command: /home/james/tmp_Saturne/V2RC1.3DEG_SAT.07051311/cs_solver *************************************************************** (R) Code_Saturne Version 2.0.0-rc2 Copyright (C) 1998-2009 EDF S.A., France build Wed 30 Jun 2010 01:16:45 PM BST MPI version 2.1 (Open MPI) The Code_Saturne CFD tool is free software; you can redistribute it and/or modify it under the terms of the GNU General Public License as published by the Free Software Foundation; either version 2 of the License, or (at your option) any later version. The Code_Saturne CFD tool is distributed in the hope that it will be useful, but WITHOUT ANY WARRANTY; without even the implied warranty of MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU General Public License for more details. *************************************************************** Local case configuration: Date: Mon 05 Jul 2010 01:11:45 PM BST System: Linux 2.6.18-128.1.1.el5 Machine: mbbxhjm2.mace.manchester.ac.uk Processor: Intel(R) Core(TM)2 Duo CPU E8400 @ 3.00GHz Memory: 8044052 User: james () Directory: /home/james/tmp_Saturne/V2RC1.3DEG_SAT.07051311 MPI ranks: 1 =============================================================== CALCULATION PREPARATION ======================= =========================================================== Reading file: preprocessor_output No error detected during the data verification (interface, usini1 and others). =========================================================== CALCULATION PARAMETERS SUMMARY ============================== ----------------------------------------------------------- ** DIMENSIONS ---------- --- Geometry NPRFML = 1 (Nb max. family properties ) NFML = 7 (Nb families ) --- Physics NPHAS = 1 (Nb phases ) NVAR = 6 (Nb variables ) NSCAL = 0 (Nb scalars ) NSCAUS = 0 (Nb user scalars ) NSCAPP = 0 (Nb specific physics scalars ) NPROCE = 6 (Nb cell properties ) NPROFA = 1 (Nb internal face properties ) NPROFB = 2 (Nb boundary face properties ) ----------------------------------------------------------- ** PHYSICAL PROPERTIES ------------------- GX = 0.00000E+00 (Gravity x component ) GY = 0.00000E+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 ) -- Phase: 1 RO0 = 0.10000E+04 (Reference density ) VISCL0 = 0.10000E-02 (Ref. molecular dyn. visc. ) CP0 = 0.12190E+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 = 0.12732E+04 (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 ----------------------------------------------------------- ** TURBULENCE ---------- --- Phase: 1 - Commons ITURB = 20 (Turbulence model ) IDEUCH = 1 (0: one-scale model ) (1: two-scale model ) (2: invariant wall function ) 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) ) ISCALT = -1 (Temperature salar number ) - k-epsilon (ITURB = 20) ALMAX = -0.10000E+13 (Characteristic length ) UREF = 0.10000E+01 (Characteristic velocity ) ICLKEP = 0 (k-epsilon clipping model ) IKECOU = 1 (k-epsilon coupling mode ) IGRAKE = 1 (Account for gravity ) --- Constants - Commons XKAPPA = 0.42000E+00 (Von Karman constant ) CSTLOG = 0.52000E+01 (U+=Log(y+)/kappa +CSTLOG ) APOW = 0.83000E+01 (U+=APOW (y+)**BPOW (W&W law)) BPOW = 0.14286E+00 (U+=APOW (y+)**BPOW (W&W law)) - k-epsilon (ITURB = 20) CE1 = 0.14400E+01 (Cepsilon 1: production coef.) CE2 = 0.19200E+01 (Cepsilon 2: dissipat. coef.) SIGMAK = 0.10000E+01 (Prandtl relative to k ) SIGMAE = 0.13000E+01 (Prandtl relative to epsilon ) CMU = 0.90000E-01 (Cmu constant ) ----------------------------------------------------------- ** SECONDARY VISCOSITY ------------------- --- Phase: 1 IVISSE = 1 (1: accounted for ) ----------------------------------------------------------- ** TIME STEPPING ------------- UNSTEADY ALGORITHM --- Time step parameters IDTVAR = 0 (0 cst; 1,2 var (t, t-space ) IPTLRO = 0 (1: rho-related DT clipping ) COUMAX = 0.10000E+01 (Maximum target CFL ) FOUMAX = 0.10000E+02 (Maximum target Fourier ) VARRDT = 0.10000E+00 (For var. DT, max. increase ) DTMIN = 0.10000E-02 (Minimum time step ) DTMAX = 0.10000E+02 (Maximum time step ) DTREF = 0.10000E-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 ---------------------------- Pressure 0 0.1000E+01 Velocity 1 0.1000E+01 Velocity 1 0.1000E+01 Velocity 1 0.1000E+01 Turb Kin 1 0.1000E+01 Turb Dis 1 0.1000E+01 ---------------------------- ISTAT = 0 ou 1 (1 for unsteady ) CDTVAR > 0 (time step multiplier ) --- Order of base time stepping scheme Phase: 1 ISCHTP = 1 (1: order 1; 2: order 2 ) ----------------------------------------------------------- ** CONVECTION - DIFFUSION ---------------------- ------------------------------------------------------------- Variable ICONV IDIFF IDIFFT ISCHCV ISSTPC BLENCV THETAV ------------------------------------------------------------- Pressure 0 1 1 1 0 0.00E+00 0.10E+01 Velocity 1 1 1 1 0 0.10E+01 0.10E+01 Velocity 1 1 1 1 0 0.10E+01 0.10E+01 Velocity 1 1 1 1 0 0.10E+01 0.10E+01 Turb Kin 1 1 1 1 0 0.00E+00 0.10E+01 Turb Dis 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 ------ 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 ) -- Phase: 1 IREVMC = 0 (Velocity reconstruction mode) RELAXV = 0.10000E+01 for pressure (relaxation) ARAK = 0.10000E+01 (Arakawa factor ) ISTMPF = 1 (time scheme for flow (0: explicit (THETFL = 0 ) (1: std scheme (Saturne 1.0 ) (2: 2nd-order (THETFL = 0.5 ) THETFL = -0.99900E+03 (theta for mass flow ) IROEXT = 0 (density extrapolation (0: explicit (1: n+thetro with thetro=1/2 (2: n+thetro with thetro=1 THETRO = 0.00000E+00 (theta for density ((1+theta).new-theta.old IVIEXT = 0 (total viscosity extrapolation (0: explicit (1: n+thetvi with thetro=1/2 (2: n+thetvi with thetro=1 THETVI = 0.00000E+00 (theta for total viscosity ((1+theta).new-theta.old ICPEXT = 0 (specific heat extrapolation (0: explicit (1: n+thetcp with thetro=1/2 (2: n+thetcp with thetro=1 THETCP = 0.00000E+00 (specific heat theta-scheme ((1+theta).new-theta.old THETSN = 0.00000E+00 (Nav-Stokes S.T. theta scheme) ((1+theta).new-theta.old THETST = 0.00000E+00 (Turbulence S.T. theta-scheme) ((1+theta).new-theta.old EPSUP = 0.10000E-04 (Velocity/pressure coupling stop test ) ----------------------------------------------------------- ** GRADIENTS CALCULATION --------------------- IMRGRA = 0 (Reconstruction mode ) ANOMAX = 0.78540E+00 (Non-ortho angle: limit for ) (least squares ext. neighbors) ----------------------------------------------------------- Variable NSWRGR NSWRSM EPSRGR EPSRSM EXTRAG ----------------------------------------------------------- Pressure 101 2 0.1000E-04 0.1000E-07 0.0000E+00 Velocity 102 1 0.1000E-04 0.1000E-07 0.0000E+00 Velocity 103 1 0.1000E-04 0.1000E-07 0.0000E+00 Velocity 104 1 0.1000E-04 