17 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 1690 0.264065776E+01 Free inlet 13 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : -0.19759E+03 0.62731E+03 Friction velocity uet : 0.43511E-02 0.28917E+02 Friction velocity uk : 0.79732E-01 0.30261E+03 Dimensionless distance yplus : 0.23685E+01 0.20827E+05 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 142 Nb of faces within the viscous sub-layer : 1 Total number of wall faces : 97490 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- --------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual derive --------------------------------------------------------------- c VelocityX 0.39649E+03 228 0.85489E+00 0.29059E+03 c VelocityY 0.39649E+03 228 0.85489E+00 0.00000E+00 c VelocityZ 0.39649E+03 228 0.85489E+00 0.00000E+00 c Pressure 0.63341E+00 102 0.39719E-02 0.64550E-01 c k 0.32076E+06 48 0.27460E-02 0.17304E+08 c epsilon 0.82378E+10 36 0.51513E-02 0.12385E+17 --------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a epsilon a Local Time Step 2.8424e-05 38352 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ------------------- -------------- -------------- -------------- -------------- v Velocity[X] -672.16 677.14 -8.1575 9.7656 v Velocity[Y] -530.05 899.33 -7.2518 -4.4241 v Velocity[Z] -594.64 484.38 -0.074675 1.0116 v ǁVelocityǁ 0.12367 1042.3 44.827 32.212 v Pressure -14387 16343 6007.9 6857.4 v k 0.0054445 3.8341e+05 108.94 13.653 v epsilon 0.14941 1.6622e+10 1.5018e+06 1.4312e+05 v turbulent_viscosity 1.9888e-06 0.52526 0.0019875 0.0017968 v CourantNb 0.13209 2073 17.818 5.8457 v FourierNb 0.0034013 422.27 0.97891 0.15831 v total_pressure 86938 1.1767e+05 1.0733e+05 1.0818e+05 v Local Time Step 0.0025 0.035198 0.0025548 0.0025742 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.16245 2330.2 18.797 6.004 TIME FOR THE TIME STEP 60: 0.33443E+01 =============================================================== INSTANT 0.305000000E+01 TIME STEP NUMBER 61 ============================================================= TIME FOR THE TIME STEP 61: 0.32896E+01 =============================================================== INSTANT 0.310000000E+01 TIME STEP NUMBER 62 ============================================================= TIME FOR THE TIME STEP 62: 0.35928E+01 =============================================================== INSTANT 0.315000000E+01 TIME STEP NUMBER 63 ============================================================= TIME FOR THE TIME STEP 63: 0.34066E+01 =============================================================== INSTANT 0.320000000E+01 TIME STEP NUMBER 64 ============================================================= TIME FOR THE TIME STEP 64: 0.34902E+01 =============================================================== INSTANT 0.325000000E+01 TIME STEP NUMBER 65 ============================================================= TIME FOR THE TIME STEP 65: 0.35925E+01 =============================================================== INSTANT 0.330000000E+01 TIME STEP NUMBER 66 ============================================================= TIME FOR THE TIME STEP 66: 0.37328E+01 =============================================================== INSTANT 0.335000000E+01 TIME STEP NUMBER 67 ============================================================= TIME FOR THE TIME STEP 67: 0.41089E+01 =============================================================== INSTANT 0.340000000E+01 TIME STEP NUMBER 68 ============================================================= TIME FOR THE TIME STEP 68: 0.37533E+01 =============================================================== INSTANT 0.345000000E+01 TIME STEP NUMBER 69 ============================================================= Incoming flow detained for 1 outlet faces on 1690 TIME FOR THE TIME STEP 69: 0.43150E+01 =============================================================== INSTANT 0.350000000E+01 TIME STEP NUMBER 70 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 358 -0.264069000E+01 Smooth wall 5 97490 0.102568409E-16 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 1690 0.263648801E+01 Free inlet 13 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : -0.10226E+03 0.17088E+04 Friction velocity uet : 0.50972E-02 0.62521E+02 Friction velocity uk : 0.88968E-01 0.94524E+03 Dimensionless distance yplus : 0.15774E+01 0.66216E+05 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 33 Nb of faces within the viscous sub-layer : 1 Total number of wall faces : 97490 ------------------------------------------------------------ Incoming flow detained for 1 outlet faces on 1690 ** INFORMATION ON CONVERGENCE -------------------------- --------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual derive --------------------------------------------------------------- c VelocityX 0.28478E+04 337 0.80961E+00 0.60990E+03 c VelocityY 0.28478E+04 337 0.80961E+00 0.00000E+00 c VelocityZ 0.28478E+04 337 0.80961E+00 0.00000E+00 c Pressure 0.13330E+01 95 0.50527E-02 0.76821E-01 c k 0.97109E+07 49 0.32998E-02 0.15335E+10 c epsilon 0.62213E+12 36 0.91879E-02 0.11052E+20 --------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a epsilon a Local Time Step 2.8453e-05 38352 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ------------------- -------------- -------------- -------------- -------------- v Velocity[X] -1134.6 2014.1 -8.2372 9.7641 v Velocity[Y] -1171.7 1772.2 -7.0147 -4.4109 v Velocity[Z] -1497.7 1228.6 -0.12447 0.99752 v ǁVelocityǁ 0.1089 2309.5 45.588 32.252 v Pressure -33439 38788 6366.9 7285.9 v k 0.0068794 4.2813e+06 852.69 104.39 v epsilon 0.27315 4.7233e+11 3.8507e+07 3.7094e+06 v turbulent_viscosity 2.218e-06 2.4597 0.0033292 0.0019936 v CourantNb 0.0040378 4968.6 18.612 5.9029 v FourierNb 0.0048692 1794.8 1.9288 0.22658 v total_pressure 67886 1.4011e+05 1.0769e+05 1.0861e+05 v Local Time Step 0.0025 0.026721 0.0025598 0.0025813 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.11162 6064.3 20.541 6.1294 TIME FOR THE TIME STEP 70: 0.41261E+01 =============================================================== INSTANT 0.355000000E+01 TIME STEP NUMBER 71 ============================================================= Incoming flow detained for 1 outlet faces on 1690 TIME FOR THE TIME STEP 71: 0.46041E+01 =============================================================== INSTANT 0.360000000E+01 TIME STEP NUMBER 72 ============================================================= Incoming flow detained for 1 outlet faces on 1690 TIME FOR THE TIME STEP 72: 0.44717E+01 =============================================================== INSTANT 0.365000000E+01 TIME STEP NUMBER 73 ============================================================= Incoming flow detained for 1 outlet faces on 1690 TIME FOR THE TIME STEP 73: 0.46888E+01 =============================================================== INSTANT 0.370000000E+01 TIME STEP NUMBER 74 ============================================================= Incoming flow detained for 1 outlet faces on 1690 TIME FOR THE TIME STEP 74: 0.48102E+01 =============================================================== INSTANT 0.375000000E+01 TIME STEP NUMBER 75 ============================================================= Incoming flow detained for 1 outlet faces on 1690 TIME FOR THE TIME STEP 75: 0.58521E+01 =============================================================== INSTANT 0.380000000E+01 TIME STEP NUMBER 76 ============================================================= Incoming flow detained for 1 outlet faces on 1690 TIME FOR THE TIME STEP 76: 0.47757E+01 =============================================================== INSTANT 0.385000000E+01 TIME STEP NUMBER 77 ============================================================= Incoming flow detained for 1 outlet faces on 1690 TIME FOR THE TIME STEP 77: 0.52263E+01 =============================================================== INSTANT 0.390000000E+01 TIME STEP NUMBER 78 ============================================================= Incoming flow detained for 1 outlet faces on 1690 TIME FOR THE TIME STEP 78: 0.53043E+01 =============================================================== INSTANT 0.395000000E+01 TIME STEP NUMBER 79 ============================================================= Incoming flow detained for 1 outlet faces on 1690 TIME FOR THE TIME STEP 79: 0.52379E+01 =============================================================== INSTANT 0.400000000E+01 TIME STEP NUMBER 80 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 358 -0.264069000E+01 Smooth wall 5 97490 -0.866151245E-16 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 1690 0.262846187E+01 Free inlet 13 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : -0.16805E+03 0.41762E+04 Friction velocity uet : 0.86085E-02 0.14097E+03 Friction velocity uk : 0.89502E-01 0.23745E+04 Dimensionless distance yplus : 0.32384E+01 0.17272E+06 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 28 Nb of faces within the viscous sub-layer : 0 Total number of wall faces : 97490 ------------------------------------------------------------ Incoming flow detained for 1 outlet faces on 1690 ** INFORMATION ON CONVERGENCE -------------------------- --------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual derive --------------------------------------------------------------- c VelocityX 0.14775E+05 505 0.88055E+00 0.43357E+04 c VelocityY 0.14775E+05 505 0.88055E+00 0.00000E+00 c VelocityZ 0.14775E+05 505 0.88055E+00 0.00000E+00 c Pressure 0.30832E+01 124 0.62572E-02 0.87782E-01 c k 0.16463E+09 51 0.31585E-02 0.59838E+11 c epsilon 0.24866E+14 36 0.83601E-02 0.24312E+22 --------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a epsilon a Local Time Step 2.8137e-05 38352 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ------------------- -------------- -------------- -------------- -------------- v Velocity[X] -2787.5 5065.4 -8.0576 9.75 v Velocity[Y] -2813.8 4238.1 -6.4416 -4.3335 v Velocity[Z] -3457.1 2913.1 -0.4054 0.96769 v ǁVelocityǁ 0.080794 5402.7 48.217 32.824 v Pressure -83701 92152 8073.8 9189.6 v k 0.034726 2.7997e+07 5651.7 702.3 v epsilon 0.64248 7.3642e+12 6.2905e+08 6.1411e+07 v turbulent_viscosity 8.5736e-06 6.784 0.0072998 0.0025274 v CourantNb 0.084067 11311 20.277 6.0915 v FourierNb 0.0040232 5174.4 4.6011 0.42926 v total_pressure 17624 1.9348e+05 1.094e+05 1.1051e+05 v Local Time Step 0.0025 0.03856 0.0025538 0.0025735 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.16664 14165 24.878 6.5208 TIME FOR THE TIME STEP 80: 0.54166E+01 =============================================================== INSTANT 0.405000000E+01 TIME STEP NUMBER 81 ============================================================= Incoming flow detained for 1 outlet faces on 1690 TIME FOR THE TIME STEP 81: 0.56195E+01 =============================================================== INSTANT 0.410000000E+01 TIME STEP NUMBER 82 ============================================================= Incoming flow detained for 1 outlet faces on 1690 TIME FOR THE TIME STEP 82: 0.60041E+01 =============================================================== INSTANT 0.415000000E+01 TIME STEP NUMBER 83 ============================================================= Incoming flow detained for 1 outlet faces on 1690 TIME FOR THE TIME STEP 83: 0.64328E+01 =============================================================== INSTANT 0.420000000E+01 TIME STEP NUMBER 84 ============================================================= Incoming flow detained for 1 outlet faces on 1690 TIME FOR THE TIME STEP 84: 0.60095E+01 =============================================================== INSTANT 0.425000000E+01 TIME STEP NUMBER 85 ============================================================= Incoming flow detained for 1 outlet faces on 1690 TIME FOR THE TIME STEP 85: 0.51983E+01 =============================================================== INSTANT 0.430000000E+01 TIME STEP NUMBER 86 ============================================================= Incoming flow detained for 12 outlet faces on 1690 TIME FOR THE TIME STEP 86: 0.52862E+01 =============================================================== INSTANT 0.435000000E+01 TIME STEP NUMBER 87 ============================================================= Incoming flow detained for 50 outlet faces on 1690 TIME FOR THE TIME STEP 87: 0.58263E+01 =============================================================== INSTANT 0.440000000E+01 TIME STEP NUMBER 88 ============================================================= Incoming flow detained for 144 outlet faces on 1690 TIME FOR THE TIME STEP 88: 0.53281E+01 =============================================================== INSTANT 0.445000000E+01 TIME STEP NUMBER 89 ============================================================= Incoming flow detained for 272 outlet faces on 1690 TIME FOR THE TIME STEP 89: 0.55157E+01 =============================================================== INSTANT 0.450000000E+01 TIME STEP NUMBER 90 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 358 -0.264069000E+01 Smooth wall 5 97490 0.681020149E-15 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 1690 0.261086335E+01 Free inlet 13 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : -0.14232E+02 0.10105E+05 Friction velocity uet : 0.55678E-02 0.31844E+03 Friction velocity uk : 0.13596E+00 0.57143E+04 Dimensionless distance yplus : 0.64043E+01 0.41714E+06 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 8 Nb of faces within the viscous sub-layer : 0 Total number of wall faces : 97490 ------------------------------------------------------------ Incoming flow detained for 333 outlet faces on 1690 ** INFORMATION ON CONVERGENCE -------------------------- --------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual derive --------------------------------------------------------------- c VelocityX 0.81115E+05 605 0.87621E+00 0.48437E+05 c VelocityY 0.81115E+05 605 0.87621E+00 0.00000E+00 c VelocityZ 0.81115E+05 605 0.87621E+00 0.00000E+00 c Pressure 0.74537E+01 144 0.67510E-02 0.94579E-01 c k 0.23558E+10 52 0.32281E-02 0.20184E+13 c epsilon 0.84268E+15 36 0.84344E-02 0.46746E+24 --------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a epsilon a Local Time Step 2.8114e-05 38352 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ------------------- -------------- -------------- -------------- -------------- v Velocity[X] -6583 12042 -7.8679 9.7732 v Velocity[Y] -6475.2 10067 -5.6403 -3.9395 v Velocity[Z] -8129.2 7942.2 -1.2897 0.89276 v ǁVelocityǁ 0.1572 12735 62.06 37.019 v Pressure -2.1715e+05 2.1286e+05 12558 14271 v k 0.075467 1.6785e+08 32688 4136.7 v epsilon 1.1161 1.0218e+14 8.8549e+09 8.7351e+08 v turbulent_viscosity 1.1738e-05 16.771 0.016198 0.0045267 v CourantNb 0.0025395 26260 26.011 7.0167 v FourierNb 0.0045563 12705 9.9589 0.92497 v total_pressure -1.1582e+05 3.1419e+05 1.1388e+05 1.156e+05 v Local Time Step 0.0025 0.023547 0.0025267 0.0025364 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.17666 33217 35.97 7.9417 TIME FOR THE TIME STEP 90: 0.55173E+01 =============================================================== INSTANT 0.455000000E+01 TIME STEP NUMBER 91 ============================================================= Incoming flow detained for 338 outlet faces on 1690 TIME FOR THE TIME STEP 91: 0.55676E+01 =============================================================== INSTANT 0.460000000E+01 TIME STEP NUMBER 92 ============================================================= Incoming flow detained for 338 outlet faces on 1690 TIME FOR THE TIME STEP 92: 0.58896E+01 =============================================================== INSTANT 0.465000000E+01 TIME STEP NUMBER 93 ============================================================= Incoming flow detained for 338 outlet faces on 1690 TIME FOR THE TIME STEP 93: 0.57387E+01 =============================================================== INSTANT 0.470000000E+01 TIME STEP NUMBER 94 ============================================================= Incoming flow detained for 338 outlet faces on 1690 TIME FOR THE TIME STEP 94: 0.56403E+01 =============================================================== INSTANT 0.475000000E+01 TIME STEP NUMBER 95 ============================================================= Incoming flow detained for 339 outlet faces on 1690 TIME FOR THE TIME STEP 95: 0.57869E+01 =============================================================== INSTANT 0.480000000E+01 TIME STEP NUMBER 96 ============================================================= Incoming flow detained for 338 outlet faces on 1690 TIME FOR THE TIME STEP 96: 0.60792E+01 =============================================================== INSTANT 0.485000000E+01 TIME STEP NUMBER 97 ============================================================= Incoming flow detained for 338 outlet faces on 1690 TIME FOR THE TIME STEP 97: 0.58598E+01 =============================================================== INSTANT 0.490000000E+01 TIME STEP NUMBER 98 ============================================================= Incoming flow detained for 338 outlet faces on 1690 TIME FOR THE TIME STEP 98: 0.64540E+01 =============================================================== INSTANT 0.495000000E+01 TIME STEP NUMBER 99 ============================================================= Incoming flow detained for 338 outlet faces on 1690 TIME FOR THE TIME STEP 99: 0.54364E+01 =============================================================== INSTANT 0.500000000E+01 TIME STEP NUMBER 100 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 358 -0.264069000E+01 Smooth wall 5 97490 0.860923203E-15 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 1690 0.260989567E+01 Free inlet 13 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : -0.11012E+04 0.24757E+05 Friction velocity uet : 0.76157E-02 0.73176E+03 Friction velocity uk : 0.21281E+00 0.13676E+05 Dimensionless distance yplus : 0.13711E+02 0.99521E+06 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 796 Nb of faces within the viscous sub-layer : 0 Total number of wall faces : 97490 ------------------------------------------------------------ Incoming flow detained for 338 outlet faces on 1690 Write intermediate restart files checkpoint at iteration 100, Physical time 0.50000E+01 ** Writing the main restart file ----------------------------- Start writing End writing the dimensions End writing the options End writing the main variables End writing ** Writing the auxiliary restart file ---------------------------------- Start writing End writing the dimensions and options End writing the physical properties End writing the time step End writing the mass fluxes End writing the boundary conditions End writing Time for restart files: 0.15564E+00 ** INFORMATION ON CONVERGENCE -------------------------- --------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual derive --------------------------------------------------------------- c VelocityX 0.46011E+06 621 0.87290E+00 0.32439E+06 c VelocityY 0.46011E+06 621 0.87290E+00 0.00000E+00 c VelocityZ 0.46011E+06 621 0.87290E+00 0.00000E+00 c Pressure 0.18021E+02 166 0.70687E-02 0.96983E-01 c k 0.32381E+11 52 0.30945E-02 0.60186E+14 c epsilon 0.27473E+17 36 0.83556E-02 0.85969E+26 --------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a epsilon a Local Time Step 2.8286e-05 38352 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ------------------- -------------- -------------- -------------- -------------- v Velocity[X] -15401 29969 -9.0598 9.7915 v Velocity[Y] -15207 23891 -4.9677 -3.4311 v Velocity[Z] -18934 21032 -2.866 0.79135 v ǁVelocityǁ 0.34613 30579 108.59 58.77 v Pressure -5.5134e+05 4.9608e+05 19804 23311 v k 0.00053038 9.5857e+08 1.864e+05 24225 v epsilon 1.3257 1.4041e+15 1.2133e+11 1.2115e+10 v turbulent_viscosity 1.9124e-10 40.652 0.042066 0.017977 v CourantNb 0.080547 62605 43.926 11.47 v FourierNb 0.0076814 30649 22.172 2.668 v total_pressure -4.5002e+05 5.9741e+05 1.2113e+05 1.2464e+05 v Local Time Step 0.0025 0.012644 0.0025049 0.0025087 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.23669 79428 66.098 14.138 TIME FOR THE TIME STEP 100: 0.69965E+01 =============================================================== INSTANT 0.505000000E+01 TIME STEP NUMBER 101 ============================================================= Incoming flow detained for 338 outlet faces on 1690 TIME FOR THE TIME STEP 101: 0.59076E+01 =============================================================== INSTANT 0.510000000E+01 TIME STEP NUMBER 102 ============================================================= Incoming flow detained for 338 outlet faces on 1690 TIME FOR THE TIME STEP 102: 0.57374E+01 =============================================================== INSTANT 0.515000000E+01 TIME STEP NUMBER 103 ============================================================= Incoming flow detained for 338 outlet faces on 1690 TIME FOR THE TIME STEP 103: 0.67938E+01 =============================================================== INSTANT 0.520000000E+01 TIME STEP NUMBER 104 ============================================================= Incoming flow detained for 338 outlet faces on 1690 TIME FOR THE TIME STEP 104: 0.60316E+01 =============================================================== INSTANT 0.525000000E+01 TIME STEP NUMBER 105 ============================================================= Incoming flow detained for 338 outlet faces on 1690 TIME FOR THE TIME STEP 105: 0.56891E+01 =============================================================== INSTANT 0.530000000E+01 TIME STEP NUMBER 106 ============================================================= Incoming flow detained for 338 outlet faces on 1690 TIME FOR THE TIME STEP 106: 0.75456E+01 =============================================================== INSTANT 0.535000000E+01 TIME STEP NUMBER 107 ============================================================= Incoming flow detained for 338 outlet faces on 1690 TIME FOR THE TIME STEP 107: 0.64373E+01 =============================================================== INSTANT 0.540000000E+01 TIME STEP NUMBER 108 ============================================================= Incoming flow detained for 338 outlet faces on 1690 TIME FOR THE TIME STEP 108: 0.59686E+01 =============================================================== INSTANT 0.545000000E+01 TIME STEP NUMBER 109 ============================================================= Incoming flow detained for 340 outlet faces on 1690 TIME FOR THE TIME STEP 109: 0.65793E+01 =============================================================== INSTANT 0.550000000E+01 TIME STEP NUMBER 110 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 358 -0.264069000E+01 Smooth wall 5 97490 0.458923493E-14 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 1690 0.257382145E+01 Free inlet 13 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : -0.47470E+04 0.59168E+05 Friction velocity uet : 0.13432E-01 0.16471E+04 Friction velocity uk : 0.23031E+00 0.32596E+05 Dimensionless distance yplus : 0.14595E+02 0.23860E+07 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 527 Nb of faces within the viscous sub-layer : 0 Total number of wall faces : 97490 ------------------------------------------------------------ Incoming flow detained for 339 outlet faces on 1690 ** INFORMATION ON CONVERGENCE -------------------------- --------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual derive --------------------------------------------------------------- c VelocityX 0.25505E+07 649 0.87139E+00 0.71721E+07 c VelocityY 0.25505E+07 649 0.87139E+00 0.00000E+00 c VelocityZ 0.25505E+07 649 0.87139E+00 0.00000E+00 c Pressure 0.44579E+02 139 0.72530E-02 0.99374E-01 c k 0.44387E+12 52 0.30674E-02 0.20477E+16 c epsilon 0.89257E+18 36 0.87468E-02 0.15759E+29 --------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a epsilon a Local Time Step 2.8269e-05 38352 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ------------------- -------------- -------------- -------------- -------------- v Velocity[X] -38112 69313 -8.3633 9.8202 v Velocity[Y] -36592 55638 -2.6141 -2.7087 v Velocity[Z] -46075 54109 -11.174 0.24277 v ǁVelocityǁ 0.080914 70786 177.26 85.473 v Pressure -1.3287e+06 1.1942e+06 33343 39142 v k 1.0858e-06 5.5281e+09 1.0774e+06 1.411e+05 v epsilon 0.0024743 1.9146e+16 1.6818e+12 1.6955e+11 v turbulent_viscosity 2.3252e-11 97.812 0.1062 0.059767 v CourantNb 0.092154 1.4775e+05 74.065 17.797 v FourierNb 0.0086398 74021 49.736 7.2913 v total_pressure -1.2274e+06 1.2956e+06 1.3467e+05 1.4047e+05 v Local Time Step 0.0025 0.0068274 0.0025066 0.0025093 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.13941 1.8801e+05 123.8 25.088 TIME FOR THE TIME STEP 110: 0.73431E+01 =============================================================== INSTANT 0.555000000E+01 TIME STEP NUMBER 111 ============================================================= Incoming flow detained for 338 outlet faces on 1690 TIME FOR THE TIME STEP 111: 0.80845E+01 =============================================================== INSTANT 0.560000000E+01 TIME STEP NUMBER 112 ============================================================= Incoming flow detained for 338 outlet faces on 1690 TIME FOR THE TIME STEP 112: 0.64312E+01 =============================================================== INSTANT 0.565000000E+01 TIME STEP NUMBER 113 ============================================================= Incoming flow detained for 339 outlet faces on 1690 TIME FOR THE TIME STEP 113: 0.69258E+01 =============================================================== INSTANT 0.570000000E+01 TIME STEP NUMBER 114 ============================================================= Incoming flow detained for 345 outlet faces on 1690 TIME FOR THE TIME STEP 114: 0.80495E+01 =============================================================== INSTANT 0.575000000E+01 TIME STEP NUMBER 115 ============================================================= Incoming flow detained for 339 outlet faces on 1690 TIME FOR THE TIME STEP 115: 0.69984E+01 =============================================================== INSTANT 0.580000000E+01 TIME STEP NUMBER 116 ============================================================= Incoming flow detained for 338 outlet faces on 1690 TIME FOR THE TIME STEP 116: 0.97417E+01 =============================================================== INSTANT 0.585000000E+01 TIME STEP NUMBER 117 ============================================================= Incoming flow detained for 349 outlet faces on 1690 TIME FOR THE TIME STEP 117: 0.99702E+01 =============================================================== INSTANT 0.590000000E+01 TIME STEP NUMBER 118 ============================================================= Incoming flow detained for 350 outlet faces on 1690 TIME FOR THE TIME STEP 118: 0.10586E+02 =============================================================== INSTANT 0.595000000E+01 TIME STEP NUMBER 119 ============================================================= Incoming flow detained for 346 outlet faces on 1690 TIME FOR THE TIME STEP 119: 0.98474E+01 =============================================================== INSTANT 0.600000000E+01 TIME STEP NUMBER 120 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 358 -0.264069000E+01 Smooth wall 5 97490 0.146884906E-13 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 1690 0.250198024E+01 Free inlet 13 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : -0.20836E+05 0.14166E+06 Friction velocity uet : 0.37189E-02 0.37262E+04 Friction velocity uk : 0.28873E+00 0.78022E+05 Dimensionless distance yplus : 0.18514E+02 0.57253E+07 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 355 Nb of faces within the viscous sub-layer : 0 Total number of wall faces : 97490 ------------------------------------------------------------ Incoming flow detained for 340 outlet faces on 1690 ** INFORMATION ON CONVERGENCE -------------------------- --------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual derive --------------------------------------------------------------- c VelocityX 0.14805E+08 680 0.86290E+00 0.68608E+08 c VelocityY 0.14805E+08 680 0.86290E+00 0.00000E+00 c VelocityZ 0.14805E+08 680 0.86290E+00 0.00000E+00 c Pressure 0.10910E+03 187 0.79726E-02 0.10064E+00 c k 0.61138E+13 52 0.29896E-02 0.67147E+17 c epsilon 0.29222E+20 36 0.87391E-02 0.30084E+31 --------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a epsilon a Local Time Step 2.8966e-05 38352 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ------------------- -------------- -------------- -------------- -------------- v Velocity[X] -88706 1.6437e+05 -11.197 8.01 v Velocity[Y] -88602 1.3415e+05 2.3489 -3.2918 v Velocity[Z] -1.071e+05 1.3576e+05 -24.754 -0.21853 v ǁVelocityǁ 0.85448 1.6796e+05 304.68 127.87 v Pressure -3.2716e+06 2.8098e+06 55121 67122 v k 3.0322e-08 3.1823e+10 6.197e+06 8.0843e+05 v epsilon 4.75e-06 2.6265e+17 2.3155e+13 2.3393e+12 v turbulent_viscosity 1.1235e-13 236.33 0.21403 0.079804 v CourantNb 0.12824 3.5024e+05 141.21 30.961 v FourierNb 0.010068 1.7822e+05 108.37 13.335 v total_pressure -3.1703e+06 2.9111e+06 1.5645e+05 1.6845e+05 v Local Time Step 0.0025 0.0034171 0.0025002 0.0025002 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.44354 4.4739e+05 249.58 44.296 TIME FOR THE TIME STEP 120: 0.10075E+02 =============================================================== INSTANT 0.605000000E+01 TIME STEP NUMBER 121 ============================================================= Incoming flow detained for 358 outlet faces on 1690 TIME FOR THE TIME STEP 121: 0.13195E+02 =============================================================== INSTANT 0.610000000E+01 TIME STEP NUMBER 122 ============================================================= Incoming flow detained for 352 outlet faces on 1690 TIME FOR THE TIME STEP 122: 0.98798E+01 =============================================================== INSTANT 0.615000000E+01 TIME STEP NUMBER 123 ============================================================= Incoming flow detained for 345 outlet faces on 1690 TIME FOR THE TIME STEP 123: 0.11455E+02 =============================================================== INSTANT 0.620000000E+01 TIME STEP NUMBER 124 ============================================================= Incoming flow detained for 360 outlet faces on 1690 TIME FOR THE TIME STEP 124: 0.94836E+01 =============================================================== INSTANT 0.625000000E+01 TIME STEP NUMBER 125 ============================================================= Incoming flow detained for 369 outlet faces on 1690 TIME FOR THE TIME STEP 125: 0.93854E+01 =============================================================== INSTANT 0.630000000E+01 TIME STEP NUMBER 126 ============================================================= Incoming flow detained for 365 outlet faces on 1690 TIME FOR THE TIME STEP 126: 0.85693E+01 =============================================================== INSTANT 0.635000000E+01 TIME STEP NUMBER 127 ============================================================= Incoming flow detained for 361 outlet faces on 1690 TIME FOR THE TIME STEP 127: 0.96273E+01 =============================================================== INSTANT 0.640000000E+01 TIME STEP NUMBER 128 ============================================================= Incoming flow detained for 394 outlet faces on 1690 TIME FOR THE TIME STEP 128: 0.95650E+01 =============================================================== INSTANT 0.645000000E+01 TIME STEP NUMBER 129 ============================================================= Incoming flow detained for 409 outlet faces on 1690 TIME FOR THE TIME STEP 129: 0.10554E+02 =============================================================== INSTANT 0.650000000E+01 TIME STEP NUMBER 130 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 358 -0.264069000E+01 Smooth wall 5 97490 0.619196169E-13 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 1690 0.206415767E+01 Free inlet 13 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : -0.51387E+05 0.34371E+06 Friction velocity uet : 0.22838E-01 0.90406E+04 Friction velocity uk : 0.58974E+00 0.18590E+06 Dimensionless distance yplus : 0.25734E+02 0.13666E+08 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 351 Nb of faces within the viscous sub-layer : 0 Total number of wall faces : 97490 ------------------------------------------------------------ Incoming flow detained for 384 outlet faces on 1690 ** INFORMATION ON CONVERGENCE -------------------------- --------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual derive --------------------------------------------------------------- c VelocityX 0.94768E+08 705 0.82437E+00 0.70786E+09 c VelocityY 0.94768E+08 705 0.82437E+00 0.00000E+00 c VelocityZ 0.94768E+08 705 0.82437E+00 0.00000E+00 c Pressure 0.28191E+03 210 0.10276E-01 0.10512E+00 c k 0.83544E+14 52 0.31338E-02 0.24378E+19 c epsilon 0.94470E+21 36 0.88170E-02 0.59767E+33 --------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a epsilon a Local Time Step 3.0321e-05 38352 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ------------------- -------------- -------------- -------------- -------------- v Velocity[X] -2.1672e+05 3.9442e+05 25.717 19.195 v Velocity[Y] -2.3242e+05 3.2208e+05 39.835 7.6356 v Velocity[Z] -2.6958e+05 3.9766e+05 -68.39 1.4458 v ǁVelocityǁ 1.2867 4.0296e+05 871.72 422.35 v Pressure -8.1149e+06 6.4736e+06 1.1432e+05 1.4412e+05 v k 6.666e-11 1.823e+11 3.6476e+07 4.8985e+06 v epsilon 1.0587e-08 3.5504e+18 3.2307e+14 3.3741e+13 v turbulent_viscosity 7.2539e-16 565.41 0.51813 0.20967 v CourantNb 0.08134 8.3315e+05 292.7 60.346 v FourierNb 0.011187 4.2801e+05 249.89 33.145 v total_pressure -8.0136e+06 6.5749e+06 2.1565e+05 2.4545e+05 v Local Time Step 0.0025 0.0033616 0.0025002 0.0025002 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.34336 1.0659e+06 542.59 93.491 TIME FOR THE TIME STEP 130: 0.99810E+01 =============================================================== INSTANT 0.655000000E+01 TIME STEP NUMBER 131 ============================================================= Incoming flow detained for 388 outlet faces on 1690 TIME FOR THE TIME STEP 131: 0.10497E+02 =============================================================== INSTANT 0.660000000E+01 TIME STEP NUMBER 132 ============================================================= Incoming flow detained for 386 outlet faces on 1690 TIME FOR THE TIME STEP 132: 0.12087E+02 =============================================================== INSTANT 0.665000000E+01 TIME STEP NUMBER 133 ============================================================= Incoming flow detained for 675 outlet faces on 1690 TIME FOR THE TIME STEP 133: 0.92791E+01 =============================================================== INSTANT 0.670000000E+01 TIME STEP NUMBER 134 ============================================================= Incoming flow detained for 531 outlet faces on 1690 TIME FOR THE TIME STEP 134: 0.10966E+02 =============================================================== INSTANT 0.675000000E+01 TIME STEP NUMBER 135 ============================================================= Incoming flow detained for 827 outlet faces on 1690 TIME FOR THE TIME STEP 135: 0.96652E+01 =============================================================== INSTANT 0.680000000E+01 TIME STEP NUMBER 136 ============================================================= Incoming flow detained for 537 outlet faces on 1690 TIME FOR THE TIME STEP 136: 0.11030E+02 =============================================================== INSTANT 0.685000000E+01 TIME STEP NUMBER 137 ============================================================= Incoming flow detained for 811 outlet faces on 1690 TIME FOR THE TIME STEP 137: 0.11468E+02 =============================================================== INSTANT 0.690000000E+01 TIME STEP NUMBER 138 ============================================================= Incoming flow detained for 590 outlet faces on 1690 TIME FOR THE TIME STEP 138: 0.12317E+02 =============================================================== INSTANT 0.695000000E+01 TIME STEP NUMBER 139 ============================================================= Incoming flow detained for 837 outlet faces on 1690 TIME FOR THE TIME STEP 139: 0.10717E+02 =============================================================== INSTANT 0.700000000E+01 TIME STEP NUMBER 140 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 358 -0.264069000E+01 Smooth wall 5 97490 0.337529421E-12 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 1690 -0.619200620E+00 Free inlet 13 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : -0.11768E+06 0.90941E+06 Friction velocity uet : 0.75402E-02 0.22588E+05 Friction velocity uk : 0.71179E+00 0.44386E+06 Dimensionless distance yplus : 0.26213E+02 0.32534E+08 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 339 Nb of faces within the viscous sub-layer : 0 Total number of wall faces : 97490 ------------------------------------------------------------ Incoming flow detained for 783 outlet faces on 1690 ** INFORMATION ON CONVERGENCE -------------------------- --------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual derive --------------------------------------------------------------- c VelocityX 0.64672E+09 919 0.79711E+00 0.80794E+10 c VelocityY 0.64672E+09 919 0.79711E+00 0.00000E+00 c VelocityZ 0.64672E+09 919 0.79711E+00 0.00000E+00 c Pressure 0.74031E+03 249 0.14446E-01 0.11009E+00 c k 0.11385E+16 52 0.30167E-02 0.71806E+20 c epsilon 0.30972E+23 36 0.84777E-02 0.11055E+36 --------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a epsilon a Local Time Step 3.2597e-05 38352 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ------------------- -------------- -------------- -------------- -------------- v Velocity[X] -5.4495e+05 9.3e+05 13.926 47.385 v Velocity[Y] -5.3977e+05 7.6084e+05 129.69 -8.031 v Velocity[Z] -6.9119e+05 1.1376e+06 -199.84 -40.263 v ǁVelocityǁ 0.88831 1.1486e+06 2774.8 1567.7 v Pressure -2.0879e+07 1.4665e+07 6.6639e+05 9.3259e+05 v k 1.8785e-13 1.0229e+12 2.1162e+08 2.8767e+07 v epsilon 3.4893e-11 4.8398e+19 4.4921e+15 4.8157e+14 v turbulent_viscosity 1.0641e-18 1347.8 1.474 0.75592 v CourantNb 0 1.9885e+06 817.21 195.94 v FourierNb 0.0081312 1.0205e+06 736.75 98.399 v total_pressure -2.0778e+07 1.4766e+07 7.6771e+05 1.0339e+06 v Local Time Step 0.0025 0.0033275 0.0025066 0.0025127 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.23659 2.5424e+06 1554 294.34 TIME FOR THE TIME STEP 140: 0.13090E+02 =============================================================== INSTANT 0.705000000E+01 TIME STEP NUMBER 141 ============================================================= Incoming flow detained for 827 outlet faces on 1690 TIME FOR THE TIME STEP 141: 0.17697E+02 =============================================================== INSTANT 0.710000000E+01 TIME STEP NUMBER 142 ============================================================= Incoming flow detained for 747 outlet faces on 1690 TIME FOR THE TIME STEP 142: 0.13358E+02 =============================================================== INSTANT 0.715000000E+01 TIME STEP NUMBER 143 ============================================================= Incoming flow detained for 745 outlet faces on 1690 TIME FOR THE TIME STEP 143: 0.14335E+02 =============================================================== INSTANT 0.720000000E+01 TIME STEP NUMBER 144 ============================================================= Incoming flow detained for 763 outlet faces on 1690 TIME FOR THE TIME STEP 144: 0.12912E+02 =============================================================== INSTANT 0.725000000E+01 TIME STEP NUMBER 145 ============================================================= Incoming flow detained for 765 outlet faces on 1690 TIME FOR THE TIME STEP 145: 0.11822E+02 =============================================================== INSTANT 0.730000000E+01 TIME STEP NUMBER 146 ============================================================= Incoming flow detained for 759 outlet faces on 1690 TIME FOR THE TIME STEP 146: 0.13619E+02 =============================================================== INSTANT 0.735000000E+01 TIME STEP NUMBER 147 ============================================================= Incoming flow detained for 669 outlet faces on 1690 TIME FOR THE TIME STEP 147: 0.15489E+02 =============================================================== INSTANT 0.740000000E+01 TIME STEP NUMBER 148 ============================================================= Incoming flow detained for 780 outlet faces on 1690 TIME FOR THE TIME STEP 148: 0.11867E+02 =============================================================== INSTANT 0.745000000E+01 TIME STEP NUMBER 149 ============================================================= Incoming flow detained for 876 outlet faces on 1690 TIME FOR THE TIME STEP 149: 0.14469E+02 =============================================================== INSTANT 0.750000000E+01 TIME STEP NUMBER 150 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 358 -0.264069000E+01 Smooth wall 5 97490 0.800699762E-12 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 1690 -0.320128915E+01 Free inlet 13 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : -0.19416E+06 0.25646E+07 Friction velocity uet : 0.35492E-02 0.60670E+05 Friction velocity uk : 0.83239E+00 0.10548E+07 Dimensionless distance yplus : 0.26216E+02 0.77389E+08 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 374 Nb of faces within the viscous sub-layer : 0 Total number of wall faces : 97490 ------------------------------------------------------------ Incoming flow detained for 780 outlet faces on 1690 ** INFORMATION ON CONVERGENCE -------------------------- --------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual derive --------------------------------------------------------------- c VelocityX 0.40832E+10 1190 0.79366E+00 0.57596E+11 c VelocityY 0.40832E+10 1190 0.79366E+00 0.00000E+00 c VelocityZ 0.40832E+10 1190 0.79366E+00 0.00000E+00 c Pressure 0.18858E+04 248 0.12260E-01 0.11189E+00 c k 0.15265E+17 52 0.31207E-02 0.24848E+22 c epsilon 0.99706E+24 36 0.82721E-02 0.20725E+38 --------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a epsilon a Local Time Step 2.7449e-05 38243 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ------------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.5849e+06 2.2374e+06 -3.0089 33.325 v Velocity[Y] -1.4787e+06 1.8397e+06 336.04 -65.453 v Velocity[Z] -1.6026e+06 3.3248e+06 64.604 -75.859 v ǁVelocityǁ 1.2056 3.3634e+06 6472.1 3456.1 v Pressure -5.1289e+07 3.5299e+07 6.6142e+05 9.4872e+05 v k 2.0377e-10 5.7424e+12 1.2214e+09 1.7009e+08 v epsilon 1.3139e-05 6.491e+20 6.116e+16 6.6735e+15 v turbulent_viscosity 1.2804e-16 3164.5 4.0003 2.0939 v CourantNb 0 4.758e+06 1744.5 405.79 v FourierNb 0.012292 2.424e+06 2402.3 257.9 v total_pressure -5.1188e+07 3.5401e+07 7.6274e+05 1.05e+06 v Local Time Step 0.0025 0.0033275 0.0025032 0.0025063 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.30099 6.0623e+06 4146.7 663.69 TIME FOR THE TIME STEP 150: 0.15366E+02 =============================================================== INSTANT 0.755000000E+01 TIME STEP NUMBER 151 ============================================================= Incoming flow detained for 890 outlet faces on 1690 TIME FOR THE TIME STEP 151: 0.17189E+02 =============================================================== INSTANT 0.760000000E+01 TIME STEP NUMBER 152 ============================================================= Incoming flow detained for 800 outlet faces on 1690 TIME FOR THE TIME STEP 152: 0.14573E+02 =============================================================== INSTANT 0.765000000E+01 TIME STEP NUMBER 153 ============================================================= Incoming flow detained for 554 outlet faces on 1690 TIME FOR THE TIME STEP 153: 0.14240E+02 =============================================================== INSTANT 0.770000000E+01 TIME STEP NUMBER 154 ============================================================= Incoming flow detained for 746 outlet faces on 1690 TIME FOR THE TIME STEP 154: 0.17235E+02 =============================================================== INSTANT 0.775000000E+01 TIME STEP NUMBER 155 ============================================================= Incoming flow detained for 871 outlet faces on 1690 TIME FOR THE TIME STEP 155: 0.13439E+02 =============================================================== INSTANT 0.780000000E+01 TIME STEP NUMBER 156 ============================================================= Incoming flow detained for 800 outlet faces on 1690 TIME FOR THE TIME STEP 156: 0.13818E+02 =============================================================== INSTANT 0.785000000E+01 TIME STEP NUMBER 157 ============================================================= Incoming flow detained for 722 outlet faces on 1690 TIME FOR THE TIME STEP 157: 0.12720E+02 =============================================================== INSTANT 0.790000000E+01 TIME STEP NUMBER 158 ============================================================= Incoming flow detained for 771 outlet faces on 1690 TIME FOR THE TIME STEP 158: 0.10901E+02 =============================================================== INSTANT 0.795000000E+01 TIME STEP NUMBER 159 ============================================================= Incoming flow detained for 878 outlet faces on 1690 TIME FOR THE TIME STEP 159: 0.15104E+02 =============================================================== INSTANT 0.800000000E+01 TIME STEP NUMBER 160 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 358 -0.264069000E+01 Smooth wall 5 97490 0.282800478E-11 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 1690 -0.145491697E+02 Free inlet 13 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : -0.28963E+04 0.75961E+07 Friction velocity uet : 0.26618E-01 0.16743E+06 Friction velocity uk : 0.88420E+00 0.24982E+07 Dimensionless distance yplus : 0.26222E+02 0.18223E+09 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 159 Nb of faces within the viscous sub-layer : 0 Total number of wall faces : 97490 ------------------------------------------------------------ Incoming flow detained for 809 outlet faces on 1690 ** INFORMATION ON CONVERGENCE -------------------------- --------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual derive --------------------------------------------------------------- c VelocityX 0.27929E+11 1409 0.74543E+00 0.30214E+12 c VelocityY 0.27929E+11 1409 0.74543E+00 0.00000E+00 c VelocityZ 0.27929E+11 1409 0.74543E+00 0.00000E+00 c Pressure 0.50729E+04 260 0.10403E-01 0.11782E+00 c k 0.20908E+18 52 0.31169E-02 0.90127E+23 c epsilon 0.36053E+26 36 0.73312E-02 0.53297E+40 --------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a epsilon a Local Time Step 1.0137e-06 38319 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ------------------- -------------- -------------- -------------- -------------- v Velocity[X] -3.978e+06 5.17e+06 274.06 -100.59 v Velocity[Y] -4.7038e+06 4.3531e+06 -88.004 -366.02 v Velocity[Z] -4.7381e+06 9.1683e+06 -434.83 20.677 v ǁVelocityǁ 0.99605 9.1929e+06 13312 6647.3 v Pressure -1.2356e+08 8.7127e+07 1.5391e+07 2.0751e+07 v k 2.4371 3.1899e+13 7.2522e+09 1.0471e+09 v epsilon 47.18 8.6567e+21 8.7418e+17 1.0412e+17 v turbulent_viscosity 0.00013264 7451.2 12.438 6.1552 v CourantNb 0 1.1352e+07 5591 1453.5 v FourierNb 0.032558 5.6754e+06 9261.8 751.07 v total_pressure -1.2345e+08 8.7229e+07 1.5492e+07 2.0853e+07 v Local Time Step 0.0025 0.003025 0.0025001 0.0025001 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.53452 1.443e+07 14853 2204.6 TIME FOR THE TIME STEP 160: 0.15840E+02 =============================================================== INSTANT 0.805000000E+01 TIME STEP NUMBER 161 ============================================================= Incoming flow detained for 862 outlet faces on 1690 TIME FOR THE TIME STEP 161: 0.13465E+02 =============================================================== INSTANT 0.810000000E+01 TIME STEP NUMBER 162 ============================================================= Incoming flow detained for 809 outlet faces on 1690 TIME FOR THE TIME STEP 162: 0.16064E+02 =============================================================== INSTANT 0.815000000E+01 TIME STEP NUMBER 163 ============================================================= Incoming flow detained for 545 outlet faces on 1690 TIME FOR THE TIME STEP 163: 0.15210E+02 =============================================================== INSTANT 0.820000000E+01 TIME STEP NUMBER 164 ============================================================= Incoming flow detained for 793 outlet faces on 1690 TIME FOR THE TIME STEP 164: 0.15528E+02 =============================================================== INSTANT 0.825000000E+01 TIME STEP NUMBER 165 ============================================================= Incoming flow detained for 617 outlet faces on 1690 TIME FOR THE TIME STEP 165: 0.15043E+02 =============================================================== INSTANT 0.830000000E+01 TIME STEP NUMBER 166 ============================================================= Incoming flow detained for 809 outlet faces on 1690 TIME FOR THE TIME STEP 166: 0.18829E+02 =============================================================== INSTANT 0.835000000E+01 TIME STEP NUMBER 167 ============================================================= Incoming flow detained for 650 outlet faces on 1690 TIME FOR THE TIME STEP 167: 0.14086E+02 =============================================================== INSTANT 0.840000000E+01 TIME STEP NUMBER 168 ============================================================= Incoming flow detained for 843 outlet faces on 1690 TIME FOR THE TIME STEP 168: 0.14859E+02 =============================================================== INSTANT 0.845000000E+01 TIME STEP NUMBER 169 ============================================================= Incoming flow detained for 712 outlet faces on 1690 TIME FOR THE TIME STEP 169: 0.13393E+02 =============================================================== INSTANT 0.850000000E+01 TIME STEP NUMBER 170 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 358 -0.264069000E+01 Smooth wall 5 97490 0.445274599E-11 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 1690 -0.455590300E+02 Free inlet 13 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : -0.20846E+06 0.22100E+08 Friction velocity uet : 0.95665E-02 0.45980E+06 Friction velocity uk : 0.12883E+01 0.59725E+07 Dimensionless distance yplus : 0.26233E+02 0.54168E+09 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 1836 Nb of faces within the viscous sub-layer : 0 Total number of wall faces : 97490 ------------------------------------------------------------ Incoming flow detained for 907 outlet faces on 1690 ** INFORMATION ON CONVERGENCE -------------------------- --------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual derive --------------------------------------------------------------- c VelocityX 0.20379E+12 2263 0.70628E+00 0.32189E+13 c VelocityY 0.20379E+12 2263 0.70628E+00 0.00000E+00 c VelocityZ 0.20379E+12 2263 0.70628E+00 0.00000E+00 c Pressure 0.12838E+05 358 0.15745E-01 0.11399E+00 c k 0.33176E+19 52 0.32223E-02 0.40071E+25 c epsilon 0.20219E+28 34 0.48808E-02 0.22158E+43 --------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a epsilon a Local Time Step 7.9347e-07 35987 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ------------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.1635e+07 1.2006e+07 4306.3 795.29 v Velocity[Y] -1.4283e+07 1.0365e+07 -1174.9 -2580.5 v Velocity[Z] -1.2556e+07 2.5558e+07 -799.96 -50.915 v ǁVelocityǁ 4.584 2.5823e+07 63040 25873 v Pressure -3.9094e+08 2.9895e+08 3.2473e+07 4.7051e+07 v k 6.7402 1.8368e+14 4.9158e+10 7.2585e+09 v epsilon 146.08 1.4206e+23 1.4158e+19 1.9052e+18 v turbulent_viscosity 5.5082e-10 17908 45.719 19.397 v CourantNb 0 2.7009e+07 15914 4270.1 v FourierNb 0.0031284 1.3754e+07 45785 2381.2 v total_pressure -3.9084e+08 2.9906e+08 3.2574e+07 4.7153e+07 v Local Time Step 0.0025 0.003025 0.0025018 0.0025042 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.36337 3.4397e+07 61699 6651.3 TIME FOR THE TIME STEP 170: 0.24958E+02 =============================================================== INSTANT 0.855000000E+01 TIME STEP NUMBER 171 ============================================================= Incoming flow detained for 726 outlet faces on 1690 TIME FOR THE TIME STEP 171: 0.12435E+02 =============================================================== INSTANT 0.860000000E+01 TIME STEP NUMBER 172 ============================================================= Incoming flow detained for 950 outlet faces on 1690 TIME FOR THE TIME STEP 172: 0.12667E+02 =============================================================== INSTANT 0.865000000E+01 TIME STEP NUMBER 173 ============================================================= Incoming flow detained for 740 outlet faces on 1690 TIME FOR THE TIME STEP 173: 0.12156E+02 =============================================================== INSTANT 0.870000000E+01 TIME STEP NUMBER 174 ============================================================= Incoming flow detained for 921 outlet faces on 1690 TIME FOR THE TIME STEP 174: 0.12157E+02 =============================================================== INSTANT 0.875000000E+01 TIME STEP NUMBER 175 ============================================================= Incoming flow detained for 830 outlet faces on 1690 TIME FOR THE TIME STEP 175: 0.14800E+02 =============================================================== INSTANT 0.880000000E+01 TIME STEP NUMBER 176 ============================================================= Incoming flow detained for 860 outlet faces on 1690 TIME FOR THE TIME STEP 176: 0.13953E+02 =============================================================== INSTANT 0.885000000E+01 TIME STEP NUMBER 177 ============================================================= Incoming flow detained for 830 outlet faces on 1690 TIME FOR THE TIME