0.1000E-07 0.0000E+00 Turb Kin 105 1 0.1000E-04 0.1000E-07 0.0000E+00 Turb Dis 106 1 0.1000E-04 0.1000E-07 0.0000E+00 ----------------------------------------------------------- ----------------------------------- Variable IRCFLU IMLIGR CLIMGR ----------------------------------- Pressure 1 -1 0.1500E+01 Velocity 1 -1 0.1500E+01 Velocity 1 -1 0.1500E+01 Velocity 1 -1 0.1500E+01 Turb Kin 1 -1 0.1500E+01 Turb Dis 1 -1 0.1500E+01 ----------------------------------- NSWRGR = (nb sweep gradient reconstr. ) NSWRSM = (nb sweep rhs reconstrcution ) EPSRGR = (grad. reconstruction prec. ) EPSRSM = (rhs reconstruction prec. ) EXTRAG = [0.;1.] (gradients extrapolation ) IRCFLU = 0 ou 1 (flow reconstruction ) IMLIGR = < 0, 0 ou 1 (gradient limitation method ) CLIMGR = > 1 ou 1 (gradient limitation coeff. ) ----------------------------------------------------------- ** FACE INTERPOLATION ------------------ IMVISF = 0 (0 arithmetic ) ----------------------------------------------------------- ** CALCULATION OF TEMPORAL MEANS (MOMENTS) --------------------------------------- NBMOMT = 0 (Number of moments ) ----------------------------------------------------------- ** BASE ITERATIVE SOLVERS ---------------------- ------------------------------------------ Variable IRESOL NITMAX EPSILO IDIRCL ------------------------------------------ Pressure -1 10000 0.1000E-07 1 Velocity -1 10000 0.1000E-07 1 Velocity -1 10000 0.1000E-07 1 Velocity -1 10000 0.1000E-07 1 Turb Kin -1 10000 0.1000E-07 1 Turb Dis -1 10000 0.1000E-07 1 ----------------------------------- IRESOL = -1 (automatic solver choice ) IPOL*1000 + 0 (p conjuguate gradient ) 1 (Jacobi ) IPOL*1000 + 2 (bicgstab ) avec IPOL (preconditioning degree ) NITMAX = (max number of iterations ) EPSILO = (resolution precision ) IDIRCL = 0 ou 1 (shift diagonal if ISTAT=0 and no Dirichlet ) ----------------------------------------------------------- ** MULTIGRID --------- NCEGRM = 30 (Max nb cells coarsest grid ) NGRMAX = 25 (Max numeber of levels ) ------------------------------ Variable IMGR NCYMAX NITMGF ------------------------------ Pressure 1 100 10 Velocity 0 100 10 Velocity 0 100 10 Velocity 0 100 10 Turb Kin 0 100 10 Turb Dis 0 100 10 ------------------------------ IMGR = 0 ou 1 (1: multigrid activated ) NCYMAX = (Max number of cycles ) NITMGF = (Max nb iter on coarsest grid) ----------------------------------------------------------- ** CALCULATION MANAGEMENT ---------------------- --- Restarted calculation ISUITE = 0 (1: restarted calculuation ) ILEAUX = 1 (1: also read suiamx ) IECAUX = 1 (1: also write suiavx ) suiamx and suiavx are the auxiliary restart files. --- 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 = 1 (Final time step required ) --- CPU time margin TMARUS = -0.10000E+01 (CPU time margin before stop ) ----------------------------------------------------------- ** INPUT-OUTPUT ------------ --- Restart file NTSUIT = 0 (Checkpoint frequency ) --- EnSight, MED, or CGNS output NTCHR = -1 (Output frequency ) Number Name 2 Pressure 3 VelocityX 4 VelocityY 5 VelocityZ 6 Turb Kinetic Ene 7 Turb Dissipation 10 Turb Viscosity 11 CFL 12 Fourier Number 13 Total Pressure -- -- --- Probe history files NTHIST = 1 (Output frequency ) NCAPT = 10 (Number of probes ) NTHSAV = 0 (Checkpoint frequency ) Number Name Nb. probes (-1: all) 2 Pressure -1 3 VelocityX -1 4 VelocityY -1 5 VelocityZ -1 6 Turb Kinetic Ene -1 7 Turb Dissipation -1 8 Density -1 10 Turb Viscosity -1 11 CFL -1 12 Fourier Number -1 13 Total Pressure -1 -- -- -- --- Log files NTLIST = 1 (Output frequency ) Number Name IWARNI verbosity level (-999: not applicable) 2 Pressure 0 3 VelocityX 0 4 VelocityY 0 5 VelocityZ 0 6 Turb Kinetic Ene 3 7 Turb Dissipation 0 8 Density -999 10 Turb Viscosity -999 13 Total Pressure -999 -- -- -- --- Additional post-processing variables IPSTDV = 210 (Product of the following values based on activation ) IPSTYP = 2 (Yplus on boundary ) IPSTCL = 3 (Variables on boundary ) IPSTFT = 5 (Thermal flow on boundary ) IPSTFO = 7 (Force exerted on boundary ) and IPSTDV = 1 (No additional output ) ----------------------------------------------------------- ** FILES ----- --- Standard files GEOMETRY MAIN RESTART AUX RESTART STOP Name geomet suiamo suiamx ficstp Unit 10 12 MAIN CHECKPOINT AUX CHECKPOINT Name suiava suiavx --- Radiative files DATA RESTART JANAF CHECKPOINT Name dp_tch rayamo JANAF rayava Unit 25 25 --- Lagrangian files --- RESTART --- -- CHECKPOINT - ---- POST ---- CALCUL. STAT. CALCUL. STAT. LOG HIST. Name lagamo lasamo lagava lasava listla Unit 80 81 82 --- Other files for Lagrangian module Unit 50 51 52 53 54 55 56 57 58 59 60 61 62 63 64 65 66 67 68 --- Developper files for probe history IMPHIS(1) IMPHIS(2) Unit 30 31 --- User files for probe history 16 files Name and unit ush001 ush002 ush003 ush004 ush005 ush006 ush007 ush008 ush009 ush010 ush011 ush012 ush013 ush014 ush015 ush016 33 34 35 36 37 38 39 40 41 42 43 44 45 46 47 48 --- Free user files 10 files Name and unit usrf01 usrf02 usrf03 usrf04 usrf05 usrf06 usrf07 usrf08 usrf09 usrf10 70 71 72 73 74 75 76 77 78 79 --- Preprocessor files Format: 1=Read preprocessor_output file 0=Standalone solver Format 1 ----------------------------------------------------------- ** ALE METHOD (MOVING MESH) ----------- IALE = 0 (1: activated ) NALINF = -999 (Fluid initialization iterations) ----------------------------------------------------------- Finished reading: preprocessor_output Number of cells: 4800 ---------------------------------------------------------- Number of cells + halo cells: 4800 ---------------------------------------------------------- Number of interior faces: 9450 ---------------------------------------------------------- Number of boundary faces: 9900 ---------------------------------------------------------- Histogram of the number of interior faces per cell: minimum value = 2 maximum value = 4 1 : [ 2 ; 3 [ = 2 2 : [ 3 ; 4 ] = 4798 ---------------------------------------------------------- Renumbering mesh: Mesh Number of cells: 4800 Number of interior faces: 9450 Number of boundary faces: 9900 Number of vertices: 9900 Computing geometric quantities (0.0052 s) Mesh coordinates: minimum and maximum X : -1.2482869e+01 2.0000000e+01 Y : -1.2500000e+01 1.2500000e+01 Z : -5.0000000e-01 5.0000000e-01 --- Main Fortran work arrays: longia = 297000 (Number of integers) longra = 1188000 (Number of reals) (4 bytes/integer, 8 bytes/real) --- User Fortran work arrays: nituse = 0 (Number of integers) nrtuse = 0 (Number of reals) --- Information on the volumes Minimum control volume = 0.405021068E-03 Maximum control volume = 0.309605049E+01 Total volume for the domain = 0.745030842E+03 --- Phase: 1 ALMAX = 0.90455E+01 (Characteristic length ) ALMAX is the cubic root of the domain volume. ALMAX is the length used to initialize the turbulence. 