STEP 177: 0.13827E+02 =============================================================== INSTANT 0.890000000E+01 TIME STEP NUMBER 178 ============================================================= Incoming flow detained for 848 outlet faces on 1690 TIME FOR THE TIME STEP 178: 0.17023E+02 =============================================================== INSTANT 0.895000000E+01 TIME STEP NUMBER 179 ============================================================= Incoming flow detained for 911 outlet faces on 1690 TIME FOR THE TIME STEP 179: 0.89982E+01 =============================================================== INSTANT 0.900000000E+01 TIME STEP NUMBER 180 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 358 -0.264069000E+01 Smooth wall 5 97490 0.115155423E-10 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 1690 -0.116209583E+03 Free inlet 13 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : -0.28516E+05 0.56786E+08 Friction velocity uet : 0.77338E-02 0.11426E+07 Friction velocity uk : 0.13390E+01 0.14227E+08 Dimensionless distance yplus : 0.26400E+02 0.12593E+10 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 5 Nb of faces within the viscous sub-layer : 0 Total number of wall faces : 97490 ------------------------------------------------------------ Incoming flow detained for 774 outlet faces on 1690 ** INFORMATION ON CONVERGENCE -------------------------- --------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual derive --------------------------------------------------------------- c VelocityX 0.12260E+13 1548 0.70976E+00 0.89469E+13 c VelocityY 0.12260E+13 1548 0.70976E+00 0.00000E+00 c VelocityZ 0.12260E+13 1548 0.70976E+00 0.00000E+00 c Pressure 0.33411E+05 395 0.16211E-01 0.11570E+00 c k 0.44324E+20 52 0.29459E-02 0.12673E+27 c epsilon 0.66282E+29 33 0.44121E-02 0.36583E+45 --------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a epsilon a Local Time Step 1.5272e-07 37229 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ------------------- -------------- -------------- -------------- -------------- v Velocity[X] -3.5227e+07 2.8578e+07 5154.1 -941.8 v Velocity[Y] -3.665e+07 2.4709e+07 -2656.6 -5852.1 v Velocity[Z] -3.8218e+07 6.1636e+07 -2428.6 -35.518 v ǁVelocityǁ 1.4595 6.2095e+07 1.3465e+05 55472 v Pressure -1.1644e+09 7.6018e+08 3.4564e+07 6.8422e+07 v k 6.5469 1.0405e+15 2.608e+11 3.8692e+10 v epsilon 138.64 1.7957e+24 1.8948e+20 2.4923e+19 v turbulent_viscosity 0.00090265 42703 102.52 74.211 v CourantNb 0 6.4281e+07 31012 7779.3 v FourierNb 0.22355 3.2819e+07 66669 7180.6 v total_pressure -1.1643e+09 7.6028e+08 3.4665e+07 6.8524e+07 v Local Time Step 0.0025 0.00275 0.0025009 0.002502 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 0.41607 8.1893e+07 97681 14960 TIME FOR THE TIME STEP 180: 0.16041E+02 =============================================================== INSTANT 0.905000000E+01 TIME STEP NUMBER 181 ============================================================= Incoming flow detained for 929 outlet faces on 1690 TIME FOR THE TIME STEP 181: 0.12428E+02 =============================================================== INSTANT 0.910000000E+01 TIME STEP NUMBER 182 ============================================================= Incoming flow detained for 757 outlet faces on 1690 TIME FOR THE TIME STEP 182: 0.16301E+02 =============================================================== INSTANT 0.915000000E+01 TIME STEP NUMBER 183 ============================================================= Incoming flow detained for 955 outlet faces on 1690 TIME FOR THE TIME STEP 183: 0.16576E+02 =============================================================== INSTANT 0.920000000E+01 TIME STEP NUMBER 184 ============================================================= Incoming flow detained for 704 outlet faces on 1690 TIME FOR THE TIME STEP 184: 0.11108E+02 =============================================================== INSTANT 0.925000000E+01 TIME STEP NUMBER 185 ============================================================= Incoming flow detained for 964 outlet faces on 1690 TIME FOR THE TIME STEP 185: 0.15641E+02 =============================================================== INSTANT 0.930000000E+01 TIME STEP NUMBER 186 ============================================================= Incoming flow detained for 692 outlet faces on 1690 TIME FOR THE TIME STEP 186: 0.99131E+01 =============================================================== INSTANT 0.935000000E+01 TIME STEP NUMBER 187 ============================================================= Incoming flow detained for 974 outlet faces on 1690 TIME FOR THE TIME STEP 187: 0.11216E+02 =============================================================== INSTANT 0.940000000E+01 TIME STEP NUMBER 188 ============================================================= Incoming flow detained for 710 outlet faces on 1690 TIME FOR THE TIME STEP 188: 0.10833E+02 =============================================================== INSTANT 0.945000000E+01 TIME STEP NUMBER 189 ============================================================= Incoming flow detained for 980 outlet faces on 1690 TIME FOR THE TIME STEP 189: 0.91636E+01 =============================================================== INSTANT 0.950000000E+01 TIME STEP NUMBER 190 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 358 -0.264069000E+01 Smooth wall 5 97490 0.517018095E-10 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 1690 0.277345677E+03 Free inlet 13 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : -0.92616E+06 0.15465E+09 Friction velocity uet : 0.40220E+00 0.29606E+07 Friction velocity uk : 0.14926E+01 0.36827E+08 Dimensionless distance yplus : 0.27459E+02 0.34346E+10 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 11 Nb of faces within the viscous sub-layer : 0 Total number of wall faces : 97490 ------------------------------------------------------------ Incoming flow detained for 710 outlet faces on 1690 ** INFORMATION ON CONVERGENCE -------------------------- --------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual derive --------------------------------------------------------------- c VelocityX 0.99493E+13 1138 0.70248E+00 0.85630E+14 c VelocityY 0.99493E+13 1138 0.70248E+00 0.00000E+00 c VelocityZ 0.99493E+13 1138 0.70248E+00 0.00000E+00 c Pressure 0.87216E+05 353 0.12438E-01 0.11552E+00 c k 0.70307E+21 51 0.25010E-02 0.43046E+28 c epsilon 0.31736E+31 32 0.33566E-02 0.97904E+47 --------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a epsilon -2.8145e+10 3 a Local Time Step 1.9873e-07 38352 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ------------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.7565e+07 6.8471e+07 18064 -2142 v Velocity[Y] -8.3803e+07 6.4055e+07 -8165.6 -9424.3 v Velocity[Z] -1.1837e+08 1.6342e+08 -20242 -123.45 v ǁVelocityǁ 1.7502 1.6462e+08 2.7845e+05 1.3533e+05 v Pressure -3.1024e+09 1.8189e+09 1.7249e+07 7.0384e+07 v k 6.3139 5.873e+15 1.5591e+12 2.4268e+11 v epsilon 131.7 3.4902e+25 2.8213e+21 3.9826e+20 v turbulent_viscosity 0.00019449 1.0224e+05 239.74 169.9 v CourantNb 1.5046 1.5415e+08 85049 27210 v FourierNb 0.057693 7.8636e+07 1.7033e+05 16161 v total_pressure -3.1023e+09 1.8191e+09 1.735e+07 7.0486e+07 v Local Time Step 0.0025 0.0025 0.0025 0.0025 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.6687 1.9642e+08 2.5538e+05 43371 TIME FOR THE TIME STEP 190: 0.93045E+01 =============================================================== INSTANT 0.955000000E+01 TIME STEP NUMBER 191 ============================================================= Incoming flow detained for 980 outlet faces on 1690 TIME FOR THE TIME STEP 191: 0.11348E+02 =============================================================== INSTANT 0.960000000E+01 TIME STEP NUMBER 192 ============================================================= Incoming flow detained for 683 outlet faces on 1690 TIME FOR THE TIME STEP 192: 0.12519E+02 =============================================================== INSTANT 0.965000000E+01 TIME STEP NUMBER 193 ============================================================= Incoming flow detained for 957 outlet faces on 1690 TIME FOR THE TIME STEP 193: 0.14342E+02 =============================================================== INSTANT 0.970000000E+01 TIME STEP NUMBER 194 ============================================================= Incoming flow detained for 730 outlet faces on 1690 TIME FOR THE TIME STEP 194: 0.82727E+01 =============================================================== INSTANT 0.975000000E+01 TIME STEP NUMBER 195 ============================================================= Incoming flow detained for 980 outlet faces on 1690 TIME FOR THE TIME STEP 195: 0.17117E+02 =============================================================== INSTANT 0.980000000E+01 TIME STEP NUMBER 196 ============================================================= Incoming flow detained for 710 outlet faces on 1690 TIME FOR THE TIME STEP 196: 0.91672E+01 =============================================================== INSTANT 0.985000000E+01 TIME STEP NUMBER 197 ============================================================= Incoming flow detained for 980 outlet faces on 1690 TIME FOR THE TIME STEP 197: 0.13799E+02 =============================================================== INSTANT 0.990000000E+01 TIME STEP NUMBER 198 ============================================================= Incoming flow detained for 720 outlet faces on 1690 TIME FOR THE TIME STEP 198: 0.84514E+01 =============================================================== INSTANT 0.995000000E+01 TIME STEP NUMBER 199 ============================================================= Incoming flow detained for 961 outlet faces on 1690 TIME FOR THE TIME STEP 199: 0.13159E+02 =============================================================== INSTANT 0.100000000E+02 TIME STEP NUMBER 200 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 358 -0.264069000E+01 Smooth wall 5 97490 0.941870751E-10 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 1690 -0.816918285E+03 Free inlet 13 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : -0.65582E+07 0.44683E+09 Friction velocity uet : 0.42966E+00 0.81574E+07 Friction velocity uk : 0.66169E+02 0.10765E+09 Dimensionless distance yplus : 0.12795E+04 0.94919E+10 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 44 Nb of faces within the viscous sub-layer : 0 Total number of wall faces : 97490 ------------------------------------------------------------ Incoming flow detained for 729 outlet faces on 1690 Write intermediate restart files checkpoint at iteration 200, Physical time 0.10000E+02 ** Writing the main restart file ----------------------------- Start writing End writing the dimensions End writing the options End writing the main variables End writing ** Writing the auxiliary restart file ---------------------------------- Start writing End writing the dimensions and options End writing the physical properties End writing the time step End writing the mass fluxes End writing the boundary conditions End writing Time for restart files: 0.16982E+00 ** INFORMATION ON CONVERGENCE -------------------------- --------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual derive --------------------------------------------------------------- c VelocityX 0.79480E+14 1701 0.75836E+00 0.99477E+15 c VelocityY 0.79480E+14 1701 0.75836E+00 0.00000E+00 c VelocityZ 0.79480E+14 1701 0.75836E+00 0.00000E+00 c Pressure 0.24544E+06 502 0.21631E-01 0.12294E+00 c k 0.13408E+23 49 0.36651E-02 0.39021E+30 c epsilon 0.19959E+33 29 0.29732E-02 0.11354E+51 --------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a epsilon a Local Time Step 3.6911e-08 38352 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ------------------- -------------- -------------- -------------- -------------- v Velocity[X] -3.0447e+08 1.617e+08 -3883.3 18940 v Velocity[Y] -2.4502e+08 1.421e+08 61048 -12723 v Velocity[Z] -3.3311e+08 4.673e+08 -82921 -1690.1 v ǁVelocityǁ 37.333 4.7482e+08 9.7881e+05 5.4186e+05 v Pressure -1.0108e+10 4.1365e+09 -2.0879e+08 -1.738e+08 v k 31622 5.4021e+16 1.0018e+13 1.7117e+12 v epsilon 8.8292e+07 9.8836e+26 5.0085e+22 8.1627e+21 v turbulent_viscosity 5.72e-06 2.425e+05 598.25 475.89 v CourantNb 2.0822 3.654e+08 2.0923e+05 63762 v FourierNb 1.9351 1.868e+08 3.1898e+05 44672 v total_pressure -1.0108e+10 4.1366e+09 -2.0869e+08 -1.737e+08 v Local Time Step 0.0025 0.0025 0.0025 0.0025 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 45.474 4.6524e+08 5.2821e+05 1.0843e+05 TIME FOR THE TIME STEP 200: 0.13760E+02 =============================================================== INSTANT 0.100500000E+02 TIME STEP NUMBER 201 ============================================================= Incoming flow detained for 967 outlet faces on 1690 TIME FOR THE TIME STEP 201: 0.86486E+01 =============================================================== INSTANT 0.101000000E+02 TIME STEP NUMBER 202 ============================================================= Incoming flow detained for 723 outlet faces on 1690 TIME FOR THE TIME STEP 202: 0.73086E+01 =============================================================== INSTANT 0.101500000E+02 TIME STEP NUMBER 203 ============================================================= Incoming flow detained for 967 outlet faces on 1690 TIME FOR THE TIME STEP 203: 0.13925E+02 =============================================================== INSTANT 0.102000000E+02 TIME STEP NUMBER 204 ============================================================= Incoming