0 K-EPS VALUES BEYOND THE SCALES BASED ON ALMAX ----------------------------------------------------------- ** VARIABLES INITIALIZATION ------------------------ --------------------------------- Variable Min. value Max. value --------------------------------- Pressure 0.0000E+00 0.0000E+00 Velocity 0.0000E+00 0.0000E+00 Velocity 0.0000E+00 0.0000E+00 Velocity 0.0000E+00 0.0000E+00 Turb Kin 0.6000E-03 0.6000E-03 Turb Dis 0.1462E-06 0.1462E-06 --------------------------------- Tz 0.1000E-01 0.1000E-01 --------------------------------- ------------------------------------------------------------- ALL PHASES : 1D-WALL THERMAL MODULE NOT ACTIVATED NFPT1D = 0 ------------------------------------------------------------- PHASE 1 : HEAD LOSS TREATMENT NOT ACTIVATED NCEPDC = 0 ------------------------------------------------------------- PHASE 1 : MASS SOURCE TERMS TREATMENT NOT ACTIVATED NCETSM = 0 ------------------------------------------------------------- =============================================================== MAIN CALCULATION ================ =============================================================== =============================================================== INSTANT 0.100000000E-01 TIME STEP NUMBER 1 ============================================================= --- Phase: 1 --------------------------------- Property Min. value Max. value --------------------------------- Density 0.1000E+04 0.1000E+04 Laminar 0.1000E-02 0.1000E-02 Turb Vis 0.2216E+03 0.2216E+03 --------------------------------- ** INFORMATION ON BOUNDARY FACES TYPE ---------------------------------- Phase : 1 ------------------------------------------------------------------------- Boundary type Code Nb faces ------------------------------------------------------------------------- Inlet 2 80 Smooth wall 5 80 Rough wall 6 0 Symmetry 4 9680 Free outlet 3 60 Undefined 1 0 ------------------------------------------------------------------------- PHASE 1 : Boundary faces with free inlet/outlet detected Update of reference point for total pressure XYZP0 = 0.20000E+02 -0.12500E-01 0.00000E+00 ** BOUNDARY MASS FLOW INFORMATION ------------------------------ Phase : 1 --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 80 0.000000000E+00 Smooth wall 5 80 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 9680 0.000000000E+00 Free outlet 3 60 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Phase 1 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 : 0.13416E-01 0.13416E-01 Dimensionless distance yplus : 0.12227E+03 0.17111E+03 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 0 Total number of wall faces : 80 ------------------------------------------------------------ ** PHASE 1 SOLVING K-EPSILON ------------------------------ GRADRC ISWEEP = 4 NORMED RESIDUAL: 0.1953E-07 NORM: 0.2727E+01 PARAMETER IVAR = 2 GRADRC ISWEEP = 105 NORMED RESIDUAL: 0.2984E+00 NORM: 0.2699E-11 PARAMETER IVAR = 0 @ @ @@ WARNING: NON CONVERGENCE OF GRADRC @ ======== @ Turb Kin : CONVECTION IN CENTRE BLENDING WITH 100. % OF UPWIND Turb Kin : 9450 FACES WITH UPWIND ON 9450 INTERIOR FACES Turb Kin : EXPLICIT BALANCE = 0.11322E+04 Turb Kin : CONVECTION IN CENTRE BLENDING WITH 100. % OF UPWIND Turb Kin : 9450 FACES WITH UPWIND ON 9450 INTERIOR FACES Jacobi [Turb Kin]: n_iter res_abs res_nor 1 1.1322e+03 5.1658e-01 2 3.4006e+01 1.5516e-02 3 1.1538e+01 5.2643e-03 4 5.8644e+00 2.6758e-03 5 3.2716e+00 1.4927e-03 6 1.9037e+00 8.6860e-04 7 1.1324e+00 5.1670e-04 8 6.8271e-01 3.1150e-04 9 4.1446e-01 1.8911e-04 10 2.5279e-01 1.1534e-04 11 1.5444e-01 7.0469e-05 12 9.4502e-02 4.3119e-05 13 5.7817e-02 2.6380e-05 14 3.5393e-02 1.6149e-05 15 2.1658e-02 9.8820e-06 16 1.3268e-02 6.0537e-06 17 8.1382e-03 3.7132e-06 18 5.0143e-03 2.2879e-06 19 3.1146e-03 1.4211e-06 20 1.9680e-03 8.9793e-07 21 1.2807e-03 5.8434e-07 22 8.7376e-04 3.9867e-07 23 6.3357e-04 2.8908e-07 24 4.8947e-04 2.2333e-07 25 3.9810e-04 1.8164e-07 26 3.3516e-04 1.5292e-07 27 2.8792e-04 1.3137e-07 28 2.5008e-04 1.1411e-07 29 2.1849e-04 9.9692e-08 30 1.9149e-04 8.7374e-08 31 1.6814e-04 7.6717e-08 32 1.4780e-04 6.7436e-08 33 1.3002e-04 5.9326e-08 34 1.1446e-04 5.2223e-08 35 1.0081e-04 4.5996e-08 36 8.8831e-05 4.0531e-08 37 7.8313e-05 3.5732e-08 38 6.9070e-05 3.1515e-08 39 6.0944e-05 2.7807e-08 40 5.3795e-05 2.4545e-08 41 4.7504e-05 2.1675e-08 42 4.1965e-05 1.9147e-08 43 3.7086e-05 1.6921e-08 44 3.2786e-05 1.4959e-08 45 2.8995e-05 1.3229e-08 46 2.5651e-05 1.1704e-08 47 2.2701e-05 1.0358e-08 48 2.0096e-05 9.1694e-09 Turb Kin : CV-DIF-TS 1 IT - RES= 0.11322E+04 NORM= 0.21917E+04 @ @ @@ WARNING: Turb Kin CONVECTION-DIFFUSION-SOURCE TERMS @ ======== @ Maximum number of iterations 1 reached @ 0 K-EPS VALUES BEYOND THE SCALES BASED ON ALMAX Write final restart files checkpoint at iteration 1, Physical time 0.10000E-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 auxilliary 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 CPU time for restart files: 0.40000E-02 ** INFORMATION ON CONVERGENCE -------------------------- --------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual derive --------------------------------------------------------------- c Pressure 0.50632E+04 898 0.88447E-08 0.10000E+01 c VelocityX 0.17455E+04 29 0.62659E-08 0.96842E+02 c VelocityY 0.00000E+00 0 0.00000E+00 0.27628E+00 c VelocityZ 0.00000E+00 0 0.00000E+00 0.11784E-07 c Turb Kinetic 0.21917E+04 48 0.91694E-08 0.10480E-04 c Turb Dissipa 0.68849E+01 174 0.99042E-08 0.24359E-06 --------------------------------------------------------------- ** INFORMATION ON VARIABLES ------------------------ --------------------------------------------------------------- Variable Min. value Max. value Min clip Max clip --------------------------------------------------------------- v Pressure 0.90092E+05 0.31747E+07 -- -- v VelocityX 0.22442E+00 0.12437E+01 -- -- v VelocityY -0.38279E+00 0.44476E+00 -- -- v VelocityZ -0.94790E-04 0.14940E-04 -- -- v Turb Kinetic 0.58528E-03 0.20071E-02 0 0 v Turb Dissipa 0.14623E-06 0.70413E-02 0 0 v Density 0.10000E+04 0.10000E+04 0 0 v Turb Viscosi 0.22157E+03 0.22157E+03 0 0 v Total Pressu 0.19142E+06 0.32760E+07 0 0 --------------------------------------------------------------- ** INFORMATION ON CLIPPINGS ------------------------ --------------------------------------------------------------- Variable Min wo clips Max wo clips Min clip Max clip --------------------------------------------------------------- a