flow detained for 674 outlet faces on 1690 TIME FOR THE TIME STEP 204: 0.86218E+01 =============================================================== INSTANT 0.102500000E+02 TIME STEP NUMBER 205 ============================================================= Incoming flow detained for 935 outlet faces on 1690 TIME FOR THE TIME STEP 205: 0.11057E+02 =============================================================== INSTANT 0.103000000E+02 TIME STEP NUMBER 206 ============================================================= Incoming flow detained for 721 outlet faces on 1690 TIME FOR THE TIME STEP 206: 0.20011E+02 =============================================================== INSTANT 0.103500000E+02 TIME STEP NUMBER 207 ============================================================= Incoming flow detained for 968 outlet faces on 1690 TIME FOR THE TIME STEP 207: 0.13294E+02 =============================================================== INSTANT 0.104000000E+02 TIME STEP NUMBER 208 ============================================================= Incoming flow detained for 719 outlet faces on 1690 TIME FOR THE TIME STEP 208: 0.10666E+02 =============================================================== INSTANT 0.104500000E+02 TIME STEP NUMBER 209 ============================================================= Incoming flow detained for 971 outlet faces on 1690 TIME FOR THE TIME STEP 209: 0.14940E+02 =============================================================== INSTANT 0.105000000E+02 TIME STEP NUMBER 210 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 358 -0.264069000E+01 Smooth wall 5 97490 0.352700110E-09 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 1690 -0.225686068E+04 Free inlet 13 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : -0.10616E+06 0.11695E+10 Friction velocity uet : 0.69633E+01 0.20418E+08 Friction velocity uk : 0.27127E+03 0.30602E+09 Dimensionless distance yplus : 0.11039E+05 0.28541E+11 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 67 Nb of faces within the viscous sub-layer : 0 Total number of wall faces : 97490 ------------------------------------------------------------ Incoming flow detained for 719 outlet faces on 1690 ** INFORMATION ON CONVERGENCE -------------------------- --------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual derive --------------------------------------------------------------- c VelocityX 0.55153E+15 802 0.69556E+00 0.76006E+16 c VelocityY 0.55153E+15 802 0.69556E+00 0.00000E+00 c VelocityZ 0.55153E+15 802 0.69556E+00 0.00000E+00 c Pressure 0.66302E+06 308 0.22342E-01 0.12456E+00 c k 0.27148E+24 46 0.20009E-02 0.84566E+31 c epsilon 0.12991E+35 26 0.16382E-02 0.21081E+53 --------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a epsilon a Local Time Step 1.1302e-08 38352 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ------------------- -------------- -------------- -------------- -------------- v Velocity[X] -6.0675e+08 3.7973e+08 -18751 13190 v Velocity[Y] -6.6299e+08 3.8135e+08 90832 -347.25 v Velocity[Z] -7.4777e+08 1.3329e+09 -1.281e+05 -30437 v ǁVelocityǁ 189.47 1.3459e+09 2.3203e+06 1.4237e+06 v Pressure -2.8475e+10 9.5037e+09 -2.0116e+09 -2.6024e+09 v k 98659 3.6245e+17 5.9516e+13 1.0679e+13 v epsilon 6.6381e+10 1.8858e+28 8.2651e+23 1.4556e+23 v turbulent_viscosity 0.00066942 5.7739e+05 1835 1691.7 v CourantNb 39.078 9.9441e+08 4.7858e+05 1.4436e+05 v FourierNb 0.64566 4.4522e+08 1.0481e+06 1.4211e+05 v total_pressure -2.8475e+10 9.5038e+09 -2.0115e+09 -2.6023e+09 v Local Time Step 0.0025 0.0025 0.0025 0.0025 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 406.98 1.137e+09 1.5267e+06 2.8647e+05 TIME FOR THE TIME STEP 210: 0.80763E+01 =============================================================== INSTANT 0.105500000E+02 TIME STEP NUMBER 211 ============================================================= Incoming flow detained for 1155 outlet faces on 1690 TIME FOR THE TIME STEP 211: 0.14704E+02 =============================================================== INSTANT 0.106000000E+02 TIME STEP NUMBER 212 ============================================================= Incoming flow detained for 711 outlet faces on 1690 TIME FOR THE TIME STEP 212: 0.68119E+01 =============================================================== INSTANT 0.106500000E+02 TIME STEP NUMBER 213 ============================================================= Incoming flow detained for 1012 outlet faces on 1690 TIME FOR THE TIME STEP 213: 0.12521E+02 =============================================================== INSTANT 0.107000000E+02 TIME STEP NUMBER 214 ============================================================= Incoming flow detained for 765 outlet faces on 1690 TIME FOR THE TIME STEP 214: 0.17636E+02 =============================================================== INSTANT 0.107500000E+02 TIME STEP NUMBER 215 ============================================================= Incoming flow detained for 975 outlet faces on 1690 TIME FOR THE TIME STEP 215: 0.17575E+02 =============================================================== INSTANT 0.108000000E+02 TIME STEP NUMBER 216 ============================================================= Incoming flow detained for 709 outlet faces on 1690 TIME FOR THE TIME STEP 216: 0.93417E+01 =============================================================== INSTANT 0.108500000E+02 TIME STEP NUMBER 217 ============================================================= Incoming flow detained for 981 outlet faces on 1690 TIME FOR THE TIME STEP 217: 0.13274E+02 =============================================================== INSTANT 0.109000000E+02 TIME STEP NUMBER 218 ============================================================= Incoming flow detained for 709 outlet faces on 1690 TIME FOR THE TIME STEP 218: 0.10172E+02 =============================================================== INSTANT 0.109500000E+02 TIME STEP NUMBER 219 ============================================================= Incoming flow detained for 980 outlet faces on 1690 TIME FOR THE TIME STEP 219: 0.12220E+02 =============================================================== INSTANT 0.110000000E+02 TIME STEP NUMBER 220 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 358 -0.264069000E+01 Smooth wall 5 97490 0.135319527E-09 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 1690 -0.519765266E+04 Free inlet 13 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : -0.16980E+07 0.29371E+10 Friction velocity uet : 0.27362E+01 0.49522E+08 Friction velocity uk : 0.55915E+02 0.72035E+09 Dimensionless distance yplus : 0.62339E+04 0.67183E+11 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 381 Nb of faces within the viscous sub-layer : 0 Total number of wall faces : 97490 ------------------------------------------------------------ Incoming flow detained for 710 outlet faces on 1690 ** INFORMATION ON CONVERGENCE -------------------------- --------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual derive --------------------------------------------------------------- c VelocityX 0.38210E+16 1343 0.68015E+00 0.28961E+17 c VelocityY 0.38210E+16 1343 0.68015E+00 0.00000E+00 c VelocityZ 0.38210E+16 1343 0.68015E+00 0.00000E+00 c Pressure 0.16813E+07 252 0.16075E-01 0.12172E+00 c k 0.38948E+25 45 0.28788E-02 0.42959E+33 c epsilon 0.45301E+36 26 0.22336E-02 0.50919E+55 --------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a epsilon -9.8561e+14 2 a Local Time Step 8.122e-09 38352 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ------------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.8571e+09 1.0139e+09 -93584 -56215 v Velocity[Y] -1.8688e+09 1.2595e+09 -91378 -1.4792e+05 v Velocity[Z] -1.9096e+09 3.5408e+09 -1.3287e+05 -88127 v ǁVelocityǁ 93.274 3.5686e+09 4.7443e+06 2.8644e+06 v Pressure -5.876e+10 3.2396e+10 4.5389e+09 6.2742e+09 v k 73033 2.108e+18 3.4768e+14 6.5236e+13 v epsilon 6.4366e+09 2.6256e+29 1.1533e+25 2.0952e+24 v turbulent_viscosity 1.1759e-05 1.3567e+06 3863.3 3318.2 v CourantNb 14.574 2.7338e+09 1.2225e+06 4.1811e+05 v FourierNb 0.075663 1.0435e+09 2.0971e+06 2.9385e+05 v total_pressure -5.876e+10 3.2396e+10 4.539e+09 6.2743e+09 v Local Time Step 0.0025 0.0025 0.0025 0.0025 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 146.64 3.07e+09 3.3196e+06 7.1196e+05 TIME FOR THE TIME STEP 220: 0.10509E+02 =============================================================== INSTANT 0.110500000E+02 TIME STEP NUMBER 221 ============================================================= Incoming flow detained for 984 outlet faces on 1690 TIME FOR THE TIME STEP 221: 0.11652E+02 =============================================================== INSTANT 0.111000000E+02 TIME STEP NUMBER 222 ============================================================= Incoming flow detained for 706 outlet faces on 1690 TIME FOR THE TIME STEP 222: 0.12457E+02 =============================================================== INSTANT 0.111500000E+02 TIME STEP NUMBER 223 ============================================================= Incoming flow detained for 984 outlet faces on 1690 TIME FOR THE TIME STEP 223: 0.14801E+02 =============================================================== INSTANT 0.112000000E+02 TIME STEP NUMBER 224 ============================================================= Incoming flow detained for 706 outlet faces on 1690 TIME FOR THE TIME STEP 224: 0.10473E+02 =============================================================== INSTANT 0.112500000E+02 TIME STEP NUMBER 225 ============================================================= Incoming flow detained for 984 outlet faces on 1690 TIME FOR THE TIME STEP 225: 0.97810E+01 =============================================================== INSTANT 0.113000000E+02 TIME STEP NUMBER 226 ============================================================= Incoming flow detained for 706 outlet faces on 1690 TIME FOR THE TIME STEP 226: 0.11565E+02 =============================================================== INSTANT 0.113500000E+02 TIME STEP NUMBER 227 ============================================================= Incoming flow detained for 1019 outlet faces on 1690 TIME FOR THE TIME STEP 227: 0.10641E+02 =============================================================== INSTANT 0.114000000E+02 TIME STEP NUMBER 228 ============================================================= Incoming flow detained for 667 outlet faces on 1690 TIME FOR THE TIME STEP 228: 0.14676E+02 =============================================================== INSTANT 0.114500000E+02 TIME STEP NUMBER 229 ============================================================= Incoming flow detained for 1026 outlet faces on 1690 TIME FOR THE TIME STEP 229: 0.73325E+01 =============================================================== INSTANT 0.115000000E+02 TIME STEP NUMBER 230 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 358 -0.264069000E+01 Smooth wall 5 97490 0.291174483E-08 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 1690 0.345800443E+04 Free inlet 13 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : -0.35702E+06 0.85751E+10 Friction velocity uet : 0.29285E+01 0.13799E+09 Friction velocity uk : 0.13683E+04 0.21694E+10 Dimensionless distance yplus : 0.26876E+05 0.20233E+12 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 1 Nb of faces within the viscous sub-layer : 0 Total number of wall faces : 97490 ------------------------------------------------------------ Incoming flow detained for 688 outlet faces on 1690 ** INFORMATION ON CONVERGENCE -------------------------- --------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual derive --------------------------------------------------------------- c VelocityX 0.29548E+17 2187 0.63750E+00 0.32728E+18 c VelocityY 0.29548E+17 2187 0.63750E+00 0.00000E+00 c VelocityZ 0.29548E+17 2187 0.63750E+00 0.00000E+00 c Pressure 0.44401E+07 407 0.13937E-01 0.12025E+00 c k 0.96624E+26 41 0.31404E-02 0.33167E+35 c epsilon 0.32741E+38 25 0.25909E-02 0.43618E+58 --------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a epsilon a Local Time Step 3.87e-09 38352 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ------------------- -------------- -------------- -------------- -------------- v Velocity[X] -5.0883e+09 2.474e+09 -5.0754e+05 -3.5674e+05 v Velocity[Y] -5.0306e+09 3.3192e+09 -4.0858e+05 -2.7569e+05 v Velocity[Z] -5.4432e+09 9.704e+09 3.7689e+05 75746 v ǁVelocityǁ 437.83 9.7372e+09 9.4354e+06 5.2675e+06 v Pressure -1.5217e+11 1.254e+11 2.0662e+10 2.7565e+10 v k 3.9912e+06 1.9403e+19 2.2429e+15 4.5646e+14 v epsilon 7.313e+11 6.8733e+30 2.3548e+26 4.7836e+25 v turbulent_viscosity 0.0011587 3.197e+06 9022.9 8163.7 v CourantNb 18.621 7.3967e+09 4.1623e+06 1.7707e+06 v FourierNb 75.312 2.4602e+09 3.6606e+06 7.2972e+05 v total_pressure -1.5217e+11 1.254e+11 2.0662e+10 2.7565e+10 v Local Time Step 0.0025 0.0025 0.0025 0.0025 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 360.44 8.475e+09 7.8229e+06 2.5004e+06 TIME FOR THE TIME STEP 230: 0.17680E+02 =============================================================== INSTANT 0.115500000E+02 TIME STEP NUMBER 231 ============================================================= Incoming flow detained for 976 outlet faces on 1690 TIME FOR THE TIME STEP 231: 0.16258E+02 =============================================================== INSTANT 0.116000000E+02 TIME STEP NUMBER 232 ============================================================= Incoming flow detained for 1061 outlet faces on 1690 TIME FOR THE TIME STEP 232: 0.13792E+02 =============================================================== INSTANT 0.116500000E+02 TIME STEP NUMBER 233 ============================================================= Incoming flow detained for 782 outlet faces on 1690 TIME FOR THE TIME STEP 233: 0.10621E+02 =============================================================== INSTANT 0.117000000E+02 TIME STEP NUMBER 234 ============================================================= Incoming flow detained for 963 outlet faces on 1690 TIME FOR THE TIME STEP 234: 0.10121E+02 =============================================================== INSTANT 0.117500000E+02 TIME STEP NUMBER 235 ============================================================= Incoming flow detained for 726 outlet faces on 1690 TIME FOR THE TIME STEP 235: 0.18322E+02 =============================================================== INSTANT 0.118000000E+02 TIME STEP NUMBER 236 ============================================================= Incoming flow detained for 958 outlet faces on 1690 TIME FOR THE TIME STEP 236: 0.14685E+02 =============================================================== INSTANT 0.118500000E+02 TIME STEP NUMBER 237 ============================================================= Incoming flow detained for 735 outlet faces on 1690 TIME FOR THE TIME STEP 237: 0.15250E+02 =============================================================== INSTANT 0.119000000E+02 TIME STEP NUMBER 238 ============================================================= Incoming flow detained for 1051 outlet faces on 1690 TIME FOR THE TIME STEP 238: 0.15774E+02 =============================================================== INSTANT 0.119500000E+02 TIME STEP NUMBER 239 ============================================================= Incoming flow detained for 683 outlet faces on 1690 TIME FOR THE TIME STEP 239: 0.63689E+01 =============================================================== INSTANT 0.120000000E+02 TIME STEP NUMBER 240 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 358 -0.264069000E+01 Smooth wall 5 97490 0.482157572E-08 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 1690 -0.108736351E+04 Free inlet 13 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : -0.46336E+06 0.24565E+11 Friction velocity uet : 0.31227E+02 0.37899E+09 Friction velocity uk : 0.98221E+04 0.65978E+10 Dimensionless distance yplus : 0.26684E+06 0.61535E+12 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 3 Nb of faces within the viscous sub-layer : 0 Total number of wall faces : 97490 ------------------------------------------------------------ Incoming flow detained for 822 outlet faces on 1690 ** INFORMATION ON CONVERGENCE -------------------------- --------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual derive --------------------------------------------------------------- c VelocityX 0.21471E+18 1710 0.67457E+00 0.23537E+19 c VelocityY 0.21471E+18 1710 0.67457E+00 0.00000E+00 c VelocityZ 0.21471E+18 1710 0.67457E+00 0.00000E+00 c Pressure 0.12057E+08 388 0.13210E-01 0.11946E+00 c k 0.25016E+28 36 0.30721E-02 0.19914E+37 c epsilon 0.26421E+40 22 0.27617E-02 0.27256E+61 --------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a epsilon -7.9531e+18 2 a Local Time Step 3.4833e-10 38352 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ------------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.4653e+10 6.0246e+09 -3.1006e+05 -5.8068e+05 v Velocity[Y] -1.3535e+10 7.5306e+09 7.6298e+05 -3006.8 v Velocity[Z] -1.3181e+10 2.9245e+10 1.5564e+06 2.245e+05 v ǁVelocityǁ 2311.8 2.9498e+10 2.4076e+07 1.3989e+07 v Pressure -5.5331e+11 2.1086e+11 2.6366e+10 3.8894e+10 v k 1.1833e+08 1.7729e+20 1.6139e+16 3.6376e+15 v epsilon 7.4166e+13 1.9689e+32 5.7907e+27 1.239e+27 v turbulent_viscosity 0.12866 7.5979e+06 27921 30324 v CourantNb 4.7946e-11 1.9153e+10 8.7378e+06 3.247e+06 v FourierNb 165.67 5.818e+09 1.026e+07 2.4324e+06 v total_pressure -5.5331e+11 2.1086e+11 2.6366e+10 3.8894e+10 v Local Time Step 0.0025 0.0025 0.0025 0.0025 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1762.6 2.244e+10 1.8998e+07 5.6794e+06 TIME FOR THE TIME STEP 240: 0.13069E+02 =============================================================== INSTANT 0.120500000E+02 TIME STEP NUMBER 241 ============================================================= Incoming flow detained for 1092 outlet faces on 1690 TIME FOR THE TIME STEP 241: 0.16840E+02 =============================================================== INSTANT 0.121000000E+02 TIME STEP NUMBER 242 ============================================================= Incoming flow detained for 1066 outlet faces on 1690 TIME FOR THE TIME STEP 242: 0.89408E+01 =============================================================== INSTANT 0.121500000E+02 TIME STEP NUMBER 243 ============================================================= Incoming flow detained for 1042 outlet faces on 1690 TIME FOR THE TIME STEP 243: 0.87865E+01 =============================================================== INSTANT 0.122000000E+02 TIME STEP NUMBER 244 ============================================================= Incoming flow detained for 672 outlet faces on 1690 TIME FOR THE TIME STEP 244: 0.11946E+02 =============================================================== INSTANT 0.122500000E+02 TIME STEP NUMBER 245 ============================================================= Incoming flow detained for 983 outlet faces on 1690 TIME FOR THE TIME STEP 245: 0.98521E+01 =============================================================== INSTANT 0.123000000E+02 TIME STEP NUMBER 246 ============================================================= Incoming flow detained for 694 outlet faces on 1690 TIME FOR THE TIME STEP 246: 0.11552E+02 =============================================================== INSTANT 0.123500000E+02 TIME STEP NUMBER 247 ============================================================= Incoming flow detained for 1049 outlet faces on 1690 TIME FOR THE TIME STEP 247: 0.89017E+01 =============================================================== INSTANT 0.124000000E+02 TIME STEP NUMBER 248 ============================================================= Incoming flow detained for 733 outlet faces on 1690 TIME FOR THE TIME STEP 248: 0.88680E+01 =============================================================== INSTANT 0.124500000E+02 TIME STEP NUMBER 249 ============================================================= Incoming flow detained for 1017 outlet faces on 1690 TIME FOR THE TIME STEP 249: 0.10392E+02 =============================================================== INSTANT 0.125000000E+02 TIME STEP NUMBER 250 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 358 -0.264069000E+01 Smooth wall 5 97490 0.335057385E-08 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 1690 -0.875659605E+05 Free inlet 13 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : -0.32654E+07 0.65386E+11 Friction velocity uet : 0.41559E+02 0.98417E+09 Friction velocity uk : 0.82503E+04 0.15354E+11 Dimensionless distance yplus : 0.39397E+06 0.14320E+13 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 26 Nb of faces within the viscous sub-layer : 0 Total number of wall faces : 97490 ------------------------------------------------------------ Incoming flow detained for 910 outlet faces on 1690 ** INFORMATION ON CONVERGENCE -------------------------- --------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual derive --------------------------------------------------------------- c VelocityX 0.17130E+19 1527 0.68439E+00 0.17220E+20 c VelocityY 0.17130E+19 1527 0.68439E+00 0.00000E+00 c VelocityZ 0.17130E+19 1527 0.68439E+00 0.00000E+00 c Pressure 0.32776E+08 321 0.10582E-01 0.12128E+00 c k 0.36048E+29 36 0.15282E-02 0.40453E+38 c epsilon 0.95587E+41 23 0.15599E-02 0.35601E+63 --------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a epsilon a Local Time Step 2.7665e-10 38352 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ------------------- -------------- -------------- -------------- -------------- v Velocity[X] -3.841e+10 2.1873e+10 -1.4571e+06 -1.4837e+06 v Velocity[Y] -3.5116e+10 2.4437e+10 -5.2408e+05 -1.0307e+06 v Velocity[Z] -4.7191e+10 7.0209e+10 -1.8521e+06 1.6475e+06 v ǁVelocityǁ 2214.3 7.04e+10 5.8183e+07 3.6532e+07 v Pressure -1.0634e+12 6.2423e+11 1.1944e+11 1.5364e+11 v k 1.0622e+07 9.5863e+20 8.9903e+16 1.9612e+16 v epsilon 2.5379e+14 2.6068e+33 7.7054e+28 1.6197e+28 v turbulent_viscosity 1.8135e-05 1.7785e+07 60348 63476 v CourantNb 172.76 5.7623e+10 2.3942e+07 1.0057e+07 v FourierNb 188.78 1.3629e+10 1.8026e+07 5.3068e+06 v total_pressure -1.0634e+12 6.2423e+11 1.1944e+11 1.5364e+11 v Local Time Step 0.0025 0.0025 0.0025 0.0025 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 3988.7 6.4414e+10 4.1969e+07 1.5364e+07 TIME FOR THE TIME STEP 250: 0.13154E+02 =============================================================== INSTANT 0.125500000E+02 TIME STEP NUMBER 251 ============================================================= Incoming flow detained for 1193 outlet faces on 1690 TIME FOR THE TIME STEP 251: 0.14778E+02 =============================================================== INSTANT 0.126000000E+02 TIME STEP NUMBER 252 ============================================================= Incoming flow detained for 860 outlet faces on 1690 TIME FOR THE TIME STEP 252: 0.15611E+02 =============================================================== INSTANT 0.126500000E+02 TIME STEP NUMBER 253 ============================================================= Incoming flow detained for 946 outlet faces on 1690 TIME FOR THE TIME STEP 253: 0.11846E+02 =============================================================== INSTANT 0.127000000E+02 TIME STEP NUMBER 254 ============================================================= Incoming flow detained for 846 outlet faces on 1690 TIME FOR THE TIME STEP 254: 0.13451E+02 =============================================================== INSTANT 0.127500000E+02 TIME STEP NUMBER 255 ============================================================= Incoming flow detained for 1145 outlet faces on 1690 TIME FOR THE TIME STEP 255: 0.10269E+02 =============================================================== INSTANT 0.128000000E+02 TIME STEP NUMBER 256 ============================================================= Incoming flow detained for 683 outlet faces on 1690 TIME FOR THE TIME STEP 256: 0.79048E+01 =============================================================== INSTANT 0.128500000E+02 TIME STEP NUMBER 257 ============================================================= Incoming flow detained for 811 outlet faces on 1690 TIME FOR THE TIME STEP 257: 0.10985E+02 =============================================================== INSTANT 0.129000000E+02 TIME STEP NUMBER 258 ============================================================= Incoming flow detained for 660 outlet faces on 1690 TIME FOR THE TIME STEP 258: 0.12823E+02 =============================================================== INSTANT 0.129500000E+02 TIME STEP NUMBER 259 ============================================================= Incoming flow detained for 1103 outlet faces on 1690 TIME FOR THE TIME STEP 259: 0.11774E+02 =============================================================== INSTANT 0.130000000E+02 TIME STEP NUMBER 260 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 358 -0.264069000E+01 Smooth wall 5 97490 0.271705558E-07 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 1690 -0.172592477E+06 Free inlet 13 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : -0.35846E+09 0.18845E+12 Friction velocity uet : 0.56669E+02 0.27131E+10 Friction velocity uk : 0.43617E+04 0.45918E+11 Dimensionless distance yplus : 0.90013E+05 0.42826E+13 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 43 Nb of faces within the viscous sub-layer : 0 Total number of wall faces : 97490 ------------------------------------------------------------ Incoming flow detained for 745 outlet faces on 1690 ** INFORMATION ON CONVERGENCE -------------------------- --------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual derive --------------------------------------------------------------- c VelocityX 0.12969E+20 1353 0.70252E+00 0.13824E+21 c VelocityY 0.12969E+20 1353 0.70252E+00 0.00000E+00 c VelocityZ 0.12969E+20 1353 0.70252E+00 0.00000E+00 c Pressure 0.96945E+08 424 0.16166E-01 0.13262E+00 c k 0.90982E+30 34 0.24026E-02 0.46156E+40 c epsilon 0.64258E+43 24 0.30762E-02 0.32178E+66 --------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a epsilon a Local Time Step 9.0458e-11 38352 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ------------------- -------------- -------------- -------------- -------------- v Velocity[X] -1.0405e+11 6.0325e+10 8.8846e+06 -5.3062e+06 v Velocity[Y] -9.8109e+10 7.4118e+10 -2.7008e+06 -4.8743e+05 v Velocity[Z] -1.2929e+11 2.0313e+11 -2.3135e+07 1.2853e+06 v ǁVelocityǁ 12969 2.042e+11 2.1931e+08 1.3633e+08 v Pressure -2.4061e+12 2.1554e+12 5.6183e+11 7.2729e+11 v k 2.2157e+06 8.7349e+21 6.8339e+17 1.6734e+17 v epsilon 1.8895e+14 6.4681e+34 1.8532e+30 4.1301e+29 v turbulent_viscosity 1.7135e-06 4.2366e+07 1.7149e+05 2.0527e+05 v CourantNb 69.685 1.5752e+11 6.2043e+07 2.6223e+07 v FourierNb 91.807 3.2384e+10 4.1661e+07 1.6032e+07 v total_pressure -2.4061e+12 2.1554e+12 5.6183e+11 7.2729e+11 v Local Time Step 0.0025 0.0025 0.0025 0.0025 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7444 1.8068e+11 1.037e+08 4.2255e+07 TIME FOR THE TIME STEP 260: 0.12841E+02 =============================================================== INSTANT 