Turb Kinetic 0.58528E-03 0.20071E-02 0 0 a Turb Dissipa 0.14623E-06 0.70413E-02 0 0 --------------------------------------------------------------- ** INFORMATION ON THE TIME STEP ----------------------------- --------------------------------------------------------------- Criterion Value at xc yc zc --------------------------------------------------------------- Courant min 0.00000E+00 0.25000E-01 -0.12500E-01 0.00000E+00 Courant max 0.00000E+00 0.25000E-01 -0.12500E-01 0.00000E+00 Fourier min 0.15189E-02 0.19099E+02 -0.11641E+02 0.00000E+00 Fourier max 0.22627E+02 -0.97431E+00 0.92574E-01 0.18457E-03 Cou_Fou min 0.15189E-02 0.19099E+02 -0.11641E+02 0.00000E+00 Cou_Fou max 0.22627E+02 -0.97431E+00 0.92574E-01 0.18457E-03 --------------------------------------------------------------- CPU TIME FOR THE TIME STEP 1: 0.21997E+00 =============================================================== =============================================================== FINAL STAGE OF THE CALCULATION ============================== =========================================================== ** CPU TIME FOR FINAL WRITING: 0.10000E-02 --------------------------- =========================================================== END OF CALCULATION ================== =============================================================== Summary of multigrid for "Pressure": Smoother: Conjugate gradient Coarsest level solver: Conjugate gradient Number of constructions: 1 Number of resolutions: 2 Number of levels: minimum: 5 maximum: 5 mean: 5 Number of iterations: on finest grid: minimum: 191 maximum: 289 mean: 240 on coarsest grid: minimum: 174 maximum: 301 mean: 237 total on grids: minimum: 3496 maximum: 5414 mean: 4455 equivalent (total weighted by number of cells) : minimum: 357 maximum: 541 mean: 449 Associated times (construction, resolution) total elapsed: 0.002 0.081 Total CPU time: 0.002 0.081 Summary of resolutions for Turb Dis (Jacobi): Number of calls: 1 Minimum number of iterations: 174 Maximum number of iterations: 174 Mean number of iterations: 174 Total elapsed time: 0.010 Total CPU time: 0.011 Summary of resolutions for Turb Kin (Jacobi): Number of calls: 1 Minimum number of iterations: 48 Maximum number of iterations: 48 Mean number of iterations: 48 Total elapsed time: 0.003 Total CPU time: 0.004 Summary of resolutions for Velocity (Jacobi): Number of calls: 3 Minimum number of iterations: 0 Maximum number of iterations: 29 Mean number of iterations: 9 Total elapsed time: 0.002 Total CPU time: 0.002 Destroying structures and ending computation Writing of "chr" (EnSight Gold) summary: CPU time for meshes: 0.001 CPU time for variables: 0.002 Elapsed time for meshes: 0.001 Elapsed time for variables: 0.002 Checkpoint / restart files summary: Number of files read: 0 Number of files written: 2 Elapsed time for reading: 0.000 Elapsed time for writing: 0.005 Calculation time summary: User CPU time: 0.221 s System CPU time: 0.022 s Elapsed time: 0.263 s CPU / elapsed time 0.922 Memory use summary: Total memory used: 144.488 mb Theoretical instrumented dynamic memory: 13.139 mb Fortran work arrays memory use: 103801 integers needed (maximum reached in TRIDIM) 795901 reals needed (maximum reached in MEMCLI) Local maximum work memory requested 10.441 mb used 6.623 mb