0.130500000E+02 TIME STEP NUMBER 261 ============================================================= Incoming flow detained for 982 outlet faces on 1690 TIME FOR THE TIME STEP 261: 0.17544E+02 =============================================================== INSTANT 0.131000000E+02 TIME STEP NUMBER 262 ============================================================= Incoming flow detained for 705 outlet faces on 1690 TIME FOR THE TIME STEP 262: 0.11557E+02 =============================================================== INSTANT 0.131500000E+02 TIME STEP NUMBER 263 ============================================================= Incoming flow detained for 1020 outlet faces on 1690 TIME FOR THE TIME STEP 263: 0.11704E+02 =============================================================== INSTANT 0.132000000E+02 TIME STEP NUMBER 264 ============================================================= Incoming flow detained for 1043 outlet faces on 1690 TIME FOR THE TIME STEP 264: 0.86679E+01 =============================================================== INSTANT 0.132500000E+02 TIME STEP NUMBER 265 ============================================================= Incoming flow detained for 687 outlet faces on 1690 TIME FOR THE TIME STEP 265: 0.12579E+02 =============================================================== INSTANT 0.133000000E+02 TIME STEP NUMBER 266 ============================================================= Incoming flow detained for 942 outlet faces on 1690 TIME FOR THE TIME STEP 266: 0.89142E+01 =============================================================== INSTANT 0.133500000E+02 TIME STEP NUMBER 267 ============================================================= Incoming flow detained for 752 outlet faces on 1690 TIME FOR THE TIME STEP 267: 0.10023E+02 =============================================================== INSTANT 0.134000000E+02 TIME STEP NUMBER 268 ============================================================= Incoming flow detained for 892 outlet faces on 1690 TIME FOR THE TIME STEP 268: 0.18604E+02 =============================================================== INSTANT 0.134500000E+02 TIME STEP NUMBER 269 ============================================================= Incoming flow detained for 619 outlet faces on 1690 TIME FOR THE TIME STEP 269: 0.10417E+02 =============================================================== INSTANT 0.135000000E+02 TIME STEP NUMBER 270 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 358 -0.264069000E+01 Smooth wall 5 97490 0.120499452E-06 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 1690 -0.721734499E+06 Free inlet 13 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : -0.10444E+10 0.49581E+12 Friction velocity uet : 0.50971E+03 0.69152E+10 Friction velocity uk : 0.11899E+06 0.12631E+12 Dimensionless distance yplus : 0.14760E+07 0.11780E+14 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 27 Nb of faces within the viscous sub-layer : 0 Total number of wall faces : 97490 ------------------------------------------------------------ Incoming flow detained for 642 outlet faces on 1690 ** INFORMATION ON CONVERGENCE -------------------------- --------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual derive --------------------------------------------------------------- c VelocityX 0.10927E+21 836 0.67315E+00 0.15657E+22 c VelocityY 0.10927E+21 836 0.67315E+00 0.00000E+00 c VelocityZ 0.10927E+21 836 0.67315E+00 0.00000E+00 c Pressure 0.25857E+09 356 0.15374E-01 0.13009E+00 c k 0.20291E+32 38 0.21004E-02 0.35089E+42 c epsilon 0.42081E+45 24 0.19958E-02 0.17219E+69 --------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a epsilon a Local Time Step 3.7326e-11 38352 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ------------------- -------------- -------------- -------------- -------------- v Velocity[X] -2.508e+11 1.465e+11 3.8283e+07 -1.8749e+06 v Velocity[Y] -3.2221e+11 1.4952e+11 5.9276e+07 2.9758e+07 v Velocity[Z] -3.9088e+11 4.8986e+11 -8.1998e+06 2.3604e+07 v ǁVelocityǁ 16190 4.9433e+11 6.2592e+08 3.5429e+08 v Pressure -7.123e+12 7.7399e+12 1.7574e+12 2.2019e+12 v k 2.6624e+10 6.3707e+22 5.0187e+18 1.2937e+18 v epsilon 2.3339e+17 1.3519e+36 4.0695e+31 9.2493e+30 v turbulent_viscosity 0.12281 1.0151e+08 3.6948e+05 3.8759e+05 v CourantNb 4445.2 4.5259e+11 2.1188e+08 9.1201e+07 v FourierNb 138.88 7.4506e+10 9.6737e+07 3.2813e+07 v total_pressure -7.123e+12 7.7399e+12 1.7574e+12 2.2019e+12 v Local Time Step 0.0025 0.0025 0.0025 0.0025 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 48526 5.132e+11 3.0862e+08 1.2401e+08 TIME FOR THE TIME STEP 270: 0.75358E+01 =============================================================== INSTANT 0.135500000E+02 TIME STEP NUMBER 271 ============================================================= Incoming flow detained for 1052 outlet faces on 1690 TIME FOR THE TIME STEP 271: 0.15526E+02 =============================================================== INSTANT 0.136000000E+02 TIME STEP NUMBER 272 ============================================================= Incoming flow detained for 718 outlet faces on 1690 TIME FOR THE TIME STEP 272: 0.15854E+02 =============================================================== INSTANT 0.136500000E+02 TIME STEP NUMBER 273 ============================================================= Incoming flow detained for 964 outlet faces on 1690 TIME FOR THE TIME STEP 273: 0.20191E+02 =============================================================== INSTANT 0.137000000E+02 TIME STEP NUMBER 274 ============================================================= Incoming flow detained for 981 outlet faces on 1690 TIME FOR THE TIME STEP 274: 0.11022E+02 =============================================================== INSTANT 0.137500000E+02 TIME STEP NUMBER 275 ============================================================= Incoming flow detained for 1078 outlet faces on 1690 TIME FOR THE TIME STEP 275: 0.17878E+02 =============================================================== INSTANT 0.138000000E+02 TIME STEP NUMBER 276 ============================================================= Incoming flow detained for 1058 outlet faces on 1690 TIME FOR THE TIME STEP 276: 0.13516E+02 =============================================================== INSTANT 0.138500000E+02 TIME STEP NUMBER 277 ============================================================= Incoming flow detained for 974 outlet faces on 1690 TIME FOR THE TIME STEP 277: 0.12149E+02 =============================================================== INSTANT 0.139000000E+02 TIME STEP NUMBER 278 ============================================================= Incoming flow detained for 694 outlet faces on 1690 TIME FOR THE TIME STEP 278: 0.89968E+01 =============================================================== INSTANT 0.139500000E+02 TIME STEP NUMBER 279 ============================================================= Incoming flow detained for 1267 outlet faces on 1690 TIME FOR THE TIME STEP 279: 0.19185E+02 =============================================================== INSTANT 0.140000000E+02 TIME STEP NUMBER 280 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 358 -0.264069000E+01 Smooth wall 5 97490 0.314370188E-06 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 1690 -0.234167833E+07 Free inlet 13 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : -0.44359E+10 0.17324E+13 Friction velocity uet : 0.76068E+03 0.23402E+11 Friction velocity uk : 0.78811E+05 0.35905E+12 Dimensionless distance yplus : 0.98779E+06 0.33336E+14 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 51 Nb of faces within the viscous sub-layer : 0 Total number of wall faces : 97490 ------------------------------------------------------------ Incoming flow detained for 760 outlet faces on 1690 ** INFORMATION ON CONVERGENCE -------------------------- --------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual derive --------------------------------------------------------------- c VelocityX 0.79311E+21 1226 0.74509E+00 0.13378E+23 c VelocityY 0.79311E+21 1226 0.74509E+00 0.00000E+00 c VelocityZ 0.79311E+21 1226 0.74509E+00 0.00000E+00 c Pressure 0.75669E+09 395 0.26538E-01 0.13398E+00 c k 0.46149E+33 33 0.28429E-02 0.36442E+44 c epsilon 0.28524E+47 23 0.20103E-02 0.14476E+72 --------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a epsilon -5.0249e+19 1 a Local Time Step 1.1459e-11 38352 ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - ------------------- -------------- -------------- -------------- -------------- v Velocity[X] -6.9137e+11 4.4412e+11 1.6392e+08 -1.8265e+07 v Velocity[Y] -1.0389e+12 4.3801e+11 1.7379e+08 2.9544e+07 v Velocity[Z] -1.1252e+12 1.858e+12 -4.0695e+06 5.1301e+06 v ǁVelocityǁ 1.1997e+05 1.872e+12 2.6584e+09 1.9308e+09 v Pressure -1.7006e+13 5.0155e+13 1.1814e+13 1.5464e+13 v k 3.1417e+08 5.4044e+23 3.8838e+19 1.0451e+19 v epsilon 1.2313e+17 3.4089e+37 1.0081e+33 2.3246e+32 v turbulent_viscosity 0.00015886 2.8166e+08 1.4618e+06 1.7534e+06 v CourantNb 9509.9 1.1637e+12 4.1992e+08 1.6598e+08 v FourierNb 25.517 1.7912e+11 3.1831e+08 1.3816e+08 v total_pressure -1.7006e+13 5.0155e+13 1.1814e+13 1.5464e+13 v Local Time Step 0.0025 0.0025 0.0025 0.0025 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.4313e+05 1.2088e+12 7.3823e+08 3.0413e+08 TIME FOR THE TIME STEP 280: 0.12836E+02 =============================================================== INSTANT 0.140500000E+02 TIME STEP NUMBER 281 ============================================================= Incoming flow detained for 1369 outlet faces on 1690 TIME FOR THE TIME STEP 281: 0.20203E+02 =============================================================== INSTANT 0.141000000E+02 TIME STEP NUMBER 282 ============================================================= Incoming flow detained for 687 outlet faces on 1690 TIME FOR THE TIME STEP 282: 0.10260E+02 =============================================================== INSTANT 0.141500000E+02 TIME STEP NUMBER 283 ============================================================= Incoming flow detained for 793 outlet faces on 1690 TIME FOR THE TIME STEP 283: 0.16074E+02 =============================================================== INSTANT 0.142000000E+02 TIME STEP NUMBER 284 ============================================================= Incoming flow detained for 876 outlet faces on 1690 TIME FOR THE TIME STEP 284: 0.10919E+02 =============================================================== INSTANT 0.142500000E+02 TIME STEP NUMBER 285 ============================================================= Incoming flow detained for 873 outlet faces on 1690 TIME FOR THE TIME STEP 285: 0.15006E+02 =============================================================== INSTANT 0.143000000E+02 TIME STEP NUMBER 286 ============================================================= Incoming flow detained for 1052 outlet faces on 1690 TIME FOR THE TIME STEP 286: 0.10068E+02 =============================================================== INSTANT 0.143500000E+02 TIME STEP NUMBER 287 ============================================================= Incoming flow detained for 1266 outlet faces on 1690 TIME FOR THE TIME STEP 287: 0.19716E+02 =============================================================== INSTANT 0.144000000E+02 TIME STEP NUMBER 288 ============================================================= Incoming flow detained for 866 outlet faces on 1690 TIME FOR THE TIME STEP 288: 0.10764E+02 =============================================================== INSTANT 0.144500000E+02 TIME STEP NUMBER 289 ============================================================= Incoming flow detained for 889 outlet faces on 1690 TIME FOR THE TIME STEP 289: 0.20195E+02 =============================================================== INSTANT 0.145000000E+02 TIME STEP NUMBER 290 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 358 -0.264069000E+01 Smooth wall 5 97490 0.131027802E-05 Rough wall 6 0 0.000000000E+00 Symmetry 4 0 0.000000000E+00 Free outlet 3 1690 -0.517316180E+07 Free inlet 13 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : -0.56263E+10 0.38624E+13 Friction velocity uet : 0.76807E+03 0.50250E+11 Friction velocity uk : 0.87096E+04 0.11040E+13 Dimensionless distance yplus : 0.13890E+06 0.10297E+15 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 33 Nb of faces within the viscous sub-layer : 0 Total number of wall faces : 97490 ------------------------------------------------------------ Incoming flow detained for 1115 outlet faces on 1690 -------------------------------------------------------------------------- MPI_ABORT was invoked on rank 2 in communicator MPI_COMM_WORLD with errorcode 1. NOTE: invoking MPI_ABORT causes Open MPI to kill all MPI processes. You may or may not see output from other processes, depending on exactly when Open MPI kills them. -------------------------------------------------------------------------- -------------------------------------------------------------------------- mpiexec.openmpi has exited due to process rank 2 with PID 4883 on node Workstation exiting without calling "finalize". This may have caused other processes in the application to be terminated by signals sent by mpiexec.openmpi (as reported here). -------------------------------------------------------------------------- **************************** Saving calculation results **************************** solver script exited with status 1. Error running the calculation. Check Code_Saturne log (listing) and error* files for details. Error in calculation stage.